N560UW
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| U.A Airways Inc | Operator | 2013-04-05 – 2013-04-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS NOT GROUNDED: DOOR L1 CHECK DOOR PRESSURE CAUTION MESSAGE ON FLIGHT ATTENDANTS PANEL. MAINTENANCE SERVICED THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00 WHICH CLEARED THE MESSAGE.
AIRCRAFT WAS NOT GROUNDED: ON DESCENT FORWARD FLIGHT ATTENDANT DISPLAY SHOWED CAUTION CHECK DOOR PRESSURE. MAINTENANCE SERVICED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: DOOR 2R DOOR ARMING HANDLE IS LOOSE. MAINTENANCE TIGHTEND HARDWARE ON DOOR 2R EMERGENCY CONTROL HANDLE PER AMM 52-11-22.
AIRCRAFT WAS NOT GROUNDED: DISARMING HANDLE DOOR 2R LOOSE. MAINTENANCE TIGHTENED DOOR 2R DOOR ARMING HANDLE PER AMM 25-62-47.
AIRCRAFT WAS GROUNDED: WHEN ARMING CABIN DOORS FLIGHT ATTENDANT REPORTS 1R DOOR INDICATES CHECK DOOR PRESSURE ON FLIGHT ATTENDANTS PANEL. MAINTENANCE FOUND THE R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER WAS LEAKING AND REPLACED IT PER AMM 52-22-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: 2R ARMING LEVER HAS A LOOSE SCREW. MAINTENANCE SECURED SCREW ON 2R LEVER.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THAT THE 2L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IS SHOWING LOW PRESSURE. MAINTENANCE REPLACED THE 2L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-14.
AIRCRAFT WAS GROUNDED: AFTER FLIGHT ATTENDANTS ARMED THE DOORS FOR DEPARTURE THE FLIGHT ATTENDANTS PANEL IS NOT SHOWING THE 2L DOOR ARMED AND THE MESSAGE CHECK DOOR PRESSURE IS DISPLAYED. MAINTENANCE SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00 WHICH CLEARED THE FAULTS.
AIRCRAFT WAS GROUNDED: AFTER FLIGHT ATTENDANTS ARMED THE DOORS FOR DEPARTURE, THE FLIGHT ATTENDANTS PANEL INDICATED THE 2L IS NOT SHOWING ARMED AND THE MESSAGE CHECK DOOR PRESSURE IS DISPLAYED. MAINTENANCE SERVICED THE 2L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-00-00.
AIRCRAFT WAS NOT GROUNDED: CHECK DOOR PRESSURE CAUTION ILLUMINATED ON FLIGHT ATTENDANT PANEL FOR THE 2L DOOR. MAINTENANCE SERVICED THE L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE 2L DOOR IS SHOWING CABIN PRESSURE INDICATION. MAINTENANCE SERVICED THE 2L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: SLIDE DISARMED CHECK PRESSURE APPEARED INFLIGHT ON FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE SERVICED L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: FUEL RIGHT WING TANK OVERFLOW ECAM ALERT. FLIGHT CREW SUCCESSFULLY RAN ECAM WITH CENTER TANK RIGHT TRANSFER REMAINING OFF. MAINTENANCE REPLACED FULL LEVEL SENSOR CHANNEL A 23QJ2 (AALA202512188968), UNDERFULL LEVEL SENSOR 24QJ2 (AALA202512181754) AND FULL LEVEL SENSOR CHANNEL B 27QJ2 (AALA202512188656) ON THE RIGHT-WING FUEL TANK PER AMM 28-46-15-401.
AIRCRAFT WAS GROUNDED: FUEL RIGHT WING TANK OVERFLOW ECAM ALERT. FLIGHT CREW SUCCESSFULLY RAN ECAM WITH CENTER TANK RIGHT TRANSFER REMAINING OFF. MAINTENANCE REPLACED FULL LEVEL SENSOR CHANNEL A 23QJ2 (AALA202512188968), UNDERFULL LEVEL SENSOR 24QJ2 (AALA202512181754) AND FULL LEVEL SENSOR CHANNEL B 27QJ2 (AALA202512188656) ON THE RIGHT-WING FUEL TANK PER AMM 28-46-15-401.
