N193AN
Registered owner: WILMINGTON TRUST COMPANY TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2020-03-21 | Operator named in NTSB report |
Accident & incident history
Operated by American Airlines (per NTSB report)
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.
103 reports on file, 2003-02-09 – 2026-08-17.
Part: COUPLER — FAULTY (ZONE 300) · airframe 71,685 hrs · 19,293 cycles
ETOPS : RIGHT HF SYSTEM INOPERATIVE. REPLACED RIGHT HF COUPLER PER APPLICABLE AMM.
Part: SENSOR — FAULTY (APU BLEED) · airframe 71,622 hrs · 19,275 cycles
APU BLEED PRESSURE LOW, REPLACED APU FLOW SENSING MODULE IAW AMM
Part: ECU — FAULTY (APU) · airframe 71,622 hrs · 19,275 cycles
APU FAILED TO START TWICE AFTER LANDING. REPLACED APU ECU IAW APPLICABLE AMM.
Part: IGNITER — FAULTY (RT ENGINE) · airframe 71,606 hrs · 19,272 cycles
RIGHT ENGINE IGNITION SYSTEM INOPERATIVE. REPLACED RT ENGINE IGNITER PLUGS IAW AMM
Part: IGNITER — FAULTY (LT ENGINE) · airframe 71,583 hrs · 19,268 cycles
LEFT ENGINE IGNITION SYSTEM INOPERATIVE. REPLACED LT ENGINE IGNITER PLUGS IAW AMM.
Part: SOLENOID VALVE — FAULTED (APU) · airframe 71,460 hrs · 19,234 cycles
APU FAILED TO START DURING LANDING. R & R APU DEOIL SOLENOID VALVE IAW AMM.
Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 70,889 hrs · 19,093 cycles
LEFT ENG LOW OIL PRESS LIGHT INOP. R & R LT ENG LOW PRESSURE SWITCH IAW AMM, OPS CHECKED NORMAL.
Part: EXCITER — FAILED (LT ENGINE) · airframe 70,633 hrs · 19,015 cycles
FLIGHT MGE305, LEFT ENGINE IGNITION SYSTEM 1 INOP. REPLACED SYS 1 EXCITER.
Part: IGNITER — FAILED (LH ENGINE) · airframe 70,606 hrs · 19,008 cycles
FLIGHT MGE410, LEFT ENGINE IGNITION SYSTEM INOP. REPLACED SYS 1 AND 2 IGNITERS.
Part: IGNITER — FAULTED (LT ENG) · airframe 70,325 hrs · 18,930 cycles
FLIGHT MGE301. LEFT ENGINE NO LIGHT OFF. R & R LEFT ENGINE NR 1 IGNITER IAW AMM.
Part: MANIFOLD — LEAKING (LT ENGINE) · airframe 70,221 hrs · 18,902 cycles
FUEL LEAK FOUND AT LEFT ENGINE. REPLACED FUEL NOZZLE MANIFOLD PER AMM.
Part: IGNITER — WORN (RT ENGINE) · airframe 70,197 hrs · 18,894 cycles
RIGHT ENGINE IGNITER PLUGS FOUND OUT OF LIMITS DURING INSPECTION. REPLACED RT IGNITER PLUGS PER AMM.
Part: STARTER — MAKING METAL (RT ENGINE) · airframe 70,197 hrs · 18,894 cycles
CONTAMINATION FOUND ON RT START CHIP DETECTOR DURING SERVICING. REPLACED RT STARTER PER AMM.
Part: CONTROL VALVE — FAULTED (ZONE 100) · airframe 70,117 hrs · 18,873 cycles
FLT: MGE300 . NO INDICATION ON ECS PAGE FOR LEFT PACK TEMP CONTROL VALVE. REPLACED TEMP CONTROL VALVE IAW AMM.
Earlier reports · 2003–2025 · 89 reports
2025
Part: EXCITER — INOPERATIVE (LT ENGINE) · airframe 68,057 hrs · 18,589 cycles
LEFT ENGINE IGNITION SYSTEM 1 INOPERATIVE. REPLACED LEFT ENGINE IGNITION SYSTEM 1 EXCITER.
