N390AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
168 reports on file, 1997-08-11 – 2021-04-28.
Part: KEELBEAM — DAMAGED (BS 720 RBL9.5) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND DAMAGED HOLE ON KEEL BEAM, STA 720, RBL 9.5
Part: SKIN — DAMAGED (BS 889-991) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND GOUGES AND SCRATCHES AT TREE (3) LOCATION UNDER THE LH PASSENGER AFT ENTRY DOOR CUTOUT, DOOR STA 889 - 991, STR 20L -22L.
Part: KEELBEAM — CORRODED (BS 788 LBL9.5) · corrosion level 2 · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND CORROSION ON KEEL BEAM SPLICE FITTING IN FOUR (4) PLACES.
Part: SKIN — DENTED (FUSELAGE) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND THREE (3) DENTS ON EXTERNAL FUSELAGE SKIN BETWEEN DOOR STA 111 AND DOOR STA 129, BETWEEN STR 7L AND 9L.
Part: SKIN — DAMAGED (BS 1395 S26R) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND A SCRATCH EXTERNAL FUSELAGE SKIN, STA 1395, STR 26R.
Part: FRAME — CORRODED (BS 1373 S17R) · corrosion level 2 · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND CORROSION IN MAIN DECK FRAME OUTBD CHORD FREE FLANGE AT STA 1373, STR 17R
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND GOUGES, NICKS AND SCRATCHES ON FWD EDGE OF BULK CARGO DOOR CUTOUT, SEC 46, BETWEEN STA 1395 AND STA 1471, STR 26L TO STR 31L.
Part: SKIN — SCRATCHED (BS 478-522) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND SEVERAL SCRATCHES ON EXTERNAL FUSELAGE SKIN COMMON TO FASTENERS ZONE AND LARGE CARGO DOOR CUTOUT.
Part: SKIN — BULGED (BS 522-544) · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND SEVERAL BULGED AREAS ON THE EXTERNAL FUSELAGE SKIN, SEC 43, STA 522 TO STA 544, STR 31L TO STR 32L.
Part: FRAME — CORRODED (BS 1285 S17R) · corrosion level 2 · airframe 98,630 hrs · 16,219 cycles
DURING MAINTENENCE INSPECTION FOUND CORROSION IN MAIN DECK FRAME OUTBD CHORD FREE FLANGE AT STA 1285, STR 17R.
Earlier reports · 1997–2020 · 158 reports
2020
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,408 hrs · 16,159 cycles
AIRCRAFT WAS GROUNDED: OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND BATTERY PACK DEFECTIVE AND REPLACED BATTERY PACK PER AMM 33-51-07.
2019
Part: LIGHT — INOPERATIVE (SEAT 13B)
SEAT 13B SEAT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD
Part: LOCK — UNLOCKED (CARGO BAY) · airframe 97,279 hrs · 15,871 cycles
AIRCRAFT NOT GROUNDED: CREW DECLARED AN EMERGENCY INTO MIA ON ACCOUNT OF NOISE COMING FROM NOSE LANDING GEAR. MAINTENANCE CHECKED AIRCRAFT AND CONFIRMED CARGO INCORRECTLY LOADED AND CARGO LOCKS NOT IN LOCKED POSITION. CARGO SYSTEM CHECK OK.
Part: STRINGER SPLICE — CORRODED (BS 1225) · corrosion level 2 · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER SPLICE AT BS 1225 AND S39L. REPLACED STRINGER SPLICE PER AARD 51-00-05-1.
Part: BATTERY PACK — FAILED (CABIN) · 15,861 cycles
EMERGENCY LIGHTS DID NOT TEST.
Part: CHARGER — FAILED (CABIN) · 15,861 cycles
EMERGENCY LIGHT DID NOT TEST.
Part: WEB — CRACKED (FUSELAGE) · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED WEB AT BS 1197 AND LBL 44. REPAIRED WEB PER SRM 51-70-13
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR TIE AT BS 1562 BETWEEN S39L AND S39R. REPLACED SHEAR TIE PER SRM 51-10-02-0G.
Part: FRAME — CORRODED (FUSELAGE) · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME UPPER T CHORD AT BS 1197 MINUS 88, BETWEEN S31L AND S31R. REPACED T CHORD PER AARD 51-00-05-1.
Part: FRAME — CORRODED (FUSELAGE) · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME UPPER T CHORD AT BS 1197 +132 BETWEEN S31L AND S31R. REPLACED T CHORD PER AARD 51-00-05-1.
Part: SHIM — CORRODED (BS 1219) · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHIMAT BS 1219 AND S38L. REPLACED SHIMS PER SRM 51-20-11.
Part: STRINGER — CORRODED (BS 1197) · corrosion level 2 · airframe 97,242 hrs · 15,861 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER AT BS 1197 + 105 AT S36L. REPAIRED STRINGER PER SRM 53-00-03-2R.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 96,954 hrs · 15,809 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT HAND MID FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 96,954 hrs · 15,809 cycles
AIRCRAFT NOT GROUNDED: RH MID FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACE RH MID FLASHLIGHT BATTERY IAW AMM 25-64-00 OPS CHECK GOOD.
Part: LIGHT — DAMAGED (CABIN) · airframe 96,711 hrs · 15,757 cycles
AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 3A FORWARD POSITION DAMAGED. MAINTENANCE REPLACED LIGHT LUMINATOR ASSEMBLY PER AMM 33-51-00.