AIRCRAFT WAS GROUNDED: FUEL RIGHT WING TANK OVERFLOW ECAM ALERT. FLIGHT CREW SUCCESSFULLY RAN ECAM WITH CENTER TANK RIGHT TRANSFER REMAINING OFF. MAINTENANCE REPLACED FULL LEVEL SENSOR CHANNEL A 23QJ2 (AALA202512188968), UNDERFULL LEVEL SENSOR 24QJ2 (AALA202512181754) AND FULL LEVEL SENSOR CHANNEL B 27QJ2 (AALA202512188656) ON THE RIGHT-WING FUEL TANK PER AMM 28-46-15-401.
AIRCRAFT WAS NOT GROUNDED: CHECK DOOR PRESSURE ON CIDS PANEL DISPLAYS BY 2L AND PRESSURE LIGHT FLASHES ON DOOR. MAINTENANCE SERVICED THE L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ECAM ALERTED IN FLIGHT FOR 2 MINUTES. FLIGHT ATTENDANTS REPORTED ALL LAVATORIES UNOCCUPIED AT TIME OF ALERT, AND NO INDICATIONS OF SMOKE OR SCENTS IN ANY LAVATORY. MAINTENANCE ACCOMPLISHED RESET OF LAVATORY SMOKE DETECTION SYSTEM WITH NO FAULTS NOTED PER AMM 26-17-00.
AIRCRAFT WAS NOT GROUNDED: DOOR 2R ARMING LEVER LOOSE. MAINTENANCE TIGHTENED ARMING HANDLE AT DOOR 2R PER AMM 20-21-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED RIGHT BRAKE HARD SHUTTER WHILE BRAKING AT SLOW SPEEDS 1-3 KNOTS. MAINTENANCE REPLACED THE #4 MAIN LANDING GEAR TACHOMETER PER AMM 32-42-57 (AALA202509111082) AND BSCU PER AMM 32-42-34. (AALA202509110859) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED RIGHT BRAKE HARD SHUTTER WHILE BRAKING AT SLOW SPEEDS 1-3 KNOTS. MAINTENANCE REPLACED THE #4 MAIN LANDING GEAR TACHOMETER PER AMM 32-42-57 (AALA202509111082) AND BSCU PER AMM 32-42-34. (AALA202509110859) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS R2 EMERGENCY EXIT DOOR ARM HANDLE IS LOOSE. MAINTENANCE TIGHTENED SLIDE ARMING HANDLE PER AMM 52-22-21.
AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
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.
AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE 1L DOOR GUST LOCK WAS INOPERATIVE. MAINTENANCE CLEANED L1 DOOR GUST LOCK MECHANISM AND ACCOMPLISHED A A SATISFACTORY OPERATIONAL CHECK PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: ON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, AN ECAM BRAKES HOT DELAY TAKEOFF WARNING APPEARED. LOW SPEED REJECT ACCOMPLISHED IMMEDIATELY. BRAKE TEMPERATURE INDICATIONS ON LEFT BRAKES WERE ABOVE 500& 400 C ON LEFT SIDE, AND 80C AND 110C ON RIGHT SIDE. PRIOR TO TAKEOFF, ALL BRAKE INDICATIONS WERE BELOW 100C. MAINTENANCE ACCOMPLISHED TSM 32-42-00-810-922A. JACKED LEFT MAIN LANDING GEAR, #1 BRAKE DRAGGING SLIGHTLY, REPLACED #1 BRAKE ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-42-27.
AIRCRAFT WAS IN BASE MAINTENANCE: DELAMINATED SLIDING WINDOW PANEL CAPTAIN SIDE IN COCKPIT. REMOVED AND REPLACED SLIDING WINDOW PANEL CAPTAIN SIDE IN COCKPIT.