Part: FIRE LOOP — FAULTED (LT ENGINE) · airframe 68,057 hrs · 18,589 cycles
LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE. REPLACED LEFT ENGINE FIRE LOOP PER AMM
Part: PRESSURE SWITCH — FAULTED (RT ENG A/I) · airframe 68,947 hrs · 18,558 cycles
RIGHT ENGINE ANIT ICE ON DECENT. R & R RT ENG ANTI ICE LOW PRESS SWITCH PER AMM. OPS CHECK OK.
Part: TRANSCEIVER — INOPERATIVE (RT HF COMMS) · airframe 68,893 hrs · 18,545 cycles
RIGHT HF INOPERATIVE. R & R RT HF TRANSCEIVER IAW AMM, OPS CHECK NORMAL.
Part: THRUST REVERSER — INOPERATIVE (RT ENGINE) · airframe 68,893 hrs · 18,545 cycles
RIGHT THRUST REVERSER INOPERATIVE. R & R RT OTBD T/R IAW AMM, OPS CHECK NORMAL.
Part: SWITCH — FAULTY (RT ENGINE) · airframe 68,893 hrs · 18,545 cycles
RIGHT TURB OVHR DET 1 STATUS MSG. R & R RT ENG OVHT DET 1 SWITCH PER AMM, OPS CHECK NORMAL.
Part: TRANSCEIVER — FAULTY (HF COMMS) · airframe 68,893 hrs · 18,545 cycles
RIGHT HF INOPERATIVE. R & R RT HF TRANSCEIVER IAW AMM, OPS CHECK NORMAL.
Part: STARTER — FAILED (APU) · airframe 68,879 hrs · 18,537 cycles
APU STARTER FAILED. R & R APU STARTER PER AMM.
Part: EXCITER — FAULTED (APU) · airframe 68,519 hrs · 18,435 cycles
FLT NO: MGE 402, APU FAULT ON THE GROUND, UNABLE TO START APU. PERFORMED ECU BITE TEST, MINI FLAGS 28 AND 91. ISOLATED ISSUE TO APU EXCITER. MX R/R APU EXCITER, OPS CHECK.
Part: IGNITER — WORN (RT ENGINE) · airframe 68,452 hrs · 18,409 cycles
FLT NT: MGE 410. RT ENG ABORT START QRH PERFORMED. R & R RT ENG #1 AND #2 IGNITER PLUGS PER AMM 74-21-01. OPS TEST OK PER AMM 71-00-00/501.
Part: IGNITION LEAD — INOPERATIVE (LEFT ENG) · airframe 68,139 hrs · 18,333 cycles
FLT NO: N/A, MGE 400, ESI (ETOPS) NR 1 IGN ON LH ENG DID NOT START FROM 2 ATTEMPTS. 3RD ATTEMPT STARTED WITH #2 IGN. R/R LH ENG #1 IGNITER LEAD AND PLUG PER AMM 74-21-01.
Part: COUPLER — FAULTED (ZONE 300) · airframe 67,976 hrs · 18,282 cycles
FLT NO: N/A (MX INSP) ESI - LH HF INOP. R/R LH HF COUPLER PER AMM 23-11-01. OPS CHECK GOOD.
Part: HEAT EXCHANGER — LEAKING (LT IDG) · airframe 67,957 hrs · 18,269 cycles
FLT NO: N/A (MX INSP). ESI - LEFT ENG IDG AIR/OIL HEAT EXCHANGER LEAKING. R/R LH ENG IDG AIR/OIL HEAT EXCHANGER. NO LEAKS NOTED.
Part: IGNITION LEAD — WORN (LT ENGINE) · airframe 67,957 hrs · 18,269 cycles
FLT NO: N/A (MX INSP) ESI - LEFT ENG SLOW TO START. R/R LH ENG #2 IGNITION LEAD. OPS CHECK GOOD.
Part: FIRE LOOP — FAULTED (ZONE 400) · airframe 67,957 hrs · 18,269 cycles
FLT NO: N/A (MX INSP). ESI - LEFT ENG FIRE LOOP 1 STATUS MESSAGE. R/R LH FIRE LOOP 1 PER AMM 26-11-01. OPS CHECK GOOD.
