N9010R
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 | Operator | 2026-02-11 – 2026-02-11 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2026-02-11 – 2026-02-11 | Operator named in NTSB report |
| ROBERTSON CROP DUSTING SERVICE INC | Operator | 2009-06-15 – 2009-06-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN PANEL INTERNAL SURFACE AT FR 59 BETWEEN S42L AND S43L. REPAIRED SKIN PANEL PER EA 375970.
AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTIONAL TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER CREW DOOR CUT OUT LOWER FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 2 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #2 RH STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 4 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #4 RH STABILIZER IAW AMM 55-16-42-000-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 5 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #5 RH STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 6 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #6 RH STABILIZER IAWA 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 3 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #3 RH STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR BEARING HINGE ARM 1 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #1 RH STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 2 ON LH ELEVATOR. MAINTENANCE REPLACED LH ELEVATOR HINGE ARM END FITTING 2 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 5 ON LH ELEVATOR. MAINTENANCE REPLACED LH ELEVATOR HINGE ARM END FITTING 5 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 4 ON LH ELEVATOR. MAINTENANCE REPLACED LH ELEVATOR HINGE ARM END FITTING 4 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 6 ON LH ELEVATOR. REPLACED LH ELEVATOR HINGE ARM END FITTING 6 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 1 ON LH ELEVATOR. MAINTENANCE REPLACED LH ELEVATOR HINGE ARM END FITTING 1 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM END FITTING 3 ON LH ELEVATOR. MAINTENANCE REPLACED LH ELEVATOR HINGE ARM END FITTING 3 IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME AT FR 16 BETWEEN S22L AND S23L. REPAIRED FRAME PER EA 375284.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 67 PLUS 17 INCHES AND AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 42 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 58 AND +Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 41 PLUS 9 INCHES, AND AT +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT FORWARD PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 16 AND S23R. REPAIRED LOWER SILL PER EA 375267.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SEAT TRACK AT FR 64 AND -Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ONM MID CABIN FLOOR SEAT TRACK AT FR 44 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 37 AND FR 40 AT -Y1292. REPAIRED SEAT TRACK PER EA 375481.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 41 AND FR 47/51 AT +Y765. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD RIGHT PASSENGER / CREW DOOR LOWER SILL CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 39 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 842 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS DAMPING FUNCTION TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
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.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y1162. REPLACED BEAM PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L. REPAIRED SILL PER SRM 53-41-14.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 66 AND S11R AT THE #7 DOOR STOP AREA. REPAIRED FRAME PER SRM 53-41-12-300-011.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S43L. REPAIRED STRINGER IAW EA 375970.
AIRCRAFT IN BASE MAINTENANCE: CORROSION INBOARD PIN SPOILER 1 ON LT WING. THE MEASURES OF CORROSION ARE: L = 0.752 INCH, W = 0.215 INCH, D = 0.098 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 1 ON LH WING. MEASURES OF CORROSION ARE: L = 0.512 INCH, W = 0.120 INCH, D = 0.016 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 2 ON LH WING. MEASURES OF CORROSION ARE: L = 0.217 INCH, W = 0.101 INCH, D = 0.006 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OUTBOARD PIN SPOILER 5 ON LH WING. THE MEASURES OF CORROSION ARE: L = 0.750 INCH, W = 0.326 INCH, D = 0.006 INCH. MAINTENANCE REPLACED PIN-HINGE SPOILER IAW SRM A319 51-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R AT THE #1 DOORSTOP FITTING. REPAIRED FRAME PER SRM 53-41-12-300-011.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S42L. REPAIRED STRINGER PER EA 375970.
AIRCRAFT WAS GROUNDED: FLIGHT DECK RIGHT HAND SLIDING WINDOW HAS THIN SCRATCHES AND SWIRLS MAKE VISIBILITY DIFFICULT. REPLACED SLIDING WINDOW IAW AMM 56-12-11.
AIRCRAFT WAS GROUNDED: LOST BOTH GENERATORS SIMULTANEOUSLY AT FL270. ABLE TO RESTORE BOTH VIA CHECKLIST. RAT DEPLOYED. DIVERTED TO CLT. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. (OPEN)
AIRCRAFT WAS GROUNDED: LOST BOTH GENERATORS SIMULTANEOUSLY AT FL270. ABLE TO RESTORE BOTH VIA CHECKLIST. RAT DEPLOYED. DECESION MADE TO DIVERT TO CLT. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED # 1GCU (AALA202602131987) AND #2 GCU (AALA202602183619) IAW AMM 24-22-35 AND #1 IDG (AALA202602180630) AND #2 IDG (AALA202602186690) IAW JC 26J40024001.