AIRCRAFT WAS IN BASE MAINTENANCE: DELAMINATED SLIDING WINDOW PANEL FIRST OFFICER IN COCKPIT. REMOVED AND REPLACED SLIDING WINDOW PANEL FIRST OFFICER IN COCKPIT
AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ON SLIDE AT PASSENGER CREW DOOR 832 (WHEN DOOR IS FULL OPEN MECHANISM DOES NOT SECURE). REPLACED ESCAPE SLIDE DOOR 832.
AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ON SLIDE AT PASSENGER CREW DOOR 831 (WHEN DOOR IS FULL OPE N THE MECHANISM, DOES NOT SECURE. REPLACED ESCAPE SLIDE DOOR 831.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION CORNER FITTING LOCATED AT FR 68 AT LEVEL OF STR 23R IN AFT GALLEY AREA (CPCP C534143-01). REPLACED CORNER FITTING PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR 66 AT LEVEL OF STR 23R IN AFT GALLEY AREA. REPLACED CORNER FITTING PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA CORNER FITTING AT FR 66 AND S23L. REPLACED CORNER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA CORNER FITTING AT FR 68 AND S23L. REPLACED CORNER FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENNACE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENNACE: 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 LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL S23R IN PASSNGER CABIN. REPLACED LOWER SILL PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM LOCATED AT +Y765 BETWEEN FR 69 AND FR 70 IN PASSENGER CABIN. REPLACED FLOOR BEAM PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL S23L IN PASSENGER CABIN. REPLACED LOWER SILL PER SRM 51-42-11-801.
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR MORE DIFFICULT THAN NORMAL TO OPEN AND CLOSE. RESECURED LOOSE PHILOP SCREW.
AIRCRAFT WAS GROUNDED: FUME EVENT: DESCENDING FROM 23000 FEET TO 10000 FEET. IDLE THRUST. TEMPERATURE -24C SAT TO +1C SAT. UNABLE TO DETERMINE ORIGIN. COCKPIT ONLY. OXYGEN MASKS DONNED. ACCOMPLISHED JOB CARD 26L00021001. FOUND SOURCE OF ODOR TO BE #1 OVEN. REPLACED #1 OVEN PER AMM 25-35-19.
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE FOUND UPPER TRIM MISSING 2 FASTENERS AND INSTALLED THEM. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE. ADJUSTED AFT RIGHT LAVATORY DOOR.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT L1 DOOR NOT BLINKING. MAINTENANCE REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.
AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT 80 KNOTS DUE TO BRAKES RELEASED ECAM MESSAGE. SAFELY RETURNED TO GATE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT 80 KNOTS DUE TO BRAKES RELEASED ECAM MESSAGE. SAFELY RETURNED TO GATE. **SUPPLEMENTAL REPORT FOR AALA202201318680: ACCOMPLISHED TSM 32-42-00-810-815. CONFIRMED RIGHT HAND MLG, 2M AXILE HARNESS SHORT TO SHIELD CAUSING LOSS OF TACHOMETER 4 SIGNAL TO BRAKE AND STEERING CONTROL UNIT (BSCU). REPLACED HARNESS (AALA202201318680) PER AMM 32-11-43. REPLACED UNSERVICEABLE RECEPTACLE LGAB4-4 (AALA202201317638) PER ESPM 20-44-11 AND AWM 32-11-02. ACCOMPLISHED SATISFACTORY ELECTRICAL TEST BETWEEN BSCU AND TACHOMETER 4. ACCOMPLISHED SATISFACTORY LMP GROUND CONFIDENCE CHECK. ACCOMPLISHED SATISFACTORY NORMAL BRAKE OPERATION, TACHOMETER FUNCTIONAL TEST, AND BSCU BITE CHECK PER AMM 32-42-00 AND AMM 32-46-00. ACCOMPLISHED SATISFACTORY BRAKE TEMPERATURE OPERATION CHECK PER AMM 32-47-00.** (CLOSED)
