N104NN
Registered owner: UMB BANK NA TRUSTEE, UT (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 2016-06-12 | 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.
97 reports on file, 2015-07-23 – 2026-07-06.
Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 12WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERARATIONAL CHECK WITH NO ISSUES NOTED.
Part: CLAMP — MISINSTALLED (ZONE 200) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CAPTAINS SLIDING WINDOW GUST LOCK RELEASE LEVER DOESNT RESET CORRECTLY. MAINTENNACE DETERMINED THAT THE LOCK RELEASE LEVER WAS FUNCTIONING CORRECTLY BUT DID FIND CLAMP IN SIDEWALL PANEL 211GW ON CAPTAIN SLIDE WINDOW WAS NOT INSTALLED CORRECTLY. MAINTENANCE RE-INSTALLED THE CLAMP PER AMM 25-13-41.
Part: WEB — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR WEB AT FR 20 AND S23R. REPLACED WEB PER SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK BETWEEN FR 20 AND FR 21 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 65 AND +Y765. REPLACED BEAM PER SRM 51-72-11.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK BETWEEN FR 21 AND FR 23 AT -Y765. REPLACED SEAT TRACK PER SRM 51-42-11.
Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 ESCAPE SLIDE PRESSURE LOW. REPLACED SLIDE ASSEMBLY PER JOB CARD 26C83252008.
Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE ESCAPE SLIDE INFLATION RESERVOIR ON PASSENGER CREW DOOR 832. REPLACED SLIDE ASSEMBLY PER JOB CARD 26C83252008.
Part: HINGE FITTING — EXCESS PLAY (ZONE 800) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.
Part: HINGE FITTING — EXCESS PLAY (ZONE 800) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.
Part: HINGE FITTING — EXCESS PLAY (ZONE 100) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.
Part: HINGE FITTING — EXCESS PLAY (ZONE 800) · airframe 43,356 hrs · 8,721 cycles
AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.
Part: LIGHT — NO TEST (ZONE 200) · airframe 43,185 hrs · 8,688 cycles
AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY LIGHT BY SEAT ROW 6 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT PER AMM 33-51-11.
Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 43,144 hrs · 8,680 cycles
AIRCRAFT WAS NOT GROUNDED: AIRCRAFT NEEDS A SPARE FLIGHT ATTENDANT FLASHLIGHT. FLIGHT ATTENDANT MISSING PERSONAL FLASHLIGHT. FLIGHT ATTENDANT WAS SUPPLIED A PERSONAL FLASHLIGHT FROM INFLIGHT.
Part: BATTERY — NO TEST (ZONE 200) · airframe 42,607 hrs · 8,580 cycles
AIRCRAFT WAS GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT14WL DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED BATTERY PER TASK CARD 26C00033004 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FAULTS NOTED.
Part: BATTERY — NO TEST (ZONE 200) · airframe 42,607 hrs · 8,580 cycles
AIRCRAFT WAS GROUNDED: BATTERY FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT10WL DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED BATTERY PER TASK CARD 26C00033004 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FAULTS NOTED.
Part: CONTROL SERVO — FAULTED (ZONE 500) · airframe 42,116 hrs · 8,488 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETUNED TO JFK DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF, AFTER FLAP RETRACTION, THEY RECEIVED THE FOLLOWING ECAM MESSAGES: F/CTL L AIL FAULT, AND F/CTL AIL SERVO FAULT.ON SD PAGE, LEFT AILERON APPEARS INOPERATIVE, RIGHT AILERON WITH ONLY GREEN HYDRAULICS, AND FOR A SIGNIFICANT TIME RIGHT SPOILERS INDICATED RAISED/EXTENDED. THE AIRCRAFT LANDED SAFELY AT JFK WITHOUT FURTHER INCIDENT. MAINTENANCE LEFT WING AILERON SERVO CONTROL VALVE 33CEB AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 27-14-51.
Earlier reports · 2015–2025 · 77 reports
2025
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 41,577 hrs · 8,386 cycles
AIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 41,577 hrs · 8,386 cycles
AIRCRAFT IN BASE MAINTENANCE: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 40,913 hrs · 8,259 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 40,913 hrs · 8,259 cycles
AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 40,798 hrs · 8,237 cycles
AIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY NITROGEN ACCUMULATOR BELOW LIMITS. MAINTENANCE ACCOMPLISHED SERVICING IAW AMM 52-22-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 39,631 hrs · 8,009 cycles
AIRCRAFT WAS NOT GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 39,631 hrs · 8,009 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
2024
Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 37,479 hrs · 7,601 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY CEILING LIGHT INOPERATIVE JUST BEFORE L2/R2 DOOR IS INOPERATIVE. FOUND CONNECTOR OF LIGHT DISCONNECTED. RESECURED CONNECTOR PER AMM 33-51-00.
