N114NN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2019-04-10 | 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.
31 reports on file, 2014-04-13 – 2019-03-13.
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 18,078 hrs · 3,711 cycles
CABIN FLOOR PANEL 241BF WAS SOFT. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLOOR PANEL IAW EA 291650.
Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 17,654 hrs · 3,627 cycles
FORWARD LAVATORY SMOKE AND FIRE WARNING SOUNDED 40 MINS INTO FLIGHT, FOR TWENTY SECOND. THEN WENT AWAY WITH NO EVIDENCE. ACCOMPLISHED A SMOKE DETECTION SYSTEM RESET. SYSTEM GROUND CHECKED NORMAL IAW MM 26-27-00.
Earlier reports · 2014–2018 · 29 reports
2018
Part: OVEN — OVERHEATED (GALLEY) · airframe 16,295 hrs · 3,336 cycles
NR 3 OVEN IN BUSINESS CLASS GALLEY OVERHEATED IN FLIGHT. CIRCUIT BREAKER TRIPPED. REPLACED THE OVEN, OPS CHECKED IAW AMM 25-35-19.
Part: GIRT BAR — FOD (L1 DOOR) · airframe 15,590 hrs · 3,172 cycles
L1 DOOR GIRT BAR AREA HAS TRASH. REMOVED TRASH FROM L1 DOOR GIRT BAR AREA.
Part: LENS — DETACHED (SLIDE INDICATOR) · airframe 14,848 hrs · 3,008 cycles
PLASTIC LENS THAT COVERS THE SLIDE PRESSURE INDICATOR ON OVERHEAD PANEL ABOVE FLIGHT ATTENDANT JUMPSEAT AT THE L2 DOOR FELL OFF. THE LENS WAS REINSTALLED IAW MM 25-61-00. OK FOR SERVICE.
2017
Part: DOOR SEAL — DEFORMED (FWD CARGO DOOR) · airframe 13,279 hrs · 2,688 cycles
DURING CRUISE AT FL 235, CABIN ALTITUDE KEPT CLIMBING TO 9550 FEET INLET, EXTRACT AND OUTFLOW VALVES ALL FULLY CLOSED. CABIN DIFFERENTIAL WAS 4.2 PSI. UNABLE TO MAINTANIN CABIN PRESSURIZATION UNTIL DESCENDING. DECLARED EMERGENCY AND LANDED WITHOUT ISSUE. MAINTENANCE FOUND FORWARD CARGO DOOR SEAL AT TOP LEFT CORNER DEFORMED AND NOT SEALING PROPERLY. REPLACED FORWARD CARGO DOOR SEAL IAW MM 52-31-18. AIRCRAFT WAS GROUNDED.
Part: HANDLE — BROKEN (R2 DOOR) · airframe 13,278 hrs · 2,687 cycles
FOUND A BROKEN SLIDE ARM HANDLE ON THE R2 DOOR. REPLACED ARM - DISARM SLIDE HANDLE IAW AMM 52-22-22. MAINTENANCE PERFORMED SUCCESSFUL OPS CHECK. AIRCRAFT WAS GROUNDED
Part: LIGHT — UNSECURE (SEAT 11C) · airframe 13,162 hrs · 2,663 cycles
EMERGENCY EXIT LIGHT AT SEAT 11C LOOSE.. SECURED THE EMERGENCY LIGHT ASSY TO THE SEAT, OPS CHECKED OK IAW AMM.
Part: UNKNOWN — ODOR (CABIN) · airframe 12,029 hrs · 2,432 cycles
AIRCRAFT WAS NOT GROUNDED. REQUEST FOR MAINTENANCE TO CHECK THERMAL BLANKETS IN FORWARD CARGO. FLIGHT ATTENDANTS COMPLAINED OF HOT FLOOR AND WIRED SMELL NEAR 1-L JUMPSEAT. MAINTENANCE TO TROUBLESHOOT FLOOR HEATING SYSTEM PER AMM 25-27-00-740-001-A. ACCOMPLISHED TSM 25-27-00, NO FAULTS NOTED. REPLACED LEFT HAND FLOOR HEATER CONTROL UNIT 60DS (PRECAUTIONARY) PER MM 25-27-34. L1 DOOR FLOOR HEATERS BITE TEST NORMAL.
Part: SLIDE — LOOSE (L4 DOOR) · airframe 11,925 hrs · 2,412 cycles
SLIDE COVER AT THE L4 DOOR FOUND LOOSE. MAINTENANCE FOUND SLIDE STRAPS TOO LOOSE TO SECURE. REPLACED L4 DOOR SLIDE IAW AMM 25-62-44. AIRCRAFT WAS GROUNDED.
Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 11,872 hrs · 2,402 cycles
CIDS 1 EMERGENCY POWER SUPPLY UNIT SYSTEM TEST (12WL) FAULTED. REPLACED THE BATTERY IAW MM 33-51-38 AND MM 33-51-00.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 11,525 hrs · 2,324 cycles
LEFT AFT FLIGHT ATTENDANT FLASHLIGHT IS INOPERATIVE. REPLACED THE BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 11,525 hrs · 2,324 cycles
LEFT MID CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 11,280 hrs · 2,278 cycles
DELAMINATION ON FORWARD CARGO FLOOR PANEL 131HF. REPLACED CARGO FLOOR PANEL.
Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 11,280 hrs · 2,278 cycles
DELAMINATION ON FORWARD CARGO FLOOR PANEL 131EF. REPLACED THE CARGO FLOOR PANEL.