AIRCRAFT WAS GROUNDED: ABORTED TAKEOFF AT 80 KNOTS DUE TO BRAKES RELEASED ECAM MESSAGE. SAFELY RETURNED TO GATE. **SUPPLEMENTAL REPORT FOR AALA202201318680: ACCOMPLISHED TSM 32-42-00-810-815. CONFIRMED RIGHT HAND MLG, 2M AXILE HARNESS SHORT TO SHIELD CAUSING LOSS OF TACHOMETER 4 SIGNAL TO BRAKE AND STEERING CONTROL UNIT (BSCU). REPLACED HARNESS (AALA202201318680) PER AMM 32-11-43. REPLACED UNSERVICEABLE RECEPTACLE LGAB4-4 (AALA202201317638) PER ESPM 20-44-11 AND AWM 32-11-02. ACCOMPLISHED SATISFACTORY ELECTRICAL TEST BETWEEN BSCU AND TACHOMETER 4. ACCOMPLISHED SATISFACTORY LMP GROUND CONFIDENCE CHECK. ACCOMPLISHED SATISFACTORY NORMAL BRAKE OPERATION, TACHOMETER FUNCTIONAL TEST, AND BSCU BITE CHECK PER AMM 32-42-00 AND AMM 32-46-00. ACCOMPLISHED SATISFACTORY BRAKE TEMPERATURE OPERATION CHECK PER AMM 32-47-00.** (CLOSED)
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND STABILIZER ELEVATOR #4 HINGE FITTING BEARING SHOWS SIGNS OF CORROSION. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY FAULTS AT FORWARD LEFT (10WL). REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT 10WL PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY FAULTS AT MID RIGHT (14WL). REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT 14WL PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: SMOKE LAVATORY DETECTOR FAULT MESSAGE IN CRUISE. VISUAL INSPECTION OF LAVATORIES WAS NORMAL. RESET LAVATORY SMOKE DETECTOR PER AMM 26-17-00.
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT ARE FAILING OPERATIONAL CHECK. REPLACED L1 DOOR SLIDE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-44, 52-10-00 AND 33-51-00.
AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN CEILING EMERGENCY LIGHT HAS BROKEN TERMINAL(201WL). REPLACED TERMINAL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER ESPM 20-56-22-0301 AND AMM 33-51-11.
AIRCRAFT IN BASE MAINTENANCE: CABIN EMERGENCY LIGHT ASSEMBLY MOUNTED IN THE CEILING ADJACENT TO L3 DOOR FAILS TO ILLUMINATE DURING TESTING. SECURED LIGHT CONNECTOR PER AMM IAW 33-51-16.
AIRCRAFT WAS NOT GROUNDED. L1 DOOR DAMPER NITROGEN CHARGE LOW. SERVICED DAMPER PER AMM 52-11-00.
AIRCRAFT WAS GROUNDED: L2 DOOR ASSIST BOTTLE LEAKING. REPLACED DIAPHRAGM OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS CABIN INTERCOMMUNICATION DATA SYSTEM SHOWS CHECK PRESSURE FOR 2L DOOR. SERVICED 2L DOOR BOTTLE PER AMM 52-10-00-614-001A.
AIRCRAFT WAS NOT GROUNDED: 22D EMERGENCY ESCAPE LIGHT LENS MISSING. MAINTENANCE REPLACED LIGHT PER AMM 33-50-00.
AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT DISPLAYED CHECK DOOR PRESSURE ON DOOR 2L. MAINTENANCE SERVICED DOOR DAMPER TO PROPER PRESSURE PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT LED WOULD NOT FLASH AT 4R DOOR. MAINTENANCE REPLACED FLASHLIGHT PER STANDARD PRACTICES.
AIRCRAFT WAS NOT GROUNDED: DURING WAKE UP CHECK, SEAT MOUNTED EMERGENCY LIGHT AT ROW 9R DAMAGED. MAINTENANCE REPLACED LIGHT PER AMM 33-51-18-000-001-A.