AIRCRAFT WAS GROUNDED: LOST BOTH GENERATORS SIMULTANEOUSLY AT FL270. ABLE TO RESTORE BOTH VIA CHECKLIST. RAT DEPLOYED. DECESION MADE TO DIVERT TO CLT. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED # 1GCU (AALA202602131987) AND #2 GCU (AALA202602183619) IAW AMM 24-22-35 AND #1 IDG (AALA202602180630) AND #2 IDG (AALA202602186690) IAW JC 26J40024001.
AIRCRAFT WAS GROUNDED: LOST BOTH GENERATORS SIMULTANEOUSLY AT FL270. ABLE TO RESTORE BOTH VIA CHECKLIST. RAT DEPLOYED. DECESION MADE TO DIVERT TO CLT. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT MAINTENANCE REPLACED # 1GCU (AALA202602131987) AND #2 GCU (AALA202602183619) IAW AMM 24-22-35 AND #1 IDG (AALA202602180630) AND #2 IDG (AALA202602186690) IAW JC 26J40024001.
AIRCRAFT WAS GROUNDED: LOST BOTH GENERATORS SIMULTANEOUSLY AT FL270. ABLE TO RESTORE BOTH VIA CHECKLIST. RAT DEPLOYED. DECESION MADE TO DIVERT TO CLT. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED # 1GCU (AALA202602131987) AND #2 GCU (AALA202602183619) IAW AMM 24-22-35 AND #1 IDG (AALA202602180630) AND #2 IDG (AALA202602186690) IAW JC 26J40024001.
AIRCRAFT WAS GROUNDED: DURING DESCENT STRONG ODOR PRESENT IN FLIGHT DECK AND AFT GALLEY. MOSTLY ASSOCIATED WITH POWER CHANGES. IMPROVED IN FLIGHT DECK AFTER CROSS-BLEED SELECTED TO SHUT. STRONGER IN AFT GALLEY AFTER CROSS-BLEED SHUT. (OPEN)
AIRCRAFT WAS GROUNDED: DURING DESCENT STRONG ODOR PRESENT IN FLIGHT DECK AND AFT GALLEY. MOSTLY ASSOCIATED WITH POWER CHANGES. IMPROVED IN FLIGHT DECK AFTER CROSS-BLEED SELECTED TO SHUT. STRONGER IN AFT GALLEY AFTER CROSS-BLEED SHUT. MAINTENANCE FOUND THE APU OIL LUBE MODULE VALVE CAP LEAKING OIL AND REPLACED THE VALVE CAP PER CMM 49-90-57. A SATISFTORY LEAK CHECK WAS ACCOMPLISHED WITH NO LEAKS NOTED.
AIRCRAFT WAS GROUNDED: FAIRLY RAPID DECREASE NUMBER 1 ENGINE OIL QUANTITY IN CRUISE FLIGHT LEVEL 360. REDUCED THRUST ON NUMBER 1 WHEN OIL QUANTITY REACHED 4QTS AND DIVERTED TO KMIA. PERFORMED A PRECAUTIONARY SHUTDOWN ENGINE ONE WHEN OIL QUANTITY REACHED 3QTS. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TGB SEALS IAW ESM 72-00-62.
AIRCRAFT WAS GROUNDED: SMELL OF MELTED PLASTIC NOTICED IN THE COCKPIT AS WELL AS AFT CABIN. #1 FA SHUT OFF OVEN IN FORWARD GALLEY AND SMELL DISSIPATED. NOTHING FURTHER NOTED. AFTER COMPLETING J/C 26L00021001 SOF TROUBLESHOOTING FOUND NUMBER ONE OVEN COULD BE THE CAUSE OR ODOR. REPLACED OVEN PER AMM 25-35-19.