Part: FILTER — CLOGGED (ENGINE OIL) · airframe 11,091 hrs · 2,234 cycles
DURING THE DESCENT ENF NR 1 AND 2, 10-12 HIGHER THAN NR 2 ENGINE. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL/OIL COOLER FILTER ELEMENT IAW AMM 73-12-42. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 71-00-00.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 10,980 hrs · 2,208 cycles
ON CIDS, AFT LEFT EMERGENCY POWER SUPPLY BATTERY 13WL FAILED SYSTEM TEST. REPLACED THE BATTERY PACK IAW AMM 33-51-38.
Part: BATTERY — DISCHARGED (CABIN) · airframe 10,144 hrs · 2,039 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT 14WL MIDDLE RIGHT FAILED TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 10,144 hrs · 2,039 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT 15WL MIDDLE LEFT FAILED TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 10,056 hrs · 2,021 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY DECLARED. BRAKE SYSTEM 2 FAULT INDICATION ONE HOUR INTO FLIGHT. LANDING UNEVENTFUL. ACCOMPLISHED BRAKING AND STEERING CONTROL UNIT RESET IAW AMM 32-46-00. OPERATIONAL CHECK GOOD.
2016
Part: OVEN — FAULTY (GALLEY) · airframe 9,634 hrs · 1,932 cycles
AIRCRAFT NOT GROUNDED. METALLIC BURNING ODOR EMITTED FROM NR 4 OVEN IN MID GALLEY WHEN TURNED ON HIGH. REMOVED AND REPLACED OVEN IAW AMM 25-35-19. OPERATIONAL CHECK GOOD.
Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 9,573 hrs · 1,920 cycles
EMERGENCY LIGHTING EXIT MARKER AT L1 DOOR IS BROKEN. REMOVED AND REPLACED EXIT MARKER IAW AMM 33-51-17.
Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 9,573 hrs · 1,920 cycles
EMERGENCY LIGHTING EXIT MARKER AT R1 DOOR IS BROKEN. REMOVED AND REPLACED EXIT MARKER IAW AMM 33-51-17.
Part: LIGHT — BROKEN (SEAT 11C) · airframe 8,974 hrs · 1,793 cycles
AISLE MOUNTED EMERGENCY LIGHT AT SEAT ROW 11C BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW MM 33-51-19. THE AIRCRAFT WAS GROUNDED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,623 hrs · 1,720 cycles
DURING EMERGENCY LIGHTING TEST, RECEIVED POWER SUPPLY FAULT CODE 13WL. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY AT 13WL.
Part: POWER CABLE — DISCONNECTED (CABIN) · airframe 6,763 hrs · 1,304 cycles
OVERHEAD AISLE CEILING EMER LIGHT INOPERATIVE. LOCATED JUST FWD OF THE R2 DOOR. APPLIED MEL 33-16D. THE ACFT WAS NOT GNDED. RE-CONNECTED POWER CABLES FOR EMER CEILING AISLE LIGHT AT MID-CLOSET IAW AMM 33-51-11. OPERATIONS CHECKED GOOD. REMOVED PLACARD.
2015
Part: DIAPHRAGM — PUNCTURED (L4 DOOR) · airframe 5,781 hrs · 1,102 cycles
L4 DOOR OPENED FROM INSIDE WHILE ARMED. SLIDE PARTIALLY DEPLOYED. R & R THE L4 DOOR DAMPER CYLINDER DIAPHRAGM IAW AMM 52-22-00, LEAK CHECKED GOOD. R & R L4 DOOR ESCAPE SLIDE PACK IAW AMM 25-64-44, OPERATIONAL CHECKED GOOD. SEE ALSO AALA20151113004.
Part: SLIDE — PARTIAL DEPLOY (L4 DOOR) · airframe 5,781 hrs · 1,102 cycles
L4 DOOR OPENED FROM INSIDE WHILE ARMED. SLIDE PARTIALLY DEPLOYED. R & R THE L4 DOOR DAMPER CYLINDER DIAPHRAGM IAW AMM 52-22-00, LEAK CHECKED GOOD. R & R L4 DOOR ESCAPE SLIDE PACK IAW AMM 25-64-44. OPERATIONAL CHECKED GOOD. SEE ALSO AALA20151113008.
Part: SLIDE — UNWANTED DEPLOY (R3 DOOR) · airframe 4,768 hrs · 909 cycles
R3 SLIDE DEPLOYED WHILE DOOR REPORTEDLY DISARMED. FOUND SLIDE RELEASE MECHANISM TO BE PARTIALLY TRIPPED. R & R SLIDE & INFLATION RESERVOIR IAW AMM 25-62-47 & AMM 25-62-49.
2014
Part: MECHANISM — BROKEN (ZONE 800) · airframe 18 hrs · 5 cycles
THE MECHANIC TOUCHED THE LEVER ON THE DOOR FRAME PART OF THE SLIDE ACTIVATION SET UP & THIS CAUSED THE LT NR 3 SLIDE TO DEPLOY. REPLACED BROKEN DOOR SLIDE DEPLOY MECHANISM & SLIDE.
Part: LEVER — BROKEN (ESCAPE SLIDE) · airframe 4 hrs · 2 cycles
L3 SLIDE DEPLOYED. DOOR SLIDE WAS DISARMED WHEN DOOR WAS OPENED. DURING OPENING THE DOOR, ESCAPE LEVER RELEASE MECHANISM, BROKE AWAY AT THE END OF THE LEVER WHERE A RIVET-STOP IS ASSEMBLED THROUGH THE HOLE IN THE LEVER. AS THE TECH WAS EXAMINING WHAT HAD HAPPENED HE ROTATED THE LEVER AND THE SLIDE DEPLOYED.