AIRCRAFT WAS GROUNDED: ON TAKE OFF ROLL, RECEIVED A HOT BRAKE ECAM MESSAGE. THE BRAKE ON #2 WHEEL WAS ABOVE 300 DEGREES AND THE OTHERS WERE WELL BELOW. AFTER REJECTING THE TAKEOFF, #2 BRAKE REACHED 475 DEGREES WITH BRAKE FANS ON. MAINTENANCE INSPECTED BRAKE TEMPERATURE ON #2 BRAKE PER TSM 32-42-00-810-922-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK. MAINTENANCE ALSO TROUBLESHOT PFR MESSAGE "BRAKES HOT" PER TSM 32-47-00-810-817-A, BITE TEST PASSED, AND INSPECTED "BRAKE OVERHEAT" CONDITIONS PER TSM 32-42-00-810-924-A.
AIRCRAFT WAS GROUNDED: PILOT REPORTS ON DECENT @ FL180 FLT IDLE N1 35.2% ENG 1/ ENG 2 48.7% FF 720 LBS / FF 1360 LBS AT @ 10000 FEET AT IDLE N1 29.6/840 LBS / 42.2%1440 LBS H. MAINTENANCE REPLACED RH ENGINE FUEL FILTER IAW AMM 73-12-42. ENGINE OPERATION NORMAL IAW TSM 73-22-00-810-812-A13.
SEAT 3L EMERGENCY LIGHT WAS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-18.
MULTIPLE AREAS OF CORROSION FOUND ON THE THRESHOLD PLATE, FRAMES 52 - 57. REPLACED THE THRESHOLD PLATE IAW SRM 51-72-11.
CORROSION ON THE FLOOR SUPPORT AT FRAME 16, AND Y-1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT FR 16 AND RBL 10. REPLACED FLOOR SUPPORT PER SRM 51-72-11.
CORROSION ON PLATE AT FRAME 68, -Y1292. REPAIRED THE PLATE IAW SRM 53-41-14-300-001, REPAIR PRINCIPLE 1.
CORROSION ON FLOORBEAM ANGLE AT FRAME 68, +Y1292. REPAIRED THE FLOORBEAM ANGLE IAW SRM 53-41-14-300-001, REPAIR PRINCIPAL 7.
CORROSION ON SILL SHAPE FITTING AT FRAME 67 AND STRINGER 23L. REPLACED SILL SHAPE FITTING IAW AMM 53-45-15-1401, FIG 1, SHEET 1, AND SRM 51-42--11.
CORROSION ON THE R4 DOOR SILL, FRAMES 67 AND 68, STRINGER 23R. REPLACED DOOR SILL IAW SRM 51-42-11, AND 51-72-00.
R2 DOOR DISPLAYED LOW PRESSURE ON THE CIDS PANEL. CHECKED THE R2 DOOR SLIDE BOTTLE PRESSURE AND FOUND WITHIN GREEN. ADVISED TECH FOR FOLLOW UP PER AMM AND FIM 25-62-00.
AFTER ARMING DOORS, THE FIRST FLIGHT ATTENDANT NOTICED LOW PRESSURE ON CIDS PANEL FOR THE R2 DOOR SLIDE. SERVICED THE BOTTLE IAW AMM 52-10-00. OPS CHECKED GOOD.
EMERGENCY LIGHT COVERS AT SEATS 1C, 3C WERE MISSING. REPLACED EMERGENCY LIGHTS AT ROW 3.
EMERGENCY LIGHT COVERS AT SEATS 1C, 3C, MISSING. REPLACED EMERGENCY LIGHTS.
L4 DOOR LOWER EMERGENCY LIGHT LENS WAS BROKEN. REMOVED AND REPLACED THE LENS.
THE AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHT AT 4L,12L AND 30L ARE BROKEN. REPLACED SEAT MOUNTED EMERGENCY LIGHTS AT 4L, 12L,16L AND 30L. OPERATIONS CHECK OK.
EMERGENCY LIGHT BATTERY 13WL WAS FOUND INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-55-00. OPS CHECKED GOOD.
AFT RIGHT GALLEY FLOOR IS SOFT ACCORDING TO THE FLIGHT ATTENDANT. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 53-42-12. OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.
MOMENTARY SELF CORRECTING NR 2 ENGINE STALL . ECAM MESSAGE DURING CRUISE & DESCENT WHILE ENCOUNTERING MODERATE AIRCRAFT WAKE TURBULENCE . ENGINE PERAMETERS STAYING NORMAL . REPLACED P2/T2 PROBE IAW AMM.