Part: LIGHT — DAMAGED (CABIN) · airframe 96,711 hrs · 15,757 cycles
AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 3A FORWARD POSITION DAMAGED. MAINTENANCE REPLACED LIGHT LUMINATOR ASSEMBLY PER AMM 33-51-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 96,711 hrs · 15,757 cycles
AIRCRAFT WAS GROUNDED: EMERGENCY FLASHLIGHT WAS NOT SECURED AND INOPERABLE AT RIGHT HAND MID GALLEY FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACED BATTERY PER AMM 25-64-00.
Part: PUMP — UNRELIABLE (OVERIDE) · airframe 96,233 hrs · 15,659 cycles
AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF FUEL QUANTITY LOSS AND FUEL IMBALANCE. MAINTENANCE ACCOMPLISHED FIM 28-22-00815-829. REMOVED AND REPLACED CENTER OVRD FUEL PUMP IAW AMM 28-22-05. OPS CHECK GOOD. LEAK CHECK GOOD.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 96,159 hrs · 15,643 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 3A FORWARD EMERGENCY WHITE LIGHT INOPERATIVE. MAINTENANCE RECONNECTED WIRES TO EMERGENCY LIGHT AT SEAT 3A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: SENSOR — FAULTY (ZONE 200) · airframe 96,023 hrs · 15,614 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS EMERGENCY DOORS LIGHT ILLUMINATED ON OVERHEAD PANEL. FOLLOWED A FEW MINUTES LATER BY R WING SLIDE ON EICAS. MAINTENANCE REMOVED AND REPLACED SENSOR S199 IAW AMM 52-71-01.
Part: CONTROL UNIT — FAULTY (ANTI-SKID SYS) · airframe 95,868 hrs · 15,583 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS AFTER MAIN GEAR TOUCHDOWN AUTOBRAKES DISARMED. MAINTENANCE REMOVED AND REPLACED THE ANTISKID/AUTOBRAKE CONTROL UNIT IAW AMM 32-42-01. OPS CHECK GOOD.
Part: MODULE — LEAKING (FLAP SLAT) · airframe 95,062 hrs · 15,397 cycles
CENTER HYDRAULIC LEAK SUBSEQUENT LOW HYDRAULIC PRESSURE, FOLLOWED BY CENTER SYSTEM FAILURE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND HEAVY LEAK AT FLAP/SLAP SHUTOFF VALVE MODULE AND REPLACED FLAP/SLAT MODULE PER AMM 27-51-48. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK. NO LEAKS NOTED.
2018
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 92,504 hrs · 14,894 cycles
COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. INSTALLED A SERVICEABLE EMERGENCY LIGHT IAW AMM 33-51-01.
Part: FLOORBEAM — CORRODED (BS 287) · airframe 92,504 hrs · 14,894 cycles
CORROSION ON THE FLOORBEAM AT BS 287, RBL 83. REPAIRED THE FLOORBEAM IAW SRM 53-00-51-2R-1.
Part: FLOOR SUPPORT — CRACKED (BS 325-347) · airframe 92,504 hrs · 14,894 cycles
FLOOR SUPPORT CRACKED BETWEEN BS 325 AND 347 AT LBL 40. REPLACED THE FLOOR SUPPORT IAW 51-00-05.
Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 92,504 hrs · 14,894 cycles
CORROSION ON THE FLOORBEAM UPPER TEE SPLICE AT BS 325, LBL 13 TO LBL 27. AROUND THE SCREW HOLES. REPLACED THE FLOORBEAM UPPER TEE IAW SRM 53-00-51-2R-1.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,504 hrs · 14,894 cycles
EMERGENCY LIGHTS, FIRST CLASS LEFT SIDE, SEATS 2A TO 4A FAILED A 10 MINUTE ILLUMINATION TEST. REPLACED THE BATTERY AND CHARGER IAW AMM 33-51-00.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,504 hrs · 14,894 cycles
EMERGENCY LIGHTS, FIRST CLASS LEFT SIDE SEATS 2A TO 4A FAILED A 10 MINUTE ILLUMINATION TEST. REPLACED THE BATTERY AND CHARGER IAW AMM 33-51-00.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,504 hrs · 14,894 cycles
EMERGENCY LIGHTS, LEFT CEILING LIGHTS AT L1 DOOR TO SEAT ROW 13 FAILED AN ILLUMINATION TEST. REPLACED THE BATTERY AND CHARGER IAW AMM 33-51-00.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,504 hrs · 14,894 cycles
EMERGENCY LIGHTS, LEFT CEILING LIGHTS AT L1 DOOR TO SEAT ROW 13 FAILED AN ILLUMINATION TEST. REPLACED THE BATTERY AND CHARGER IAW AMM 33-51-00.
Part: COFFEEMAKER — LEAKING (GALLEY) · airframe 92,394 hrs · 14,873 cycles
THE AIRCRAFT WAS NOT GROUNDED. COFFEE MAKER 3 IS LEAKING AND CAUSING FUMES IN MID GALLEY. TURNED OFF POWER AND WATER TO BOTH COFFEE MAKER 3 AND 4. INSTALLED NEW COFFEE MAKER 3 AND 4 PER 25-32-00. OPERATIONS CHECK OK. REMOVED PLACARD AND CLEARED MIC SHEET. TURNED ON WATER AND NO LEAKS NOTED.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 92,280 hrs · 14,857 cycles
AFT GALLEY LEFT AND CENTER LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE, CENTER. GALLEY LEFT FOWARD. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND PERFORMED SATISFACTORY OPS CHECK.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 92,009 hrs · 14,799 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT RIGHT SIDE OF ROWS 25 TO 31 INOPERABLE. RESEATED CONNECTOR AT SEAT POSITION 28HJ. EMERGENCY LIGHTS CHECKED NORMAL PER AMM 33-51-00.