Part: BOTTLE — LOW PRESSURE (EMERGENCY OPS) · airframe 36,945 hrs · 7,498 cycles
AIRCRAFT WAS NOT GROUNDED: DOOR 3R EMERGENCY CYLINDER PRESSURE BELOW PS LIMITS. SERVICED EMERGENCY EXIT DOOR DAMPER.
Part: BOTTLE — LOW PRESSURE (EMERGENCY OPS) · airframe 36,945 hrs · 7,498 cycles
AIRCRAFT WAS NOT GROUNDED: DOOR L2 EMERGENCY CYLINDER PRESSURE BELOW PS LIMITS. SERVICED EMERGENCY EXIT DOOR DAMPER.
Part: BOTTLE — LOW PRESSURE (EMERGENCY OPS) · airframe 36,945 hrs · 7,498 cycles
AIRCRAFT WAS NOT GROUNDED: DOOR 1R EMERGENCY CYLINDER PRESSURE BELOW PS LIMITS. SERVICED EMERGENCY EXIT DOOR DAMPER.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 36,414 hrs · 7,396 cycles
AIRCRAFT WAS NOT GROUNDED: L4 DOOR FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY PER AMM 25-65-00.
2022
Part: BEARING — WORN (H/STAB HINGE) · airframe 30,173 hrs · 6,202 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 3 ELEVATOR HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.
Part: HINGE FITTING — WORN (HORIZONTAL STAB) · airframe 30,173 hrs · 6,202 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 6 ELEVATOR HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.
Part: BEARING — WORN (H/STAB HINGE) · airframe 30,173 hrs · 6,202 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 4 ELEVATOR HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.
Part: HINGE FITTING — WORN (HORIZONTAL STAB) · airframe 30,173 hrs · 6,202 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER # 4 ELEVATOR HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.
Part: BONDING JUMPER — DAMAGED (RT ELEVATOR) · airframe 30,173 hrs · 6,202 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HAS DAMAGED BONDING STRAP. REPLACED RIGHT HAND ELEVATOR BONDING STRAP JUST OUT BOARD OF ELEVATOR ACTUATOR FITTING. BOND CHECK GOOD PER AMM 20-28-00.
Part: SLIDING WINDOW — DELAMINATED (ZONE 200 - FUSE) · airframe 28,787 hrs · 5,935 cycles
AIRCRAFT WAS NOT GROUNDED: CAPTAIN SLIDING WINDOW DELAMINATED. REPLACED SLIDING WINDOW PER AMM 56-11-40.
Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 28,771 hrs · 5,931 cycles
AIRCRAFT WAS NOT GROUNDED: R4 DOOR ACCUMULATOR PRESSURE BELOW PERIODIC SERVICE CHECK LIMITS. SERVICED R4 DOOR ACCUMULATOR PER AMM 52-10-00.
Part: ENGINE — FAILED (ZONE 400 - NAC/P) · airframe 27,731 hrs · 5,713 cycles
AIRCRAFT WAS GROUNDED: #2 ENGINE FAILED TO MAKE TAKEOFF POWER. REJECTED TAKE OFF UNDER 80 KNOTS. **SUPPLEMENTAL REPORT FOR AALA202205133192: REPLACED #2 ENGINE PER JOB CARD 26L40071004.** (CLOSED)
Part: NONE — NONE · airframe 27,731 hrs · 5,713 cycles
AIRCRAFT WAS GROUNDED: #2 ENGINE FAILED TO MAKE TAKEOFF POWER. REJECTED TAKE OFF UNDER 80 KNOTS. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
Part: MEGAPHONE — DAMAGED (ZONE 200 - FUSE) · airframe 27,483 hrs · 5,660 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE HANDLE IS LOOSE. REPLACED MEGAPHONE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-51.
2021
Part: ELECTRICAL BOX — DEFECTIVE (SEAT ROW 18) · airframe 25,468 hrs · 5,227 cycles
AIRCRAFT WAS GROUNDED: WHILE AT CRUISE FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM SEAT ROW 18 RIGHT. CREW FOLLOWED QRH PROCEDURE AND THE SMOKE STOPPED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MSN WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. INITIAL TROUBLESHOOTING INDICATES THE IN FLIGHT ENTERTAINMENT SYSTEM IS THE CAUSE OF THE ISSUE. FOUND SEAT ELECTRONIC BOX AT SEAT ROW 18 TO BE THE CAUSE OF THE ODOR. REPLACED SEAT ELECTRONIC BOX AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 44-24-32.
