N9011P
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2017-12-03 – 2017-12-03 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2017-12-03 – 2017-12-03 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
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.
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.
AIRCRAFT IN BASE MAINTENANCE: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #5 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #5 ON LH SIDE THS IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT FORWARD PASSENGER / CREW DOOR CUT OUT LOWER CENTER FITTING BETWEEN FR 16 AND FR 20 AT S23L. REPLACED CENTER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD RIGHT PASSENGER / CREW DOOR CUTOUT LOWER 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 AFT RIGHT PASSENGER, CREW DOOR CUTOUT LOWER SILL FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION CORNER FITTING FRAME 66L AT LEVEL STR 23 AT AFT GALLEY MEASURE ARE: L=0.751 INCH, W=0.438 INCH, D=0.020 INCH. MAINTENACE REPLACED CORNER FITTING AND FASTENERS LOC FR66L AT LEVEL STR23L AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001 AND DWG D53480505.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23L. REPLACED LOWER SILL PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BTW FR66 AND FR68 LH SIDE AFT GALLEY MEASURES ARE L=1.302 IN, W=0.383 IN, D=0.220 IN. MAINTENANCE REPLACED CENTER FITTING AND FASTENERS LOCATED BTW FR66 AND FR68 LH SIDE AFT GALLEY AREA I.A.W A319 SRM 51-72-11-911-001, A319 SRM 51-42-11-801 AND DWG D53480505, D53480048.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23R. REPLACED LOWER SILL PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION CORNER FITTING FRAME 68L AT LEVEL STR 23 AT AFT GALLEY MEASURE ARE: L=0.294 INCH, W=0.138 INCH, D=0.018 INCH. MAINTENANCE REPLACED CORNER FITTING AND FASTENERS LOC. FR68L AT LEVEL STR23L AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001 AND DWG D53480505.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 29 AND +Y1292. REPAIRED SEAT TRACK PER 53-21-15-300-009.
AIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK BETWEEN FR 36 AND FR 42 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN SEAT TRACK AT FR 44 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 59 AND +Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 47 AND FR 64 AT -Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 24 AND -Y1292. REPAIRED SEAT TRACK PER SRM 53-21-15-300-009.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR SEAT TRACK AT FR 45 PLUS 13 INCHES, AND AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 34 AND +Y765. REPAIRED SEAT TRACK PER SRM 53-21-15-300-009.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED 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 FORWARD CABIN FLOOR SUPPORT BETWEEN FR 16 AND FR 18 AT +Y1292. REPLACED FLOOR SUPPORT PER SRM 51-72-11.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING INBOARD FLAP ATTACH FITTING RT WING. MAINTENANCE REPLACED FITTING LOCATED AT INBOARD FLAP RH WING IAW A319 SRM 51-42-11-801, 51-72-11-911-001 AND DWG D57570280.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING INBOARD FLAP ATTACH FITTING LT WING. REPLACED FITTING LOC. ON INBOARD FLAP LT WING IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001, DWG D575 70280.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S43L. REPAIRED STRINGER PER EA 374801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S42L. REPAIRED STRINGER PER EA 374801.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N6 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #6 ON RH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #3 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #3 ON LH SIDE THS IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #2 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #2 ON LH SIDE THS IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #6 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #6 ON LH SIDE THS IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #1 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #1 ON LH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND A320 AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING #4 ON LH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #4 ON LH SIDE THS IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N1 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #1 ON RH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N5 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #5 ON RH SIDE THS IAW A320FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N2 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #2 ON RH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N3 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #3 ON RH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AT HINGE ARM END FITTING BEARING N4 ON RH THS. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #4 ON RH SIDE THS IAW A320 AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: SEAT MOUNTED EMERGENCY AISLE LIGHT INOP AT SET ROW 27ABC. TROUBLESHOT SEAT MOUNTED EMERGENCY AISLE LIGHT AT SEAT ROW 27ABC AND FOUND CONNECTOR FROM SEAT TO FLOOR TO BE DISCONNECTED. MAINTENANCE CONNECTED THE CONNECTOR AND ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-00.
AIRCRAFT WAS GROUNDED: FUME EVENT, AT ABOUT 12 MILE FINAL, 3000 FT FLIGHT ATTENDANTS IN THE REAR REPORTED AN ELECTRICAL SMELL FOR 5 MINUTES WHICH EVENTUALLY CLEARED AFTER SELECTING BLOWER AND EXTRACT TO OVRD. MAINTENANCE FOUND AFT GALLEY RH WORKING LIGHT BALLAST DEFECTIVE/BURNT AND REPLACED BALLAST IAW AMM 33-21-11.