2017
Part: LATCH — OUT OF ADJUST (RT OVERWING) · airframe 91,916 hrs · 14,777 cycles
RIGHT OVERWING SLIDE LIGHT MESSAGE. MAINTENANCE ADJUSTED RIGHT WING SLIDE DOOR LATCH SENSOR IAW MM 52-71-00. OPERATIONS CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 91,763 hrs · 14,749 cycles
AIRCRAFT WAS GROUNDED. FOUND EMERGENCY LIGHTS AT RIGHT AND LEFT LAVATORY FLOOD EXIT, OPERABLE. REPLACED POWER SUPPLY (CHARGER) AND BATTERY M1210 PER AMM 33-51-07 (SEE ALSO AALA201712089015 FOR BATTERY).
Part: POWER SUPPLY — FAULTY (CABIN) · airframe 91,763 hrs · 14,749 cycles
AIRCRAFT WAS GROUNDED. ESCAPE PATH LIGHT RIGHT HAND ROW 20 AND 21, INOPERABLE. FOUND POWER SUPPLY AT M1209 FAULTY. REPLACED POWER SUPPLY (CHARGER) PER AMM 33-51-07.
Part: BATTERY — DISCHARGED (CABIN) · airframe 91,763 hrs · 14,749 cycles
AIRCRAFT WAS GROUNDED. FOUND EMERGENCY LIGHTS AT RIGHT AND LEFT LAVATORY FLOOD EXIT, INOPERABLE. REPLACED POWER SUPPLY AND BATTERY M1210 PER AMM 33-51-07 (SEE ALSO AALA20171206006 FOR POWER SUPPLY - CHARGER).
Part: CHARGER — INOPERATIVE (CABIN) · airframe 91,763 hrs · 14,749 cycles
AIRCRAFT WAS GROUNDED. ESCAPE PATH LIGHT RIGHT HAND ROW 25 THRU 35, INOPERABLE. FOUND FAULTY POWER SUPPLY AT M1209. REPLACED POWER SUPPLY (CHARGER) PER AMM 33-51-07.
Part: BATTERY — DISCHARGED (CABIN) · airframe 91,516 hrs · 14,692 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY EXIT LIGHTS BATTERY AND CHARGER M730 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AND CHARGER ASSEMBLY (AALA201710279002) PER AMM 33-51-07. OPERATIONAL CHECK GOOD.
Part: CHARGER — FAILED (CABIN)
AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY EXIT LIGHTS BATTERY AND CHARGER M730 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY (AALA20171025004) AND CHARGER ASSEMBLY PER AMM 33-51-07. OPERATIONAL CHECK GOOD.
Part: FITTING — MISSING (APU DOOR) · airframe 91,510 hrs · 14,691 cycles
AIRCRAFT WAS GROUNDED. AUXILIARY POWER UNIT FAILED INFLIGHT AFTER APPROXIMATELY 4 HOURS AT 36000 FEET. APU WOULD NOT RESTART. FOUND APU INLET DOOR AND DOOR ACTUATOR ROD END FITTING MISSING. INSTALLED APU INLET DOOR PER AMM 49-15-05 (AALA201710099042) AND APU DOOR ACTUATOR ASSEMBLY PER AMM 49-15-06. OPERATIONAL CHECK GOOD. REFERENCE AALA20171004014
Part: IDG — DISCONNECTED (RIGHT) · airframe 91,510 hrs · 14,691 cycles
RIGHT ENGINE INTEGRATED DRIVE GENERATOR LIGHT ILLUMINATED DURING FLIGHT. IDG WAS DISCONNECTED AND APU STARTED BUT IT FAILED AFTER A FEW HOURS. EMERGENCY DECLARED. FLIGHT DIVERTED. LANDING UNEVENTFUL. REMOVED AND REPLACED INTEGRATED DRIVE GENERATOR ASSEMBLY IAW AMM 24-11-01. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
Part: DOOR — MISSING (APU BAY) · airframe 91,510 hrs · 14,691 cycles
AIRCRAFT WAS GROUNDED. AUXILIARY POWER UNIT FAILED INFLIGHT AFTER APPROXIMATELY 4 HOURS AT 36000 FEET. APU WOULD NOT RESTART. FOUND APU INLET DOOR AND DOOR ACTUATOR ROD END FITTING MISSING. INSTALLED APU INLET DOOR PER AMM 49-15-05 AND APU DOOR ACTUATOR ASSEMBLY PER AMM 49-15-06 (AALA201710249012) . OPERATIONAL CHECK GOOD. REFERENCE AALA20171004014 (CLOSED)
Part: COOLING FAN — ODOR (NR 1) · airframe 91,415 hrs · 14,668 cycles
FLIGHT DIVERTED DUE TO A FORWARD EQUIPMENT OVERHEAT EICAS MESSAGE AND STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. LANDING UNEVENTFUL. REMOVED AND REPLACED FORWARD EQUIPMENT COOLING SUPPLY FAN NR 1 IAW AMM 21-58-06. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: DRIVE SHAFT — CORRODED (TE FLAP) · airframe 90,490 hrs · 14,490 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON TRAILING EDGE OUTBOARD FLAP NR 7 ROTARY ACTUATOR DRIVE ARM SHAFT SPLINE, AT THE 3:00 TO 5:00 POSITION LOOKING OUTBOARD. REPAIRED IAW SRM 51-10-02-OG, AMM 27-51-22, AND EA 269911.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 90,206 hrs · 14,434 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT RIGHT SIDE MID CABIN IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 89,860 hrs · 14,377 cycles
AIRCRAFT WAS NOT GROUNDED. TWO FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS IN THE FORWARD CABIN ARE INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPERATIONAL CHECK GOOD. SEE ALSO AALA201703099039
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 89,860 hrs · 14,377 cycles
AIRCRAFT WAS NOT GROUNDED. TWO FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS IN THE FORWARD CABIN ARE INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPERATIONAL CHECK GOOD. SEE ALSO AALA201703109015
Part: LIGHT — BROKEN (CABIN) · airframe 89,705 hrs · 14,346 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHT AT SEAT 20J HAS BROKEN TABS. REMOVED AND REPLACED LIGHT ASSEMBLY L793 IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 89,559 hrs · 14,315 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MIDDLE RIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW ESO 60849. OPERATIONAL CHECK GOOD.