Part: NONE — NONE · airframe 25,468 hrs · 5,227 cycles
AIRCRAFT WAS GROUNDED: WHILE AT CRUISE FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM SEAT ROW 18 RIGHT. CREW FOLLOWED QRH PROCEDURE AND THE SMOKE STOPPED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MSN WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. INITIAL TROUBLESHOOTING INDICATES THE IN FLIGHT ENTERTAINMENT SYSTEM IS THE CAUSE OF THE ISSUE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)
Part: RELAY — NONE (ZONE 100 - FUSE) · airframe 25,292 hrs · 5,192 cycles
AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO LAX DUE TO RECEIVING AN ECAM MESSAGE FOR FUEL CENTER LEFT TRANSFER FAULT AS WELL AS LEFT WING AND RIGHT WING FUEL TANK OVERFLOW FAULTS. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT LAX WITHOUT FURTHER INCIDENT. REPLACED RELAY AUTO CONTROL #1 CENTER 7QL (AALA202110063714) AND JET PUMP 1 CONTROL ACTUATOR 11QL (AALA202110065797) PER AMM 28-26-00-810-801-A, AMM 28-26-810-804-A AND AMM 28-26-51-400-001-A. A SATISFACTORY OPERATIONAL CHECK.
Part: ACTUATOR — NONE (ZONE 100 - FUSE) · airframe 25,292 hrs · 5,192 cycles
AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO LAX DUE TO RECEIVING AN ECAM MESSAGE FOR FUEL CENTER LEFT TRANSFER FAULT AS WELL AS LEFT WING AND RIGHT WING FUEL TANK OVERFLOW FAULTS. NO EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED AT LAX WITHOUT FURTHER INCIDENT. REPLACED RELAY AUTO CONTROL #1 CENTER 7QL (AALA202110063714) AND JET PUMP 1 CONTROL ACTUATOR 11QL (AALA202110065797) PER AMM 28-26-00-810-801-A, AMM 28-26-810-804-A AND AMM 28-26-51-400-001-A. A SATISFACTORY OPERATIONAL CHECK.
Part: THERMOCOUPLE — DEFECTIVE (ZONE 400 - NAC/P) · airframe 25,284 hrs · 5,190 cycles
AIRCRAFT WAS NOT GROUNDED: #2 ENGINE APPEARED TO BE STUCK IN APPROACH IDLE DURING DESCENT. AT 13000 FT N1 IDLE WAS 43% ON ENGINE 2 N1 IDLE WAS 31% ON ENGINE 1. REPLACED FUEL TEMPERATURE THERMOCUOPLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 73-35-15.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,756 hrs · 5,088 cycles
AIRCRAFT WAS NOT GROUNDED: L2 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT.
2020
Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 22,843 hrs · 4,722 cycles
AIRCRAFT WAS NOT GROUNDED: L2 DOOR ASSIST BOTTLE FOUND LOW PS CHECK LIMITS. SERVICED L2 DOOR ASSIST BOTTLE PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (R4 DOOR ASSIST) · airframe 22,843 hrs · 4,722 cycles
AIRCRAFT WAS NOT GROUNDED: R4 DOOR ASSIST BOTTLE FOUND BELOW PS CHECK LIMITS. SERVICED R4 DOOR ASSIST BOTTLE PER AMM 52-10-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,479 hrs · 4,652 cycles
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT BATTERY LOCATED BY DOOR L1 INDICATION DEAD (FAULTY). MAINTENANCE REPLACED FLASHLIGHT BATTERY PER MM 25-65-00.
Part: DAMPER — FAULTY (L2 DOOR) · airframe 21,596 hrs · 4,463 cycles
AIRCRAFT WAS GROUNDED: L2 DOOR DAMPER REQUIRED REPLACEMENT. MAINTENANCE REPLACED DOOR DAMPER PER AMM 52-22-14.
Part: DAMPER — OUT OF RIG (L2 DOOR) · airframe 21,596 hrs · 4,463 cycles
AIRCRAFT WAS GROUNDED: L2 DOOR DAMPER REQUIRED RIGGING. MAINTENANCE ACCOMPLISHED DOOR DAMPER RIGGING PER AMM 52-22-14.