AIRCRAFT WAS NOT GROUNDED: P/S CHECK CIDS1 TEST, FAULT EPSU (10WL) FWD L. MAINTENANCE REPLACED THE BATTERY AT 10WL EPSU IAW AMM 33-51-38.OPERATIONAL TEST NORMAL.
AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, L1 DOOR ACCUMULATOR PRESSURE OUT OF LIMITS AT 1600PSI AT 55 F DEGREE. MAINTENANCE SERVICED L1 DOOR IAW AMM 52-11-00.
AIRCRAFT WAS NOT GROUNDED: DURING THE ACCOMPLISHMENT OF THE EMERGENCY POWER SUPPLY UNIT CIDS 1 TEST A FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTEANCE L2 DOOR SLIDE CONTACTS THE FUSELAGE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 26L00025011.
AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE CONTACTS THE FUSELAGE WHEN DOOR IS OPENED. MAINTENANCE REPLACED L1 DOOR SLIDE PER TASK CARD 26L00025011-01.
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTING BATTTERY / EMERGENCY POWER SUPPLY UNIT 13WL AFT L CLASS 1 FAULT. MAINTENANCE REPALCED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202212078277) AND BATTERY (AALA202212077150) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTING BATTTERY / EMERGENCY POWER SUPPLY UNIT 13WL AFT L CLASS 1 FAULT. MAINTENANCE REPALCED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202212078277) AND BATTERY (AALA202212077150) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: ECAM INTERMITTENTLY INDICATED DOOR LEFT OVER WING EXIT OPEN AT ACT 24000. NO PRESSURIZATION INDICATING. MAINTENANCE ADJUSTED EXIT DOOR FLAP COVER PROXIMITY SENSOR PER AMM 52-71-13 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: RIGHT REAR EMERGENCY OPERATION CYLINDER OF THE PASSENGER CREW DOOR DOOR PRESSURE LOW 1100 PSI 70 F. SERVICED RIGHT REAR DOOR CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: R-2 DOOR ASSIST BOTTLE DISCHARGED. REPLACED DIAPHRAGM (AALA202207059903) AND SHEAR PIN (AALA202207052088) PER AMM 52-10-00. LEAK CHECKS GOOD.
AIRCRAFT WAS NOT GROUNDED: R-2 DOOR ASSIST BOTTLE DISCHARGED. REPLACED DIAPHRAGM (AALA202207059903) AND SHEAR PIN (AALA202207052088) PER AMM 52-10-00. LEAK CHECKS GOOD.
AIRCRAFT WAS NOT GROUNDED: L1 CREW DOOR EMERGENCY CYLINDER ACCUMULATOR LOW 1450 PSI (TEMP) 80'F. SERVICED DOOR EMERGENCY CYLINDER ACCUMULATOR PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: SEAT 13C WHITE EMERGENCY PATH LIGHT INOPERATIVE. REPLACED LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SEAT 27C HAS WIRE PULLED OUT OF CONNECTOR. PER ESPM 20-44-29, REPAIRED WIRE CONNECTION FOR SEAT 27C EMERGENCY LIGHT.
AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR RIGHT AFT WILL NOT OPEN. LAVATORY DOOR LUBE AND ADJUSTED PER AMM 25-40-00.
AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY ACCUMULATOR BOTTLE SHOWS 1150 PSI AT 60 FAHRENHEIT. SERVICED L1 DOOR EMERGENCY ACCUMULATOR BOTTLE, PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. DURING CABIN INTERCOMMUNICATION DATA SYSTEM 1 EMERGENCY POWER SUPPLY UNIT SYSTEM TEST, DISCOVERED "BATTERY/EMERGENCY POWER SUPPLY UNIT (10WL) FORWARD LEFT" MESSAGE. REMOVED AND REPLACED BATTERY OF EMERGENCY POWER SUPPLY UNIT (10WL), PER AMM 33-51-38.
AIRCRAFT GROUNDED - COCKPIT, FAR LEFT FIXED WINDOW (L3), ARCING DELAMINATION (ECAM ANTI-ICE LEFT WINDOW). REMOVED AND REPLACED L3 COCKPIT FIXED WINDOW PER AMM 56-11-12.