Part: ENGINE — FAULTY (NR 1) · airframe 89,495 hrs · 14,306 cycles
AIRCRAFT WAS GROUNDED. FLIGHT DIVERTED. EMERGENCY DECLARED. AT APPROXIMATELY 3 HOURS AND 35 MINUTES INTO FLIGHT NR 1 ENGINE OIL QUANTITY SHOWED 0 FOLLOWED BY DECREASING OIL PRESSURE. ENGINEERING REPORTED BORESCOPE OF THE COMPRESSOR REAR FRAME INDICATED COKING BUT WAS UNABLE TO CONFIRM SOURCE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 89,277 hrs · 14,270 cycles
AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ACROSS FROM LAVATORY M2 FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPERATIONAL CHECK GOOD.
2016
Part: LENS — MISSING (EXIT SIGN) · airframe 88,730 hrs · 14,172 cycles
AIRCRAFT WAS NOT GROUNDED. OVERWING EXIT SIGN NEAR SEAT 20AB IS MISSING LENS. REPLACED SIGN ASSEMBLY AND LENS IAW AMM 33-51-01. OPERATIONAL CHECK NORMAL. SEE ALSO AALA20161102008.
Part: LENS — MISSING (EXIT SIGN) · airframe 88,730 hrs · 14,172 cycles
AIRCRAFT WAS NOT GROUNDED. OVERWING EXIT SIGN NEAR SEAT 20AB IS MISSING LENS. REPLACED SIGN ASSEMBLY AND LENS IAW AMM 33-51-01. OPERATIONAL CHECK NORMAL. SEE ALSO AALA20161102009.
Part: SENSOR — LEAKING (NR 1 ENGINE) · airframe 88,585 hrs · 14,148 cycles
AIRCRAFT WAS GROUNDED. AFTER PUSH BACK FROM GATE THE GROUND CREW REPORTED A FUEL LEAK FROM NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE T2 SENSOR IAW AMM 73-21-05. ENGINE RUN AND LEAK CHECK NORMAL.
Part: ANTI-SKID VALVE — FAULTY (MLG) · airframe 88,367 hrs · 14,115 cycles
AFTER ARRIVAL AT GATE, NR 2 AND 6 WHEEL FUSE PLUGS BLEW. REMOVED AND REPLACED WHEEL ASSEMBLIES . AFTER NEXT FLIGHT SMOKE WAS OBSERVED FROM LEFT MAIN GEAR INNER SIDE. MAINTENANCE REMOVED AND REPLACED THE LEFT ANTI-SKID VALVE ASSEMBLY IAW AMM 32-42-02. OPS AND LEAK CHECKED GOOD.
Part: BEAM — CORRODED (LT MLG) · corrosion level 2 · airframe 88,190 hrs · 14,091 cycles
CORROSION FOUND ON INNER BORE OF LEFT MAIN LANDING GEAR WALKING BEAM. REPAIRED THE BEAM IAW EA 263112.
Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 88,176 hrs · 14,084 cycles
EMERGENCY EXIT SIGN ON LOWER LEFT CORNER OF R1 DOOR IS MISSING. AIRCRAFT GROUNDED. INSTALLED EXIT SIGN ASSEMBLY IAW MM 33-51-09. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,800 hrs · 14,016 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT FIXTURE AT SEAT 30B IS INOPERATIVE. R & R EMERGENCY LIGHT FIXTURE AT SEAT 30B IAW 33-60-98. NORMAL OPERATION RESTORED.
Part: LENS — MISSING (EXIT SIGN) · airframe 87,295 hrs · 13,926 cycles
AIRCRAFT WAS NOT GNDED. CREW REPORTS AFT FACING EXIT SIGN AT ROW 21ABC IS MISSING. REPLACED LENS AT ROW 21ABC EXIT SIGN IAW AMM 33-51-01. SYS CHECKED NORMAL.