AIRCRAFT WAS GROUNDED: OIL ODOR CAN BE SMELLED THROUGHOUT CABIN AND COCKPIT. MAINTENANCE FOUND OIL LEAKING FROM APU DRAIN MAST REF MIC 1418556. ACCOMPLISHED WC/ 26L00021001 . CONFIRMED ODOR WAS FROM APU. BOTH ENGINE BLEEDS FOUND ODORLESS. APU DEFERED PER MIC 1418985. (OPEN)
AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW COMPLAINING OF ELECTRICAL ODOR IN AFT GALLEY. DURING PREFLIGHT. ACCOMPLISHED SOF JOB CARD 26L00021001 SUSPECT 5-7 AFT GALLEY COFFEE MAKER SOURCE OF SOF.MAINTENANCE REPLACED COFFEEMAKER.
AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT TEST FAILED DURING PS CHECK. FAULT EPSU(10WL) FWDL/DEU-B(300RH1) ATA 335138. AFTER TROUBLE SHOOTING FOUND WIRE FROM EPSU (10WL) TO R1 DOOR SLIDE OPEN. MAINTENANCE REPLACED R1 DOOR ESCAPE SLIDE IAW J/C 26L00025011.
AIRCRAFT WAS GROUNDED: FLT ATTENDANTS COMPLAINED OF AN ODOR IN THE CABIN DURING CRUISETHROUGH WEATHER AND IN THE DESCENT MOST PRONOUNCED IN AFT CABIN. **SUPPLEMENTAL REPORT FOR SDR AALA202502285271.** (CLOSED) MAINTENANCE PERFORMED DETAIL INSPECTION AND CLEANED APU AS REQUIRED IAW J/C 26L00021002 AND 26L00021014. LEAK CHECK AND OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: FLT ATTENDANTS COMPLAINED OF AN ODOR IN THE CABIN DURING CRUISETHROUGH WEATHER AND IN THE DESCENT MOST PRONOUNCED IN AFT CABIN. (OPEN)
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT ROW 14ABC SIDEWALL LIGHT INOP. MAINTENANCE REPLACED LIGHT IAW AMM 33-21-11.
AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT TO IDLE AND ENGINE STABILIZED. PUSHED THROTTLE UP SLIGHTLY AND ENGINE STALLED AGAIN. LEFT THROTTLE OF ENG 2 AT IDLE AND DIVERTED TO CMH DUE TO STRONG THUNDERSTORMS OVER THE FIELD IN PIT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: DURING DESCENT INTO PIT, GOT ENG 2 COMPRESSOR VANE ECAM. CLEARED ON ITS OWN THEN CAME BACK ABOUT 30 SECS LATER. SHORTLY AFTERWHILE DESCENDING THROUGH 28000 FEET GOT AN ENG STALL ECAM AND WECOULD HEAR THE POPPING FROM THE ENGINE. WENT TO IDLE AND ENGINE STABILIZED. PUSHED THROTTLE UP SLIGHTLY AND ENGINE STALLED AGAIN. LEFT THROTTLE OF ENG 2 AT IDLE AND DIVERTED TO CMH DUE TO STRONG THUNDERSTORMS OVER THE FIELD IN PIT. MAINTENACE PER TSM 75-30-00 FOUND #2 ENGINE VBV GEAR MOTOR BAD REPLACED GEAR MOTOR ASSEMBLY.
AIRCRAFT WAS GROUNDED: EMER LTS WIRING DAMAGED AND DISLODGED FROM SIDEWALL. SEAT ROWS 9 AND 10 LTS INOP. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHTS WIRING HARNESS FOR ROWS 9 & 10.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A STRONG MILDEW / DIRTY SWEAT SOCK ODOR IN CABIN AND FLIGHT DECK DURING ALL PHASES OF FLIGHT. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING OIL AND REPLACED IT. (AALA202408051354). MAINTENANCE ALSO REPLACED THE AIR OIL SEPERATOR (AALA202408058574). A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A STRONG MILDEW / DIRTY SWEAT SOCK ODOR IN CABIN AND FLIGHT DECK DURING ALL PHASES OF FLIGHT. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING OIL AND REPLACED IT. (AALA202408051354). MAINTENANCE ALSO REPLACED THE AIR OIL SEPERATOR (AALA202408058574). A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A DIRTY SOCK SMELL WAS NOTED ON FLIGHT DECK BEGINNING IN DESCENT THROUGH 9000. STILL EVIDENT AT 6000. MAINTENANCE FOUND THE APU GEARBOX VENT LINE CLOGGED AND UNCLOGGED THE VENT LINE.
AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT27E. REPLACED LIFE VEST PER AMM 25-66-52.
AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT15C. REPLACED LIFE VEST PER AMM 25-66-52.
AIRCRAFT WAS NOT GROUNDED: LIFE VEST PACKAGING OPENED AT SEAT13B. REPLACED LIFE VEST PER AMM 25-66-52.
AIRCRAFT WAS GROUNDED: OIL SMELL ON DESCENT INTO DFW. STARTED AT FL250 THROUGH LANDING. MAINTENANCE FOUND THE APU TURBINE BEARING RETURN TUBE LEAKING AND REPLACED IT PER CMM 49-26-95. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS NOTED.
AIRCRAFT WAS NOT GROUNDED: L2 LAVATORY DOOR DIFFICULT TO OPEN. MAINTENANCE ADJUSTED THE LAVATORY DOOR PER CMM 25-47-01.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUL. DURING CRUISE ECAM MESSAGE FOR FUEL USED AND FUEL ON BOARD DISAGREE. FLIGHT CREW ACCOMPLISHED THE QRH FUEL LEAK PROCEDURES. DURING DESCENT INTO TUL, THE FIRST OFFICER TOOK A PICTURE OF ECAM AND IT REFLECTED FUEL OVERLAND AFTER CLEARING THE INITIAL ECAM. THE LEFT MAIN TANK WAS ABOUT 1000LBS LESS THEN THE RIGHT TANK. THE AIRCRAFT LANDED SAFELY AT TUL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 28-11-00-810-805-A AND THE FAULTS CLEARED WITH NO ADDITIONAL FAULTS OR ISSUES NOTED BY MAINTENANCE. NO SPECIFIC PART CAUSING THE DIFFICULTY WAS IDENTIFIED BY MAINTENANCE.
AIRCRAFT WAS GROUNDED: L1 DOOR ASSIST BOTTLE NEEDS FULL SERVICE. SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: #2 ENGINE THRUST REVERSER PIVOT FITTING CRACKED. REPLACED PIVOT FITTING PER CMM 78-32-36 REPAIR #71
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202303245540: MAINTENANCE FOUND THE LEFT ENGINE ACCESSORY DRIVE GEAR BOX GARLOCK SEALS FOR THE IDG AND THE HYDRAULIC PUMP LEAKING. REPLACED BOTH GARLOC SEALS AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO LEAKS NOTED. (ALSO SEE AALA202304048961) ** (CLOSED)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202303245540** MAINTENANCE FOUND THE LEFT ENGINE ACCESSORY DRIVE GEAR BOX GARLOCK SEALS FOR THE IDG AND THE HYDRAULIC PUMP LEAKING. REPLACED BOTH GARLOC SEALS AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO LEAKS NOTED. (ALSO SEE AALA202304048961)
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. DURING CRUISE FLIGHT ENGINE 1 OIL QUANTITY CONTINUED TO DROP. AFTER APPROXIMATELY 2 HOURS OIL QUANTITIES AT 0.5 QUARTS. FLIGHT CREW REDUCED THRUST AND ENGINE OPERATED AT IDLE FOR LAST 45 MINUTES OF FLIGHT. ENGINE CONTINUED TO RUN. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER # 4 BEARING HINGE ARM ASSEMBLY HAS ELONGATED FASTENER HOLE. MAINTENANCE REPAIRED THE HINGE ARM ASSEMBLY PER EA 341726.
AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER # 3 BEARING HINGE ARM ASSEMBLY HAS TWO EACH EXISTING FASTENER HOLES FOR PIVOT FITTINGS OVERSIZED AND ARE OBLONGED. MAINTENANCE REPLACED THE HINGE ARM ASSEMBLY PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CABIN CEILING EMERGENCY LIGHT 205WL AT SEAT ROW 23 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY 205WL PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE: CABIN CEILING EMERGENCY LIGHT 201WL AT SEAT ROW 19 IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY 201WL PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: 1L DOOR GUST LOCK JAMMING AND HARD TP PUSH. MAINTENANCE CLEANED AND LUBRICATED GUST LOCK MECHANISM PER AMM 52-10-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, MAINTENANCE FOUND EMERGENCY POWER SUPPLY UNIT 10WL BATTERY CHARGE LOW. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT 10WL BATTERY PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY EXIT LIGHT TEST, MAINTEANCE FOUND EMERGENCY EXIT LEFT HAND EMERGENCY POWER SUPPLY UNIT BATTERY WITH LOW CHARGE. MAINTENANCE REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: AT ALTITUDE FL 230 CABIN PRESSURE EXCESSIVE FLUCTUATIONS. MAINTENANCE REPLACED RAM AIR INLET ACTUATOR FOR PACK 2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-61-51.