Part: GCU — FAULTY (RT ENGINE) · airframe 67,893 hrs · 18,246 cycles
FLT NO: N/A (MX INSP). ESI - WHEN GEN TRANFER DURING ENGINE START LOWER EICAS BLANKS OUT ALONG WITH RH IRU AND FMS. R/R RH GCU. OPS CHECK GOOD.
Part: FIRE LOOP — FAULTED (ZONE 400) · airframe 67,893 hrs · 18,246 cycles
FLT NO: N/A (MX INSP). ESI - LEFT ENG FIRE LOOP 1 STATUS MESSAGE. R/R LH FIRE LOOP 1 PER AMM26-11-01. OPS CHECK GOOD.
Part: ACM — FAULTED (RIGHT) · airframe 67,891 hrs · 18,245 cycles
FLT NO: N/A (MX INSP). ESI - RH PACK TEMP. R/R RH ACM. OPS CHECK NORMAL.
Part: ACM — FAULTED (LEFT) · airframe 67,891 hrs · 18,245 cycles
FLT NO: N/A (MX INSP). ESI - LH PACK AIR IS HOT ON THE GROUND. R/R LH ACM PER AMM 21-51-03/401. OPS CHECK NORMAL.
2020
Part: DOOR — OUT OF RIG (L2) · airframe 64,226 hrs · 17,044 cycles
AIRCRAFT NOT GROUNDED: L2 ENTRY DOOR UPPER FWD STOP HITS FRAME AND PULLS OUT SEAL WHEN CLOSING. ACCOMPLISHED RIG OF L2 DOOR IAW AMM 52-11-04-822-056.
Part: LIGHT — UNSECURE (CABIN) · airframe 64,080 hrs · 16,996 cycles
AIRCRAFT WAS NOT GROUNDED: 1R SLIDE LIGHT WAS MISSING. MAINTENANCE RELAMPED AND SECURE 1R SLIDE LIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-66-00.
2019
Part: BRACKET — BROKEN (THROTTLE CONTROL) · airframe 63,351 hrs · 16,770 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT THROTTLE STICKS AT MID POSITION. NEED TO FORCE IT PAST MID POSITION TO SET THRUST. MAINTENANCE FOUND RIGHT ENGINE THROTTLE CONTROL BOX HAS BROKEN SHIELD, BLENDED EDGE OF BRACKET, REINSTALLED RIVETS AND VERIFIED THROTTLE OPERATION IAW EA 300983.
Part: POWER LEVER — BINDING (RIGHT) · airframe 63,334 hrs · 16,766 cycles
AIRCRAFT NOT GROUNDED: RIGHT TRHUST LEVER WOULD NOT MOVE MORE THAN AN INCH FOR TAKEOFF. INSPECTED RT THRUST LEVER FOR ANY JAM AND NONE FOUND. MOVED THRUST LEVER FWD AND BACK AND MOVEMENT IS SMOOTH IAW AMM 76-11-00-001 AND FIM76-11-00.
Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 62,444 hrs · 16,503 cycles
AIRCRAFT NOT GROUNDED: AFT R/H O/B FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT R/H O/B FLIGHT ATTENDANT FLASHLIGHT BATTERY IN REFERENCE WITH A.M.M 25-64-00, OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,117 hrs · 16,410 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT JUMP SEAT EMERGENGY FLASHLIGHT INOPERABLE. MAINTENANCE REPLACED FLASH LIGHT BATTERY PER AMM 25-60-00.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 61,247 hrs · 16,188 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND L4 DOOR EXTERNAL SLIDE LIGHT INOP. RELAMPED THE L4 DOOR SLIDE IAW AMM 33-51-06. OPS CHECK GOOD.
Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 61,247 hrs · 16,188 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND SEAT MOUNTED EMERGENCY LIGHTS 27D THRU 33D DIM. REMOVED AND REPLACED BATTERY PACK AND CHARGER M10801 IAW AMM 33-51-07. OPS CHECK GOOD. SEE SDR # AALA201904189028.
Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,247 hrs · 16,188 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND SEAT MOUNTED EMERGENCY LIGHTS 27D THRU 33D DIM. REMOVED AND REPLACED BATTERY PACK AND CHARGER M10801 IAW AMM 33-51-07. OPS CHECK GOOD. SEE SDR # AALA201904189005.
Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 61,245 hrs · 16,187 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS 27D THROUGH 33D WERE VERY DIM. MAINTENANCE REPLACED CHARGER PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: LIGHT — MISSING (R1 DOOR) · airframe 60,767 hrs · 16,058 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR SLIDE LIGHT WAS MISSING. MAINTENANCE REPLACED SLIDE LIGHT/LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-60-00.
2018
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,359 hrs · 15,667 cycles
L4 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06. OPS OK.
2017
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,735 hrs · 15,220 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY AISLE LIGHT ABOVE 20ABC IS INOPERATIVE. RELAMPED EMERGENCY AISLE LIGHT PER AMM 33-51-05. OPERATIONAL CHECK NORMAL.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 57,735 hrs · 15,220 cycles
AIRCRAFT WAS NOT GROUNDED. RIGHT OVER WING EXIT SIGN HAS BULBS OUT. RELAMPED RIGHT OVER WING EXIT SIGN PER AMM 33-51-06.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,730 hrs · 15,218 cycles
AIRCRAFT WAS NOT GROUNDED. LEFT OVERWING EXIT SIGN HAS BULBS OUT. RELAMPED OVERWING EXIT SIGN PER AMM 33-51-01. OPERATIONAL CHECK OK.
Part: WIRE — BROKEN (CABIN) · airframe 56,963 hrs · 15,020 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTS AT SEATS 16DEF THROUGH 25DEF ARE INOPERATIVE. REPAIRED BROKEN WIRE AT TERMINAL FOR SEAT ROW 19DEF PER SWPM 20-10-13. OPERATIONAL CHECK GOOD.
Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,396 hrs · 14,875 cycles
EMERGENCY LIGHTS UNARMED ANNUNCIATOR IN THE COCKPIT OVERHEAD PANEL IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL PANEL IAW AMM 33-51-08. OPERATIONAL CHECKED GOOD.
Part: SEAT — OUT OF ADJUST (17B) · airframe 56,409 hrs · 14,878 cycles
SEAT 17B AT THE EMERGENCY EXIT ROW DOES NOT RECLINE AT THE CORRECT ANGLE. ADJUSTED RECLINE IAW AMM 25-25-03. OPERATIONAL CHECKED GOOD.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 56,396 hrs · 14,875 cycles
SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT SEAT 17DEF IS INOPERATIVE. SECURED THE CONNECTOR BETWEEN THE WALL AND THE SEAT HARNESS ATTACH POINT. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.
Part: LIGHT — INOPERATIVE (SEAT 3B) · airframe 55,837 hrs · 14,723 cycles
EMERGENCY EXIT LIGHT OVER SEAT 3B IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-05. OPERATIONAL CHECKED GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,837 hrs · 14,723 cycles
EXTERIOR EMERGENCY EXIT LIGHT AT L2 DOOR IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-06. OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (SEAT 19DEF) · airframe 55,837 hrs · 14,723 cycles
SEAT MOUNTED EMERGENCY LIGHT AT SEAT 19 DEF IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 55,346 hrs · 14,587 cycles
R1 DOOR SLIDE LIGHT DOES NOT ILLUMINATE. REMOVED SLIDE BUSTLE AND FOUND LACING HANGING DOWN. SECURED THE SLIDE LIGHT. OPERATIONAL CHECKED GOOD.
Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 55,311 hrs · 14,576 cycles
R1 DOOR SLIDE LANYARD PROTRUDING FROM SLIDE COVER. SECURED THE LANYARD IAW AMM 25-66-00. OPS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,971 hrs · 14,481 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS IN FIRST CLASS ARE DIM. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.
2016
Part: SIGN — INOPERATIVE (CABIN) · airframe 54,803 hrs · 14,426 cycles
AIRCRAFT WAS GROUNDED. AFT GALLEY EXIT SIGN INOPERATIVE DUE TO QUICK DISCONNECT LOOSE IN BETWEEN GALLEY AND SIDE WALL. REMOVED AND REPLACED EXIT SIGN ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,714 hrs · 14,385 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTING IS VERY DIM ON SEATS 26D THROUGH 36D. REMOVED AND REPLACED AFT POWER SUPPLY BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.
Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 54,547 hrs · 14,307 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH RECEIVED A LEFT HYDRAULIC QUANTITY EICAS MESSAGE ACCOMPANIED BY ILLUMINATION OF THE LEFT RESERVOIR ANNUNCIATOR. MAINTENANCE FOUND THE LEFT RUDDER AND ELEVATOR HYDRAULIC SHUTOFF VALVE O RING LEAKING. REMOVED AND REPLACED O RING IAW AMM 27-23-01. LEAK AND OPERATIONAL CHECKS NORMAL.
Part: DOOR FRAME — CRACKED (BS 429) · airframe 54,544 hrs · 14,305 cycles
LAVATORY SERVICE PANEL SURROUND STRUCTURE AT APPROXIMATELY BS 429 IS CRACKED. REPAIRED THE STRUCTURE IAW SRM 51-70-11-0G.
Part: BATTERY PACK — WEAK (CABIN) · airframe 53,489 hrs · 13,869 cycles
AIRCRAFT WAS NOT GNDED. EMER PATH LIGHTS BETWEEN SEATS 16 DEF & 25 DEF ARE VERY DIM. R & R BATTERY PACK & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07 & 33-51-00. SYS CHECKED NORMAL.
2015
Part: MODULE — INOPERATIVE (CABIN) · airframe 52,487 hrs · 13,475 cycles
EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE, FROM SEATS 16DEF TO 25DEF. REPLACED M10953 MODULE & BATTERY PACK IAW MM 33-51-11. OPERATIONALLY CHECKED GOOD. THE ACFT WAS NOT GNDED.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,511 hrs · 12,907 cycles
CORROSION ON FLOOR IN AFT GALLEY AREA BETWEEN FS 1711 & 1715, BETWEEN RBL 17 & RBL 33. REPAIRED IAW SRM 53-60-51 & EA 250975A.
Part: STRAP — CORRODED (APU BAY) · corrosion level 2 · airframe 50,511 hrs · 12,907 cycles
APU AIR INTAKE EXTERNAL SKIN CORRODED. R & R WITH NEW STRAP IAW AMM 51-10-02. OPEN, AWAITING CORROSION LEVEL DETERMINATION.
Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 50,228 hrs · 12,840 cycles
AIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. LT BLEED OFF LIGHT ILLUMINATED CLIMBING THROUGH 10,000 FEET. COMPLETED QRH SINGLE PACK. REPLACED NR 1 ENG PRSOV IAW AMM 36-11-09.
Part: ARM — OUT OF ADJUST (R1 DOOR) · airframe 50,106 hrs · 12,809 cycles
R1 DOOR REPORTED HARD TO OPEN, HANGS UP AT MIDWAY OPEN. FOUND GUIDE ARM ROD LENGTH TO BE INCORRECT. ADJUSTED LENGTH IAW AMM 52-11-04-002-001. SYS CHECKED NORMAL.
Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 50,072 hrs · 12,799 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. PASSING 6000 FEET ON CLIMB OUT, LT ENG BLEED & LT PACK OFF EICAS MSGS WITH LT PACK OFF LIGHT ALSO ON. REPLACED LT ENG 450 DEGREE TEMP SENSOR IAW AMM 36-11-13. REPLACED REVERSE FLOW CHECK CONTROLLER IAW AMM 36-11-18. SYS CHECKED NORMAL. ALSO REFERENCE SDR AALA20150312012.
Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 50,072 hrs · 12,799 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. PASSING 6000 FEET ON CLIMB OUT, LT ENG BLEED & LT PACK OFF EICAS MSGS WITH LT PACK OFF LIGHT ALSO ON. REPLACED LT ENG 450 DEGREE TEMP SENSOR IAW AMM 36-11-13. REPLACED REVERSE FLOW CHECK CONTROLLER IAW AMM 36-11-18. SYS CHECKED NORMAL. ALSO REFERENCE SDR AALA20150313003.
2014
Part: SHUTOFF VALVE — FAILED (LEFT) · airframe 49,399 hrs · 12,639 cycles
DURING CLIMB OUT, LT BLEED TRIP ACCOMPANIED WITH LT PACK OFF LIGHT ILLUMINATED. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND LANDED UNEVENTFULLY. R & R THE LEFT PRSOV IAW AMM. ACCOMPLISHED HIGH POWER RUNS. OPS CHECKED GOOD.