Part: ROD — OUT OF ADJUST (NLG DOOR) · airframe 86,978 hrs · 13,865 cycles
AIRCRAFT WAS GNDED. DURING CLIMB UPON GEAR DOOR RETRACTION, THE GEAR DOORS LIGHT REMAINED ILLUMINATED WITH NOTICEABLE NOISE FROM NOSE GEAR AREA. RECYCLED GEAR DOORS & LIGHT EXTINGUISHED. ACCOMPLISHED NLG NR 3 ROD ADJUSTMENT IAW AMM 32-22-02. ACCOMPLISHED JACKING PROCEDURE IAW AMM 07-11-02. OPERATIONAL CHECKED GOOD.
2015
Part: SIGN — DAMAGED (CABIN) · airframe 84,554 hrs · 13,436 cycles
LEFT AFT OVERWING ESCAPE DOOR EXIT SIGN L700 IS DAMAGED. R & R EXIT SIGN IAW AMM 33-51-01. PERFORMED OPERATIONAL CHECK. SYSTEM CHECKED NORMAL.
Part: CHARGER — FAULTY (CABIN) · airframe 84,554 hrs · 13,436 cycles
LEFT & RIGHT AFT OVERWING DOOR ESCAPE EXIT SIGN INOPERATIVE. R & R BATTERY & CHARGER AT M1209 IAW AMM 33-51-07. PERFORMED OPERATIONAL CHECK. SYSTEM CHECKED NORMAL. SEE ALSO AALA20150728006.
Part: BATTERY — DISCHARGED (CABIN) · airframe 84,554 hrs · 13,436 cycles
LEFT & RIGHT AFT OVERWING DOOR ESCAPE EXIT SIGN INOPERATIVE. R & R BATTERY & CHARGER AT M1209 IAW AMM 33-51-07. PERFORMED OPERATIONAL CHECK. SYSTEM CHECKED NORMAL. SEE ALSO AALA20150730006.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,046 hrs · 13,355 cycles
AFT SEAT MOUNTED EMER LIGHT INOPERATIVE AT SEAT 4J. REPLACED AFT EMER LIGHT ASSEMBLY. ACCOMPLISHED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED IAW AMM 33-51-10.
Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 83,583 hrs · 13,286 cycles
INOPERATIVE EMERGENCY EXIT LIGHT L781 AT LT AISLE CEILING PANEL AT SEAT 12B, BS 681. SPLICED WIRES SMZ90230 & SMZ90229 IAW SWPM 20-30-12 & DWG MZS18711250 REV E. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00-725-247.
Part: BEARING — FAILED (NR 4) · airframe 83,552 hrs · 13,279 cycles
DURING CRUISE, CREW REPORTED AUDIBLE BOOM, RUMBLE & LOSS OF FUEL FLOW ON LT ENG. SHUTDOWN LT ENG. EMERGENCY DECLARED, RETURNED TO DEPARTURE AND LANDING WAS UNEVENTFUL. R & R LT ENGINE. POWER PLANT ENGINEERING REPORTS NR 4 BEARING FAILED.
Part: BATTERY — WEAK (CABIN) · airframe 83,530 hrs · 13,271 cycles
EMERGENCY BATTERY PACK DID NOT POWER EMER LIGHTS FOR THE DURATION OF 15 MIN REQUIRED BY MCM CARD 279A. R & R BATTERY & CHARGER M734.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 82,882 hrs · 13,153 cycles
SEAT 22H, 23H & 24H AISLE EMER LIGHT INOPERATIVE. R & R BATTERY PACK & CHARGER M732 IAW AMM 33-51-07. SYS CHECKED NORMAL.
2014
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,367 hrs · 13,065 cycles
EMERGENCY LIGHTS AT 22 - 24HJ ARE INOPERATIVE, REPLACED BATTERY PACK.
Part: GCU — FAILED (ZONE 200) · airframe 82,226 hrs · 13,039 cycles
AIR INTERRUPT, LT & RT UTILITY BUSSES TRIPPED OFF DURING TAKEOFF & WOULD NOT RESET. BURNING ODOR WAS REPORTED FROM AFT & MIDDLE CABIN, DISSIPATED AFTER UTILITY BUSSES TRIPPED OFF. FOUND LT GCU TO BE AT FAULT. REPLACED LT & RT GCU`S IAW AMM 24-22-02. RAN BOTH ENGS AT HIGH POWER, CHECKED UTILITY BUSSES IAW AMM 71-00-00. SYS CHECKED NORMAL.