Part: DAMPER — FAULTY (L2 DOOR) · airframe 21,580 hrs · 4,460 cycles
AIRCRAFT WAS GROUNDED: INSPECTION OF DOOR L2, FOUND DAMPER FAULTY. MAINTENANCE REPLACED DOOR DAMPER L2 PER AMM 52-22-14.
2019
Part: PROXIMITY SENSOR — MALFUNCTIONED (LT WING TE FLAP) · airframe 20,937 hrs · 4,326 cycles
AIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO LAX ON ACCOUNT OF STUCK FLAP INDICATION. MAINTENANCE REMOVED AND REPLACED L/H FLAP INTERCONNECTING STRUT PROXIMITY SENSOR 39CV IAW AMM 27-51-44. ACCOMPLISHED OPS TEST OF FLAP FAILURE DETECTION SENSORS IAW AMM 27-51-00. OPS CHECKED NORMAL.
Part: LIGHT — LOOSE (ZONE 200) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: R4 DOOR EMERGENCY LIGHT LOOSE IN MOUNT. MAINTENANCE REPLACED LIGHT PER AMM 33-51-17.
Part: CONNECTOR — LOOSE (ZONE 200) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: DOOR R3 EVACUATION RESET AND LIGHT INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR AND RECONNECTED IT PER AMM 23-73-00.
Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: R4 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 23-73-00.
Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 7AC AND 9AC EMERGENCY ESCAPE PATH LIGHT INOPERABLE. TROUBLESHOT LIGHTING PER ASM 33-51-04 AND FOUND LOOSE CONNECTIONS AND RESEATED CONNECTIONS PER ESPM 20-44-06 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 7AC AND 9AC EMERGENCY ESCAPE PATH LIGHT INOPERABLE. TROUBLE SHOT EMERGENCY LIGHTING AND FOUND LOOSE CONNECTIONS AT IN-SEAT HARNESS AND RESEATED CONNECTIONS PER ESPM 20-44-06 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
Part: SHEAR PLATE — CRACKED (FRAME 69) · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 53-41-14.
Part: PROFILE — CORRODED (FRAME 58) · corrosion level 2 · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON JOINT PROFILE AT FR 58 AND S38R. REPLACED JOINT PROFILE PER SRM 53-41-14.
Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED SILL PER SRM 53-41-14-300-001.
Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED SILL PER SRM 53-41-14-300-001.
Part: WEB — CORRODED (FRAME 35.4) · corrosion level 2 · airframe 20,896 hrs · 4,317 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND FLOOR SUPPORT PANEL SUPPORT WEB ANGLE AT FR 35.4 AND Y-1722. REPLACED WEB PER SRM 51-74-00-801 AND 51-42-11-801.
Part: SIGN — FAULTY (EMERGENCY LIGHTS) · airframe 20,588 hrs · 4,257 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR LOWER EMERGENCY EXIT LIGHT DID NOT COME ON. MAINTENANCE REPLACED EXIT MARKER PER TASK 33-51-13 AND SWP 20-43-13.
Part: OVEN — ODOR (MID GALLEY) · airframe 20,406 hrs · 4,221 cycles
AIRCRAFT NOT GROUNDED, PILOT REPORTS THERE WAS A SPARK, THEN AN ELECTRICAL BURNING SMELL IN GALLEY 3 OVEN. MAINTENANCE REMOVED AND REPLACED NR 3 OVEN IN MID GALLEY IAW AMM 25-35-19. ALL OPS CHECK OK.
Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 20,215 hrs · 4,184 cycles
AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE INDICATION FOR 30 SECONDS IN FLIGHT. FLIGHT ATTENDANTS FOUND NO EVIDENCE OF SMOKE. MAINTENANCE ACCOMPLISHED SATISFACTORY LAVATORY SMOKE DETECTION SYSTEM CHECK PER AMM 26-17-00.
Part: SIGN — BROKEN (CABIN) · airframe 19,655 hrs · 4,073 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY LIGHT ASSEMBLY ON DOOR FRAME COVER, BROKEN. MAINTENANCE REPLACED EXIT SIGN PER AMM 33-51-13.
Part: UNKNOWN — MALFUNCTIONED (COCKPIT DOOR) · airframe 19,572 hrs · 4,057 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING CRUISE FLIGHT WE WERE UNABLE TO OPEN THE FLIGHT DECK DOOR TO LET A FLT ATT OUT. PULLED T13 C/B AND HAD FA PUSH DOOR TO ALLOW FA TO EXIT DOOR RE-SECURED. MAINTENANCE ACCOMPLISHED OPS CHECK OF CDLS IAW 52-51-00. OPS CHECK GOOD.
Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 18,470 hrs · 3,832 cycles
THE AIRCRAFT WAS GROUNDED. 1R DOOR SLIDE DEPLOYED WHEN DOOR OPENED WITH SLIDE ARM LIGHT OUT AND ARMING LEVER UP AND SHOWING DISARMED. REPLACED R1 DOOR SLIDE ASSEMBLY PER MCM 25-94-01. REPLACED DOOR DAMPER DIAPHRAGM PER AMM 52-10-00. DOOR AND SLIDE OPERATION CHECKS NORMAL AS PER SIC 25-94-01. OK FOR SERVICE.
2018
Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 18,033 hrs · 3,747 cycles
AFTER TAKEOFF, THE LANDING GEAR WAS SLOW TO RETRACT. WHILE CLIMBING AND CONTACTING MAINTENANCE THE OUTFLOW VALVE OPENED AND THE CABIN LOST PRESSURE. AN EMERGENCY WAS DECLARED AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ON APPROACH, AN ECAM MESSAGE FOR PILOT ICE FAULT. THE AIRCRAFT WAS GROUNDED. REPLACED NOSE LANDING GEAR PROXIMITY SENSOR IAW AMM 32-31-73. TESTED NORMAL. ACCOMPLISHED GEAR SWINGS IAW AMM 32-31-00. PRESSURED AIRCRAFT IAW AMM 05-53-00. OPS AND LEAK CHECKED NORMAL.
Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 16,304 hrs · 3,356 cycles
L4 WALL MOUNTED LED EMERGENCY LIGHT HOUSING BROKEN AND PULLED FROM WALL. REPLACED WALL MOUNTED EMERGENCY LIGHT HOUSING BY L4 DOOR. OPS CHECKED OK, IAW AMM 33-51-18.
Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 16,304 hrs · 3,356 cycles
EMERGENCY LIGHT BULB BY THE L2 DOOR 2L, IN FRONT OF LAVATORY H, WAS HANGING LOOSE. REPLACED THE WALL MOUNTED EMERGENCY LIGHT. OPS CHECKED OK IAW AMM 33-51-18.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,021 hrs · 3,293 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY DOOR, 3R SIDEWALL, LIGHT INOPERABLE. MAINTENANCE RELAMPED PER AMM 33-21-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: LEVER — MISINSTALLED (R3 DOOR) · airframe 15,936 hrs · 3,271 cycles
DURING A CHECK OF THE R3 DOOR ASSIST BOTTLE PRESSURE, FOUND STRIKER LEVER SAFETIED IN DISARMED POSITION. KNURLED NUT NOT PROPERLY ENGAGED ON THE STRIKE LEVER.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 15,391 hrs · 3,158 cycles
L1DOOR EMERGENCY LIGHT LENS IS DETACHED. SECURED THE L1 EMERGENCY LIGHT LENS IAW AMM 33-51-13.
Part: UNKNOWN — ODOR (CABIN) · airframe 14,845 hrs · 3,053 cycles
DETECTED A BURNING ELECTRICAL ODOR FOR A SHORT TIME AT ROW 11. APPEARED TO COME FROM THE FOLD OUT VIDEO SCREEN AT SEAT 11B. THE VIDEO SCREENS BEHIND STOPPED WORKING FOR A SHORT TIME. OPENED ALL SEAT BOXES AT ROW 11, COULD NOT DETECT ANY BURNING ELECTRICAL ODOR. ALL CONNECTORS ARE SECURE AND INSPECTED ALL VIDEO MONITORS IN ROW 11, NO BURNING ODOR. ALL VIDEO MONITORS IN ROW 11 AND ROW 12. OPERATIONS CHECKED NORMAL IAW AMM 44-21-00.
Part: UNKNOWN — ODOR (ROW 11) · airframe 14,845 hrs · 3,053 cycles
A BURNING ELECTRICAL ODOR FOR A SHORT TIME AT ROW 11. APPEARED TO COME FROM THE FOLD OUT VIDEO SCREEN AT SEAT 11B. OPENED UP ALL SEAT BOXES AT ROW 11, COULD NOT DETECT ANY BURNING ELECTRICAL ODOR. ALL CONNECTORS ARE SECURE AND INSPECTED, ALL VIDEO MONITORS IN ROW 11, NO BURNING ODOR. ALL VIDEO MONITORS AT ROW 11 AND 12. OPS CHECKED NORMAL IAW AMM 44-21-00.