Part: REHEATER — INOPERATIVE (AC BAY) · airframe 48,046 hrs · 12,322 cycles
LEFT PACK OFF & PACK TEMP LIGHTS ILLUMINATED FOLLOWED BY BLEED OFF LIGHT. PRIOR TO PACK TRIP, THE PNEUMATIC SYS COULD BE HEARD CYCLING. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT PACK REHEATER & CONDENSER MPN 1942765. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: SKIN PANEL — DAMAGED (LT HORIZ STAB) · airframe 46,654 hrs · 11,981 cycles
HAIL DAMAGE TO LT HORIZONTAL STABILIZER OTBD UPPER SKIN PANEL. REPLACED LT UPPER SKIN ON STABILIZER.
Part: SKIN PANEL — DAMAGED (RT HORIZ STAB) · airframe 46,654 hrs · 11,981 cycles
HAIL DAMAGE TO RT HORIZONTAL STABILIZER OTBD UPPER SKIN PANEL. REPLACED RT UPPER SKIN ON STABILIZER.
Part: SKIN PANEL — DAMAGED (RT HORIZ STAB) · airframe 46,654 hrs · 11,981 cycles
HAIL DAMAGE TO RT HORIZONTAL STABILIZER INBD UPPER SKIN PANEL. REPLACED RT UPPER SKIN ON STABILIZER.
Part: SKIN PANEL — DAMAGED (LT HORIZ STAB) · airframe 46,654 hrs · 11,981 cycles
HAIL DAMAGE TO LT HORIZONTAL STABILIZER INBD UPPER SKIN PANEL. REPLACED LT UPPER SKIN ON STABILIZER.
2013
Part: SENSOR — FAULTY (TE FLAP) · airframe 45,095 hrs · 11,589 cycles
OGG CREW REPORTED FLAP ASYMMETRY DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED OGG WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT INBD TE SKEW SENSORS 3 & 4. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.
2012
Part: WEDGE — DAMAGED (TE FLAP) · airframe 40,614 hrs · 10,490 cycles
OUTBOARD TRAILING EDGE WEDGE DAMAGED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,614 hrs · 10,490 cycles
DELAMINATED SKIN ALONG FORWARD EDGE OF AFT PANEL BETWEEN STATIONS 170 AND 194. REMOVED DAMAGED SKIN AND HOT BONDED NEW OVERLAY IN REPAIR AREA PER SRM 51-70-07-0G.
Part: PANEL — DAMAGED (TE FLAP) · airframe 40,614 hrs · 10,490 cycles
UPPER INBOARD PANEL DAMAGED APPROXIMATELY 112.5 INCHES FROM INBOARD END OF CENTER PANEL ASSEMBLY. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,046 hrs · 10,349 cycles
RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: PANEL — DENTED (LT HORIZ STAB) · airframe 39,759 hrs · 10,264 cycles
HAIL DAMAGE ON LEFT HORIZONTAL STABILIZER INBOARD PANEL, JUST FORWARD OF TORQUE BOX. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023482.
Part: PANEL — DENTED (LT HORIZ STAB) · airframe 39,759 hrs · 10,264 cycles
HAIL DENTS TO LEFT HORIZONTAL STABILIZER OUTBOARD PANEL, JUST FORWARD OF TORQUE BOX. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023481.
Part: SKIN — DENTED (RT HORIZ STAB) · airframe 39,759 hrs · 10,264 cycles
HAIL DAMAGE ON RIGHT HORIZONTAL STABILIZER INBOARD TORQUE BOX TOP SKIN. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023418.
Part: PANEL — DENTED (RT HORIZ STAB) · airframe 39,759 hrs · 10,264 cycles
HAIL DAMAGE TO RIGHT STABILIZER OUTBOARD PANEL, JUST FORWARD FOR TORQUE BOX UPPER SKIN. ACCOMPLISHED BONDED REPAIR PER EA B757-55-023416.