Part: ENGINE — LEAKING (LEFT) · airframe 82,224 hrs · 13,037 cycles
LEFT GEN MALFUNCTIONED WITH POSSIBLE ARCING. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND OIL LEAK ON LT ENG. REPLACED LT ENG ON 10/29/14. SYS GND CHECKED NORMAL OPERATION OPEN.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 81,939 hrs · 12,993 cycles
LEFT WING SLIDE & AFT LT DOOR SLIDE EMER GND ILLUMINATION LIGHTS L396, L397 & L645 INOPERATIVE. R & R POWER SUPPLY M738 & BATTERY PACK. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,090 hrs · 12,864 cycles
SEAT MOUNTED EMER LIGHT AT 30H INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMER LIGHT AT 30H. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
20AB EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR 20AB EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
21HJ EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR 21HJ EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
20HJ EMERGENCY EXIT SIGN LAMP INOPERATIVE. REPLACED LAMP FOR 20HJ EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LENS — MISSING (CABIN) · airframe 80,314 hrs · 12,743 cycles
SEAT 12C EMERGENCY LIGHT MISSING LENS. REPLACED LENS FOR SEAT 12C EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
RT NR 1 DOOR EMERGENCY LIGHT OUT IN SILL. REPLACED LAMP FOR RT NR 1 DOOR EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
LEFT NR 1 DOOR LOWER PORTION EMERGENCY EXIT SIGN BULBS INOPERATIVE. REPLACED LAMPS FOR LT NR 1 DOOR EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,314 hrs · 12,743 cycles
EMERGENCY LIGHT AT ROW 49 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 49. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,314 hrs · 12,743 cycles
21AB EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR 21AB EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 80,196 hrs · 12,727 cycles
RT HAND FWD OVERWING SLIDE WING ESCAPE PATH EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT HAND FWD OVERWING SLIDE WING ESCAPE PATH EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,794 hrs · 12,516 cycles
SEAT 21H EMERGENCY PATH LIGHT FAILED TEST. REPLACED LAMP FOR SEAT 21H EMERGENCY PATH LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,702 hrs · 12,494 cycles
SEAT 32H EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 32H EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,197 hrs · 12,413 cycles
EMERGENCY LIGHTS FROM ROW 6 H&J TO RT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,408 hrs · 11,976 cycles
RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHTS. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,408 hrs · 11,976 cycles
LEFT NUMBER 1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER 1 DOOR EMERGENCY EXIT LIGHTS. OPS CHECK NORMAL.
2012
Part: RECEPTACLE — FAULTY (CABIN) · airframe 73,955 hrs · 11,755 cycles
CREW REPORT SEAT 3J POWER PORT ENTERTAINMENT PLUG IN PORT SMOKED AND SPARKED. FLIGHT LANDED CDG WITHOUT INCIDENT. DEFERRED INOPERATIVE COMPLETE SYSTEM OF POWERPORTS PER NEF 25N25B. REPLACED SEAT 3HJ ISPS AT MIA ON 09/07/2012. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DEBONDED (TE FLAP) · airframe 72,592 hrs · 11,556 cycles
DISBOND ON LEFT OUTBOARD FLAP LOWER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.
Part: SKIN — PUNCTURED (TE FLAP) · airframe 72,592 hrs · 11,556 cycles
LEFT OUTBOARD FLAP UPPER SURFACE HAS PUNCTURE 83 1/2 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01-2R.
Part: SKIN — DAMAGED (TE FLAP) · airframe 72,592 hrs · 11,556 cycles
LEFT OUTBOARD FLAP UPPER SURFACE HAS PUNTURE 56 3/4 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,592 hrs · 11,556 cycles
AFT DRAIN MAST BOX SUPPORT CORRODED. REPLACED BOX SUPPORT PER SRM 51-40-02.
Part: SKIN — PUNCTURED (TE FLAP) · airframe 72,592 hrs · 11,556 cycles
LEFT OUTBOARD FLAP UPPER SURFACE HAS PUNCTURE 70 3/4 INCHES FROM INBOARD END. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,592 hrs · 11,556 cycles
CABIN RIGHT SIDE BETWEEN STATIONS 1043 AND 1065 STIFFENER JUST BELOW WINDOW HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: SKIN — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
CROWN SKIN NEAR STATION 434 STRINGER 1 RIGHT CENTER FASTENER IN SECOND ROW INBOARD FROM STRINGER 1 RIGHT SHOWS CRACK INDICATION NEAR 7 O`CLOCK POSITION UPON HFEC SURFACE INSPECTION. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-6.
Part: GUARD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,592 hrs · 11,556 cycles
RIGHT NUMBER 2 DOOR SILL SPLASH GUARD HAS CORROSION ON HORIZONTAL AND VERTICAL LEGS IN CENTER OF SPLASH GUARD. REPLACED SPLASH GUARD PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,592 hrs · 11,556 cycles
J-CAP CORRODED AT STATION 1175. REPLACED J-CAP PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1087 TO 1109 AT LEFT BUTTLINE 40 HAS 3 CRACKS AT NUT PLATES. REPLACED INTERCOSTAL ANGLE PER SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1241 TO 1263 AT RIGHT BUTTLINE 40 HAS 2 SMALL HAIRLINE CRACKS AT AROUND NUT PLATES. REPLACED INTERCOSTAL ANGLE PER SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1197+22 AND 1197+44 AT LEFT BUTTLINE 40 HAS SEVERAL CRACKS AT AROUND NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 654+66 TO 654+88 AT LEFT BUTTLINE 40 HAS 1 CRACK. REPLACED INTERCOSTAL ANGLE PER SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT RIGHT BUTTLINE 40 HAS 1 CRACK. REPLACED INTERCOSTAL ANGLE SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1395 TO 1417 AT RIGHT BUTTLINE 48 HAS 1 SMALL HAIRLINE CRACK AT AROUND NUT PLATE. REPLACED INTERCOSTAL ANGLE PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1197+22 TO 1197+44 AT RIGHT BUTTLINE 40 HAS 3 EACH CRACKS AT AROUND NUT PLATES. REPLACED INTERCOSTAL ANGLE PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT FLOOR AREA IN CABIN BETWEEN STATIONS 347 TO 368 AT AROUND RIGHT BUTTLINE 36 HAS 2 SMALL HAIRLINE CRACKS. REPLACED INTERCOSTAL ANGLE PER SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT LEFT BUTTLINE 40 HAS 2 CRACKS. REPLACED INTERCOSTAL ANGLE PER SRM 51-10-02.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
IMPACT DAMAGE TO STRINGER 30 LEFT FROM STATIONS 510 TO 515. CUT OUT DAMAGED SECTION AND INSTALLED NEW SECTION OF STRINGER PER SRM 53-00-03-2R.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
INTERCOSTAL ANGLE AT CABIN FLOOR STRUCTURE, BETWEEN STATIONS 1197+22 TO 1197+44 AT LEFT BUTTLINE 40 HAS SEVERAL CRACKS AT AROUND NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-10-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,592 hrs · 11,556 cycles
CORRODED SHEAR TIE STATION 1197. REPLACED SHEAR TIE.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,592 hrs · 11,556 cycles
VERTICAL STIFFENER IS CRACKED FORWARD SIDE OF STATION 246 LEFT BUTTLINE 40. REPLACED ANGLE PER AARD 53-10-51-2.