AIRCRAFT WAS GROUNDED: #1 BRAKE GOT EXTREMELY HOT COMPARED TO #2, 3, AND 4 WHILE TAXING SLOW. BRAKE WAS STICKING AND PULLING TO LEFT IN JAC, TEMPERATURE GOT AS HIGH AS 550 DEGREES WHILE OTHERS WERE MID 200'S. MAINTENANCE REPLACED #1 MAIN LANDING GEAR BRAKE PER AMM 32-42-27.
AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GUST LOCK IS DIFFICULT TO RELEASE. **SUPPLEMENTAL REPORT FOR AALA202207220244: REPLACED LATCH PER AMM 52-11-00. ** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GUST LOCK IS DIFFICULT TO RELEASE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: ACRID FUMES ON THE GROUND AND DURING THE DESCENT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202206106084: MAINTENANCE FOUND OIL LEAKING FROM BETWEEN THE GEAR BOX AND APU. REPLACED APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L31049003 . ** (CLOSED)
AIRCRAFT WAS GROUNDED: ACRID FUMES ON THE GROUND AND DURING THE DESCENT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: CENTER TANK 1 PUMP FAULT LIGHT ON FUEL PANEL .ECAM MESSAGE READS FUEL CENTER TANK PUMP 1 LOW PRESSURE. REPLACED RELAY 69QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TSM 28-21-00-810-817A.
AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 01 LOW PRESSURE MESSAGE / CENTER TANK PUMP FAULT LIGHT ILLUMINATED / AMBER LOW INDICATION ( FUEL PAGE). **SUPPLEMENTAL REPORT FOR AALA202201042822: REPLACED RELAY 69QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TSM 28-21-00-810-817A.**(CLOSED)
AIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 01 LOW PRESSURE MESSAGE / CENTER TANK PUMP FAULT LIGHT ILLUMINATED / AMBER LOW INDICATION ( FUEL PAGE). **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN)
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202201036694: ADJUSTED DOOR HINGE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: 9C EMERGENCY LIGHT IS WRONG COLOR. **SUPPLEMENTAL REPORT FOR AALA202111193106: REMOVED AND REPLACED 9C EMERGENCY LIGHT COVER PER AMM 33-50-00.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: 9C EMERGENCY LIGHT IS WRONG COLOR. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)
AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, DOOR L EMERGENCY EXIT CAME ON, SHOWED LEFT OVERWING EXIT NOT LOCKED. FLIGHT DECLARED EMERGENCY RETURNED TO MIA. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. INSPECTED AND ACCOMPLISHED EMERGENCY EXIT DOOR PER TSM 52-21-00-810-806-A NO FAULTS NOTED OK FOR SERVICE.
AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY PER WORK CARD 26L70032008.
AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.
AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY (AALA202109200856) AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.
AIRCRAFT WAS GROUNDED: NUMBER 4 WHEEL BRAKE TEMP PASSED 300 DEGREES DURING TAXI OUT AT JFK WITH BRAKE FANS ON. NUMBER 4 WHEEL BRAKE TEMP REACHED 440 DEGREES DURING TAXI BACK TO GATE. FOUND NUMBER 3 BRAKE SEIZED. REPLACED NUMBER 4 WHEEL BRAKE FAN MOTOR ASSEMBLY (AALA202109207894) PER AMM 32-48-51. REPLACED NUMBER 4 BRAKE ASSEMBLY (AALA202109206801) AS PER AMM 32-42-71. REPLACED NUMBER 4 WHEEL ASSEMBLY AS PER WORK CARD 26L70032008. REPLACED NUMBER 3 BRAKE ASSEMBLY (AALA202109203154) PER WORK CARD 26L70032008.