Part: SKIN — DENTED (FUSELAGE) · airframe 39,759 hrs · 10,264 cycles
FOUR DENTS LOCATED BETWEEN STATIONS 610 TO 630 JUST ABOVE STRINGER 16 RIGHT. INSTALLED DOUBLER PER EA B757-53-023316.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,759 hrs · 10,264 cycles
CORROSION ON TOP OF FLOORBEAM STATION 300.5 AT RIGHT BUTTLINE 36.2. REMOVED DAMAGED SECTION OF FLOOR BEAM AND INSTALLED NEW SECTION OF FLOORBEAM PER AARD 51-00-05-1.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,759 hrs · 10,264 cycles
AFT CABIN FLOOR DECK CORRODED, AFT DECK FLOOR PLATE REPLACED PER BOEING DRAWINGS EBE-2089-3, 146N5300, 146N2301 AND AARD 51-00-05-1 ALONG WITH EA B757-53-023128.
Part: PLATE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 39,759 hrs · 10,264 cycles
CORROSION ON TOP SURFACE OF LEFT PIVOT HINGE STIFFENER PLATE. INSTALLED FASTENERS AT LEFT PIVOT HINGE PER PER EA B757-55-023567 AND SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,759 hrs · 10,264 cycles
CORROSION ON TOP OF FLOORBEAM AT STATION 300.5 RIGHT BUTTLINE 21. REMOVED DAMAGED SECTION AND INSTALLED NEW SERVICEABLE SECTION OF FLOORBEAM PER AARD 51-00-05-1.
2011
Part: UNKNOWN — SMOKE (COCKPIT) · airframe 38,773 hrs · 9,972 cycles
LAX - CREW REPORTED STRONG BURNING SMELL OF RUBBER / ONION IN FLIGHT DECK FLOWING INTO THE FIRST CLASS GALLEY AND CAUSING SOME VISIBLE SMOKE IN GALLEY. THE FLIGHT ATTENDANTS TURNED OFF ALL OVENS AND PROBLEM NOT SOLVED. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT CURRENTLY UNDERGOING MAINTENANCE.
Part: LENS — MISSING (CABIN) · airframe 38,096 hrs · 9,815 cycles
RIGHT OVERWING EMERGENCY EXIT SIGN MISSING LENS COVER WITH EXIT MARKINGS. REPLACED LENS FOR RIGHT OVERWING EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: CONTROL VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 37,458 hrs · 9,658 cycles
LAX - CREW REPORTED AFTER TAKEOFF LEFT ENGINE BLEED OFF ANNUNCIATED WITH APU BLEED AIR ON MEL. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE REVERSE FLOW CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,817 hrs · 9,509 cycles
EXIT LIGHT FORWARD OF LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EXIT LIGHT FORWARD OF LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.
2009
Part: FAN — FAILED (CABIN) · airframe 30,644 hrs · 8,081 cycles
ELECTRICAL ODOR REPORTED IN CABIN NEAR SEAT ROW 14. EMERGENCY DECLARED. UNEVENTFUL LANDING, NOT OVERWEIGHT. FOUND RIGHT RECIRCULATION FAN FAILED. PLACARD RECIRCULATION FAN AND REPLACED RIGHT RECIRCULATION FAN AT LAX ON 24 NOV.
2008
Part: GENERATOR — FAILED (NR 1) · airframe 27,304 hrs
MIA INFLIGHT - NR 1 GENERATOR DRIVE LIGHT ILLUMINATED FOLLOWED BY LARGE JOLT IN THE FLIGHT CONTROLS. THE LT GENERATOR CONTROL LIGHT ILLUMINATED AND THE LEFT BUS WAS THEN POWERED BY THE RIGHT SIDE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,989 hrs
DFW - EMERGENCY LIGHT AT LEFT AFT EXTERIOR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT EXTERIOR SLIDE. SYTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,550 hrs
SFO - EMERGENCY LIGHT IDENTIFIER AT SEAT 15D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IDENTIFIER AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — BROKEN (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 14D HAS BROKEN SHROUD. REPLACED THE SHROUD FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — BROKEN (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT 6E HAS BROKEN SHROUD. REPLACED THE SHROUD FOR THE EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — BROKEN (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 11D HAS BROKEN SHROUD. REPLACED THE SHROUD FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: MODULE — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15 INOPERATIVE. REMOVED AND REPLACED MODULE AND BATTERY FOR EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: WIRE — DAMAGED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED LIGHT AT SEAT 9D INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRE AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)