Part: SKIN — DEBONDED (RT AILERON) · airframe 72,592 hrs · 11,556 cycles
DISBOND FOUND ON VISUAL INSPECTION OF RIGHT OUTBOARD AILERON UPPER SURFACE. HOTBOND REPAIR PER SRM 57-60-02.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,427 hrs · 11,529 cycles
OVERHEAD EMERGENCY LIGHT IN FRONT OF FS3 LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN FRONT OF FS3 LAVATORY. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,427 hrs · 11,529 cycles
SEAT 40G OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 40G OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,427 hrs · 11,529 cycles
SEAT 10G OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 10G EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,427 hrs · 11,529 cycles
LOWER LEFT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER LEFT AFT EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,427 hrs · 11,529 cycles
RIGHT WING AFT EMERGEMCY EXIT LIGHT OVERWING LAMP INOPERATIVE. REPLACED LAMP. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,427 hrs · 11,529 cycles
SEAT 13B OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 13B OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 72,244 hrs · 11,498 cycles
LHR - CREW REPORTED LEFT AFT LAVATORY SMOKE ALARM WENT OFF ON DESCENT. FLIGHT LANDED LHR WITHOUT INCIDENT. INSPECTED A5 LAVATORY FOR EVIDENCE OF FIRE AND NONE FOUND. REPLACED LEFT AFT LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,618 hrs · 11,078 cycles
EMERGENCY PATH LIGHTS MOUNTED ON LEFT SIDE OF COACH SEAT ROWS 32AB TO 41 AB INOPERATIVE. FOUND FAULTY POWER SUPPLY M739. REPLACED POWER SUPPPLY M739 FOR EMERGENCY LIGHTS. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,618 hrs · 11,078 cycles
EMERGENCY PATH LIGHT ON COACH SEATS ROWS 32AB TO 41AB INOPERATIVE. REPLACED POWER SUPPLY. OPS CHECK NORMAL.
Part: SENSOR — FAULTY (LE SLAT) · airframe 68,273 hrs · 10,865 cycles
ORD - CREW REPORTED "LEADING EDGE SLAT ASYMMETRY" EICAS MESSAGE JUST AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND SENSOR 303 ON NUMBER 9 SLAT FAULTED. REPLACED SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: FSEU — INOPERATIVE (ZONE 100) · airframe 67,390 hrs · 10,720 cycles
ORD - CREW REPORTED EICAS MESSAGE LEADING EDGE SLAT ASSYMETRY. EMERGENCY DECLARED LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH STALL WARNING CARDS (MPN 285T110423) AND FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FSEU — INOPERATIVE (TE FLAP) · airframe 67,246 hrs · 10,687 cycles
CDG - CREW REPORTED AFTER ROTATION STICK SHAKER ACTIVATED, ALPHA SPEED DISPLAYED ON ATTITUDE INDICATOR AND LEADING EDGE SLAT ASYMMETRY. EMERGENCY DECLARED RETURNED CDG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT AND BOTH STALL WARNING CARDS (MPN285T110423). SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 66,904 hrs · 10,630 cycles
THE 2A SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED LAMP FOR 2A PATH LIGHTING. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,986 hrs · 10,291 cycles
EMERGENCY EXIT LIGHT CEILING MOUNTED NEAR FIRST CLASS LAVATORY INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY EXIT LIGHT NEAR FIRST CLASS LAVATORY. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,355 hrs · 10,167 cycles
AISLE EMERGENCY LIGHT AT SEAT 38B INOPERATIVE. REPLACED LAMP FOR AISLE EMERGENCY LIGHT AT SEAT 38B, OPS CHECKS NORMAL.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 20B INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 10B INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 4B INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 4B INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,845 hrs · 10,076 cycles
EMERGENCY LIGHT AT SEAT 20B INOPERATIVE. RELAMPED 20B.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,487 hrs · 10,019 cycles
FOUND EMERGENCY LIGHTS ON LEFT OF AIRCRAFT BETWEEN 24B-36B INOPERATIVE. REPLACED BATTERY PACK.
Part: LENS — MISSING (CABIN) · airframe 63,086 hrs · 9,952 cycles
EMERGENCY EXIT LIGHT SIGN AT OVERHEAD SEAT ROW 20 MISSING COVER. REPLACED EXIT LIGHT SIGN AT OVERHEAD SEAT ROW 20.