AIRCRAFT GROUNDED - ENG NO.2 FUEL FILTER CLOG, MSG ON FINAL APPROACH. REMOVED AND REPLACED NO. 2 ENGINE FUEL PUMP PER AMM 73-11-10 AND MCM 73-94-11, OPERATIONAL CHECK AND LEAK CHECK OK.
AIRCRAFT NOT GROUNDED: AFTER RECEIPT OF ROW/ROP LOST ECAM AUTOPILOT NO.2 MADE AN UNCOMMANDED DISCONNECT FOLLOWED BY ECAM DISCONNECT WARNING AND REAL TIME ACARS, AUTO FLT AP OFF PRINTER MESSAGE. PERFORMED TSM 22-66-00-810-905-A, ACCOMPLISHED AFS TEST, TEST PASSED, NO MAINTENANCE MESSAGED NOTED. OKAY FOR SERVICE,
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (13WL) AFT L. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OKAY.
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (12WL) EMER R. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OK.
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (10WL) FWD L. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OKAY.
AIRCRAFT WAS GROUNDED: PILOT REPORTS ON TAKEOFF, FLUID THAT SMELLS LIKE URINE LEAKED UNDER THE FORWARD FLIGHT ATTENDANTS JUMP SEAT AREA. MAINTENANCE REMOVED AND REPLACED FWD FIRST CLASS LAVATORY TOILET IAW AMM 38-31-41.
AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 5 HINGE HAS EXCESSIVE PLAY AND WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.
AIRCRAFT IN BASE MAINTENANCE: ELEVATOR HINGE AT STATION 2973 AND RIB 8 HAS EXCESSIVE PLAY AND WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.
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 #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 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: CORROSION ON FLOOR PANEL 262LG. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A01.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR PANEL 261LG. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A01.
AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.
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 RIGHT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING AT FR 66 AND S23R. REPLACED FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROISON ON LEFT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING AT FR 66 AND S23L REPLACED SILL SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 FIG 001 SHEET 3 PRINCIPLE 5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 20 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.
AIRCRAFT WAS NOT GROUNDED: 1L DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 12-00-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
L1 DOOR EMERGENCY CYLINDER PRESSURE WAS LOW. MAINTENANCE SERVICED THE CYLINDER IAW AMM 52-10-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: 13WL BATTERY LOW VOLTAGE. MAINTENANCE REPLACED BATTERY PER MM 25-60-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: L1 DOOR PRESSURE LOW. MAINTENANCE DOOR TO PROPER PRESSURE PER 52-20-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
L1 DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE DOOR CYLINDER IAW AMM 52-10-00.
THE EMERGENCY LIGHTS FAILED A POWER SUPPLY CHECK. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY, PERFORMED A SATISFACTORY OPERATIONAL CHECK.
FWD ENTRY DOOR DAMPER PRESSURE LOW. TEMP 84.2 DEG, 1600 PSI. SERVICED THE FWD ENTRY DOOR DAMPER IAW AMM 52-10-00.
THE AIRCRAFT WAS GROUNDED. SMOKE IN COCKPIT DURING FLIGHT. FOLLOWED QRH AND ECAMS ISOLATED NR 1 PACK AND SMOKE STOPPED. AIR CYCLE MACHINE NEEDS REPLACEMENT AND TURBINE BYPASS PIPE ASSEMBLY NEEDS TO BE INSTALLED DUE TO SMOKE ODOR FUME. REPLACED AIR CYCLE MACHINE PER 21-52-21. (PLEASE SEE SDR AALA201809199011)
THE AIRCRAFT WAS GROUNDED. AN EMERGENCY WAS DECLARED. SMOKE IN COCKPIT DURING FLIGHT. FOLLOWED QRH AND ECAMS ISOLATED NR 1 PACK AND SMOKE STOPPED. AIR CYCLE MACHINE NEEDS REPLACEMENT AND TURBINE BYPASS PIPE ASSEMBLY NEEDS TO BE INSTALLED DUE TO SMOKE ODOR FUME. INSTALLED BYPASS VALVE AND PIPE ASSEMBLY PER AMM 21-52-21. LEAK CHECK OF LEFT ACM INSTALLATION IS GOOD. (PLEASE SEE SDR AALA201809199008 AND MIC 35304906)
L1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTNENANCE SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00.
L1 DOOR DAMPER NEEDS TO BE SERVICED. SERVICED L1 DOOR DAMPER IAW AMM 52-10-00.