AIRCRAFT WAS NOT GROUNDED FUEL CENTER TANK PUMP 1 LOW PRESSURE: **SUPPLEMENTAL REPORT FOR AALA202107270783: REPLACED THE PRESSURE SWITCH FOR THE CENTER TANK #1 FUEL PUMP AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 28-21-15** (CLOSED)
AIRCRAFT WAS NOT GROUNDED FUEL CENTER TANK PUMP 1 LOW PRESSURE: (OPEN)
AIRCRAFT WAS NOT GROUNDED. R1 WINDSHIELD DELAMINATED. REPLACED WINDSHIELD, PER TASK CARD 56-94-01.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AR FR 66 AND FR 23R. REPLACED LOWER SILL PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANEL 231FF CRACKED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #6 HAS EXCESSIVE PLAY / WEAR AT RIB 9 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER CENTER SILL SHAPE FITTING AT FR 67 AND S23L. REPLACED SILL SHAPE FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED SILL SHAPE FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY / WEAR AT RIB 2 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS AFTER PERFORMING OPS TEST OF THE ESCAPE-FACILITIES MSG SHOWS BAT/EPSU (10WL) FWD L. MAINTENANCE REMOVED AND REPLACED 10WL FWD L EPSU POWER SUPPLY IAW AMM 33-51-38. OPS TEST OKAY.
POWER SUPPLY 10WL FAULTED ON A CIDS TEST. REPLACED THE POWER SUPPLY IAW AMM 33-51-38. OPS CHECKED OK.
FOUND THE EPSU 10WL FAULTED AFTER A SYSTEM TEST. RESET EPSU AND OPS CHECKED NORMAL IAW AMM 33-51-38.
L1 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS DEAD. INSTALLED A NEW BATTERY, OPS CHECKED OK IAW AMM 25-65-00.
EMERGENCY EXIT LIGHT AT L2 DOOR IS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-57-13. OPERATIONAL CHECK GOOD.
EMERGENCY EXIT LIGHT AT R2 DOOR IS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-57-13. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-JAC FLIGHT DIVERTED TO OKC ACCOUNT METALLIC ODOR IN COCKPIT, FIRST CLASS GALLEY AND CABIN. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 GALLEY OVEN AND NR 2 GALLEY OVEN (AALA20170103005) IAW AMM 25-35-19. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-JAC FLIGHT DIVERTED TO OKC ACCOUNT METALLIC ODOR IN COCKPIT, FIRST CLASS GALLEY AND CABIN. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 GALLEY OVEN (AALA20161230025) AND NR 2 GALLEY OVEN IAW AMM 25-35-19. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS IN BASE MAINTENANCE. R1 DOOR EXIT MARKER IS DAMAGED. REMOVED AND REPLACED EXIT MARKER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.
DURING DESCENT, RECEIVED AN ECAM "BRAKE SYSTEM 1 FAULTY". EMERGENCY DECLARED. LANDING UNEVENTFUL. A SUCCESSFUL RESET WAS ACCOMPLISHED DURING FINAL APPROACH. REMOVED & REPLACED THE BRAKING AND STEERING CONTROL UNIT IAW AMM 32-42-34. OPS CHECKED GOOD.
DURING CRUISE THE CREW REPORTED SMOKE IN THE FLIGHT DECK ACCOMPANIED BY AN ELECTRICAL ODOR. EMERGENCY DECLARED. LANDING UEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED TSM 05-50-00, MCM 05-96-84, INSPECTION OF ALL DEUS AND RADIO UNIT IN THE FLIGHT DECK AND ALL E&E COMPARTMENT COMPONENTS AND WIRING WITH NO DISCREPANCIES FOUND.
DURING TAKEOFF, RECEIVED MASTER CAUTION, VENT SKIN VLV FAULT, VENT BLOWER FAULT & VENT EXTRACT FAULT. ALSO AFTER SELECTING FLX TAKEOFF SETTING, RT ENG SPOOL UP LAGGED, COMPARED TO LT ENG CAUSING ACFT TO YAW FEET TO THE RT. TAKE OFF ABORTED AT APPROX 70 KNOTS. TROUBLE SHOT VENT SKIN, BLOWER VLV & VENT EXHAUST FAULTS IAW TSM 21-26-00-810-803-A WITH NO FAULTS FOUND. ACCOMPLISHED STEERING DEVIATION TEST IAW TSM 32-51-00-810-823-A WITH ALL INDICATIONS NORMAL.