2008
Part: CHARGER — FAULTED (MAIN BATTERY) · 59,021 cycles
MAN INFLIGHT T54/21SEP. PRIOR TO FLAP EXTENSION LEADING EDGE ASYMMETRY AND EICAS MSG ILLUMINATED. LANDED WITHOUT INCIDENT MAN WITH 20 DEGREE FLAPS NO SLATS. CLEANED NR 10 SLAT SENSOR AND REPLACED MAIN BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LENS — MISSING (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT SEAT 38B LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — INOPERATIVE (EMERGNECY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 23B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. BLEND IS LOCATED AT STATION 347 AND RIGHT BUTTLINE 11 AND IS APPROXIMATELY ONE INCH IN DIAMETER AND 0,023 INCH DEEP. MATERIAL REMAINING IS WITHIN SRM LIMITS. VERIFIED THE CORROSION WAS COMPLETELY REMOVED. REFINISHED THE BLENDED AREA WITH ALODINE AND TWO COATS BMS10 11. APPLIED CORROSION INHIBITING COMPOUND TO FLOORBEAM.
2003
Part: SMOKE — DETECTED (CABIN)
DFW - FLT 1941 - EN ROUTE DFW-LAS, CREW OBSERVED SMOKE IN THE CABIN. EMERGENCY DECLARED AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT NOT OVERWEIGHT. PERFORMED OPERATIONAL CHECKS ON CHILLERS, OVENS, READING LIGHTS, SIDE AND CEILING LIGHTS, VIDEO CAMERAS, ALL ELECTRICAL COMPONENTS LEFT ON FOR 36 HOURS. RAN BOTH ENGINES TO TAKEOFF N1 ISOLATED BLEED AND PACKS, SWITCH BACK AND FORTH BETWEEN APU AIR AND ENGINE AIR. TEMPERATURES WERE RUN FROM FULL COLD TO FULL HOT, SUPPLIED FROM EARLIER ENGINE. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ORD - OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROW 20C. REPLACED EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: COFFEEMAKER — DIRTY (AFT GALLEY)
LGW - FLT 134 - EN ROUTE STL-LGW, CREW REPORTED SMOKE IN AFT GALLEY. PULLED CIRCUIT BREAKER AND SMOKE DISSIPATED. FOUND DEBRIS ON COFFEE MAKER NR 6. REMOVED DEBRIS NO SMOKE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
2001
Part: WIRE — DAMAGED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 37B HAS A BROKEN WIRE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAULTY (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 31B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 20C BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — DAMAGED (CABIN SEAT)
MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7H INOPERATIVE. REPLACED CONTACT SOCKETS IN SEAT MOUNTED EMERGENCY EXIT LIGHT CONNECTOR AT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FAN — FAILED (ACM BAY)
MXP - FLT 95 - DURING FLIGHT, EICAS MESSAGE INDICATED FORWARD EQUIPMENT COOLING FAN FAILED. CIRCUIT BREAKER TRIPPED AND ELECTRICAL BURNING SMELL IN CABIN. LANDED ORD WITHOUT INCIDENT. REPLACED COOLING FAN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: OVEN — DEFECTIVE (GALLEY)
MIA - FLT 1543 - EN ROUTE MIA-SDQ - FLIGHT ATTENDANTS NOTICED SMELL OF SMOKE AND HAZE IN FIRST CLASS GALLEY. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED OVEN IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — FAILED (AFT FUSELAGE)
SFO - DURING OVERNIGHT MAINTENANCE, RIGHT AFT GROUND ILL EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE TO RIGHT AFT GROUND ILL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: AIR DIST — ODOR (CABIN)
LAX-JFK - FLT 200 - ELECTRICAL BURNING SMELL NOTED IN CABIN. SMELL DISSIPATED BUT RETURNED WHEN GEAR LOWERED UPON RETURN TO LAX. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED WHEEL WELLS, BRAKES, AIR CONDITIONING PACKS AND APU COMPARTMENT WITH NO FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: LIGHT — DIRTY (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT A SEAT ROW 17AB INOPERATIVE. CLEANED EMERGENCY EXIT PATH LIGHT ASSEMBLY CONTACTS AT SEAT ROW 17AB AFTER REPLACING LAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SEAT TRACK — CORRODED (BS 345)
AFW - SEAT TRACK HAD CORROSION BEYOND SRM LIMITS AFTER BLENDOUT. REMOVE SEAT TRACK LIPS ON BOTH SIDE OF DAMAGED AREA PER ENGINEERING MRB 767-1555. (M)
1997
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H FOUND INOPERATIVE. REPLACED PIN ON EMERGENCY LIGHT CONNECTOR AT SEAT 22H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: BATTERIES — MISSING (MEGAPHONE)
ASU - DURING OVERNIGHT CHECK, BOTH CABIN MEGAPHONES INOPERATIVE. REPLACED BATTERIES FOUND MISSING FROM BOTH CABIN MEGAPHONES. MEGAPHONES GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 22H AND 36H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 22H AND RESEATED CONNECTOR AT PAX SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY CHARGER — FAILED (BATTERY COMPT)
JFK - FLT 0048 - MAIN BATTERY CHARGER EICAS STATUS MSG. DIVERT TO JFK. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. ACCOMPLISHED CHECKS PER MM ALL CHECKS. REF: OPERATOR CONTROL NR AALA971523. (X)
Part: BATTERY — DISCHARGED (BATTERY COMPT)
JFK - FLT 0048 - MAIN BATTERY CHARGER EICAS STATUS MSG. DIVERT TO JFK. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. ACCOMPLISHED CHECKS PER MM ALL CHECKS. REF: OPERATOR CONTROL NR 97ZZZX4170. (X)