CLIMBING 15,000 FEET AT 310 KNOTS, FELT A CONSTANT AIRFRAME VIBRATION. CONTINUED TO CLIMB TO 24,000 FEET WITH NO CHANGE. THEN SLOWED TO 280 KNOTS WITH STILL NO CHANGE. VIBRATION FELT LIKE LATERAL MOTION, SIDE TO SIDE. ACCOMPLISHED TSM 27-20-00-810-802-A, FOUND THE SERVO VALVE FAULTED AT THE NR 2 YAW DAMPER. REMOVED ND REPLACED THE SERVO VALVE IAW AMM 27-26-51. AIRCRAFT WAS GROUNDED.
1L DOOR CYLINDER WAS LOW. MAINTENANCE SERVICED THE CYLINDER TO PROPER PRESSURE IAW AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED. 1R DOOR DAMPER CYLINDER IS LOW. SERVICED 1R DOOR DAMPER CYLINDER PER AMM 52-10-00.
L1 DOOR EXIT LOWER PANEL WAS FOUND LOOSE. SECURED THE PANEL IAW AMM 20-21-11.
LEFT FORWARD DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED THE DOOR ACCUMULATOR BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00 AND OPS CHECKED GOOD.
EMERGENCY LIGHT AT SEAT 12C IS INOPERATIVE. REPAIRED A DAMAGED WIRE IAW ESPM 20-53-53. OPS CHECKED GOOD.
AIRCRAFT WAS GROUNDED. PILOT REPORTED CABIN SMELLS BAD. MAINTENANCE FOUND OIL LEAKING FROM APU GENERATOR DRAIN PLUG AND THE APU STARTER. MAINTENANCE REPLACED A BROKEN SEAL ON THE APU STARTER AMM 49-42-51 AND REPLACED THE APU GENERATOR PER AMM 24-23-51. A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED (SEE AALA201712269024 FOR STARTER SEAL).
AIRCRAFT WAS GROUNDED. PILOT REPORTED CABIN SMELLS BAD. MAINTENANCE FOUND OIL LEAKING FROM APU GENERATOR DRAIN PLUG AND THE APU STARTER. MAINTENANCE REPLACED A BROKEN SEAL ON THE APU STARTER PER AMM 49-42-51 AND REPLACED THE APU GENERATOR PER AMM 24-23-51. A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED (SEE AALA201712299030 FOR GENERATOR).
FOUND LEFT ROW 12 EMERGENCY LIGHT INOPERATIVE. CONNECTED A BROKEN WIRE AT SEAT 12 IAW AMM 20-44-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED. LOOSE SLIDE BUSTLE AT DOOR 1L. REPLACED L1 DOOR ESCAPE SLIDE RAFT PACK ASSEMBLY AFT UPPER MOUNT STUD PER AMM 25-62-44.
R1 DOOR EMERGENCY EXIT MARKER LENS IS BROKEN. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-00. OPS CHECKED NORMAL.
DURING APPROACH THE CREW WAS UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL MODES. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. FLIGHT MANAGEMENT AND GUIDANCE COMPUTER NR 1 FOUND FAULTED. REMOVED AND REPLACED FLIGHT MANAGEMENT AND GUIDANCE COMPUTER NR 1 AND ACCOMPLISHED PRESSURIZATION CHECKS IAW AMM 21-31-00. SYSYTEM CHECKS NORMAL.
R4 DOOR EMER ASSIST CYLINDER, PRESS IS LOW. SERVICED CYLINDER IAW AMM 52-13-14.
ABORTED TAKEOFF, SPEED 85 KNOTS. ACFT WEIGHT 126,000 POUNDS. MASTER CAUTION LIGHT ILLUMINATED DURING TAKEOFF. POST FLIGHT DATA FROM THE MULTIPURPOSE CONTROL & DISPLAY UNIT SHOWED NO LATCHED FAULTS. PERFORMED GND SCANNING TASK OF CENTRAL WIRING SYS IAW MM 31-50-00-710 WITH NO FAULTS FOUND. INSPECTED ACFT IAW MM 05-51016 WITH NO DEFECTS NOTED.
ESCAPE PATH LIGHT HARNESS HAS A BROKEN WIRE UNDER SEAT 24ABC. REPAIRED WIRE IAW ESPM 20-43-11. OPERATIONS CHECKED NORMAL.