2017
Part: SIGN — UNSECURE (CABIN) · airframe 13,777 hrs · 2,835 cycles
LOOSE CABIN EXIT MARKER AT THE R4 DOOR. REPLACED THE SIGN.
Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 13,700 hrs · 2,820 cycles
AIRCRAFT WAS NOT GROUNDED. R4 DOOR EMERGENCY CYLINDER PRESSURE LOW BEYOND LIMIT. SERVICED DOOR EMERGENCY CYLINDER PER AMM 52-10-00.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 12,952 hrs · 2,667 cycles
R1 DOOR EMERGENCY EXIT LIGHTS MISSING THE LENS. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-13.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,952 hrs · 2,667 cycles
R2 DOOR EMERGENCY EXIT LIGHT MISSING THE LENS. REPLACED R2 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-13.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,952 hrs · 2,667 cycles
R3 DOOR EMERGENCY EXIT LIGHT MISSING THE LENS. REPLACED R3 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-13.
Part: FILTER — ODOR (CABIN AIR) · airframe 12,682 hrs · 2,612 cycles
PERSISTENT DIRTY SOCK ODOR REPORTED FROM ROW 2D AFT. REPLACED RECIRCULATION FAN FILTERS IAW AMM 21-21-41.
Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 11,366 hrs · 2,322 cycles
EMERGENCY EXIT SIGN BY L2 DOOR IS DETACHED. SECURED EXIT SIGN. OPERATIONAL CHECK GOOD.
Part: BATTERY — FAILED (CABIN) · airframe 11,298 hrs · 2,309 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT 15WL FAILED TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. OPERATIONAL CHECK GOOD.
Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 11,188 hrs · 2,283 cycles
L4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-13-14. OPERATIONAL CHECKED GOOD.
2016
Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 10,797 hrs · 2,203 cycles
L4 DOOR DAMPER CYLINDER HAS LOW PRESSURE. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 10,663 hrs · 2,171 cycles
EMERGENCY LIGHTS AFT LEFT POWER SUPPLY UNIT FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.
Part: BATTERY — FAULTED (CABIN) · airframe 8,795 hrs · 1,764 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT TEST SHOWS POWER SUPPLY 10WL FAULTED. R & R POWER SUPPLY BATTERY. OPS CHECK NORMAL IAW AMM 34-43-00.
Part: BATTERY — FAULTED (CABIN) · airframe 8,795 hrs · 1,764 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT TEST SHOWS POWER SUPPLY 13WL FAULTED. R & R POWER SUPPLY BATTERY. OPS CHECK NORMAL IAW AMM 34-43-00.
2015
Part: COVER — MISSING (CABIN) · airframe 6,632 hrs · 1,264 cycles
AT ROW 14ABC AT SIDEWALL, FLOOR LEVEL HAS MISSING COVER EXPOSING CONNECTOR FOR EMER LIGHTS. REPLACED MISSING COVER FOR EMER LIGHT CONNECTOR ON SIDEWALL AT 14ABC. LIGHTS CHECKED OK IAW AMM 33-51-00.
Part: COVER — MISSING (CABIN) · airframe 6,632 hrs · 1,264 cycles
AT ROW 20ABC, AT SIDEWALL, FLOOR LEVEL HAS MISSING COVER EXPOSING CONNECTOR FOR EMER LIGHTS. REPLACED MISSING COVER FOR EMER LIGHT CONNECTOR ON SIDEWALL AT 20ABC. LIGHTS CHECKED OK IAW AMM 33-51-00.
Part: WIRE — BROKEN (CABNI) · airframe 6,622 hrs · 1,262 cycles
EMERGENCY LIGHTS AT SEAT ROW 11ABC & 12ABC INOPERATIVE. REPINNED WIRES IN PINS B & C OF CONNECTOR 7261VC7A IAW SWPM 20-48-21. ACCOMPLISHED EMERGENCY LIGHTS TEST AT 12ABC & 11ABC IAW AMM 33-51-00, OPERATIONS OK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 5,522 hrs · 1,051 cycles
EMERGENCY LIGHT POWER SUPPLY 11WL FAILS TEST. REPLACED BATTERY IAW AMM 33-51-38. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 5,522 hrs · 1,051 cycles
EMERGENCY LIGHT POWER SUPPLY 13WL FAILS TEST. REPLACED BATTERY IAW AMM 33-51-38. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.