DELAMINATION ON CARGO FLOOR PANEL 151MK. REMOVED AND REPLACED THE FLOOR PANEL.
DELAMINATION ON THE AFT CARGO FLOOR PANEL 151GF. REMOVED AND REPLACED THE FLOOR PANEL.
DELAMINATION ON AFT CARGO FLOOR PANEL 162EF. REPLACED THE FLOOR PANEL IAW AMM 53-42-11.
FAILED CIDS TEST. RT EXTERNAL BATTERY. RESET CIDS AND PERFORMED OPS TEST EMERGENCY POWER SUPPLY SYSTEM TEST OK.
CABIN PRESSURE LIGHT AND LENS BROKEN AT THE L2 DOOR. SECURED THE LENS. OK FOR SERVICE.
DURING APPROACH, AUTO THRUST ON, UNCOMMANDED SPEED WITH INCREASE TO +20, AUTO THRUST DISENGAGED. APPROXIMATELY 30 SECONDS LATER BOTH ENGINES EXCEEDED EGT LIMIT (EST OF 600) WITH ECAM MESSAGE. MAINTENANCE FOUND GAS PATH REPORT WITHIN LIMTS IAW 77-00-00-810. PERFORMED AUTOTHRUST DISAGREE IAW TSM 22-31-00-810-813A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
FOUND THE FLOOR LEVEL EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS .
SEAT 21F SEAT BACK WILL NOT STAY UP. MAINTENANCE TIGHTENED ROW 21F SEAT BACK ATTACH BOLTS IAW CMM 25-22-50.
UNABLE TO ARM L4 DOOR. MAINTENANCE INSPECTED AND REMOVED ICE FROM GIRT BAR IAW AMM 52-13-00.
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED DURING TAKEOFF ROLL (APROXIMATELY68 KNOTS) RECEIVING THRUST LEVEL NOT SET WARNING ALONG WITH A LANDING GEAR SYSTEM DISAGREE MESSAGE. THE CREW RETARDED THRUST LEVERS, EXITED THE RUNWAY AND RETURNED TO THE GATE. (THE AUTO BRAKE DID NOT ENGAGE (BELOW) 72 KNOTS. MAINTENANCE ACCOMPLISHED TSM 76-11-00-810-819 ENGINE THRUST LEVERS NOT SET AT CORRECT POSITION FLEX TEMP. TCU TEST PASSED, AS PER NOTE, NO MAINTENANCE ACTION IS NECESSARY AT THIS TIME. IN ADDITION MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-888 OF LANDING GEAR SYSTEM DISAGREE TEST PASSED, TSM 31-32-00-860-009 NO FAULTS NOTED ON SYSTEM REPORT TEST.
AIRCRAFT WAS NOT GROUNDED. MISSING EMERGENCY LIGHT RED LENS COVER AT SEAT 8C. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 8C PER AMM 33-51-18.
AIRCRAFT WAS NOT GROUNDED. MISSING EMERGENCY LIGHT RED LENS COVER AT SEAT 9D. EMERGENCY LIGHT ASSEMBLY AT SEAT 9D PER AMM 33-51-18.
AIRCRAFT WAS NOT GROUNDED. BROKEN LOWER EMERGENCY LIGHT COVER AT DOOR 4L. REPLACED LIGHT COVER.
CIDS PANEL SHOW 3L/3R DOOR PRESSURE. 3L/3R SLIDE PRESSURE IND INOP ON FAP PANEL. THE AIRCRAFT WAS NOT GROUNDED. REPLACED DEU B 300RH6 IAW AMM 23-73-47. OPS CHECKED GOOD.
4 LT SEAT AREA EXIT LIGHT COVER MISSING. INSTALLED LENS COVER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.
A CHECK FWD GALLEY FLOOR PANEL 222EF IS DELAMINATED. REPAIRED IAW SRM 53-12-00-201 FIGURE 2.
DURING WEEKLY CHECK FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 30ABC. UFI, FOUND CONNECTOR DISCONNECTED FROM CAIN WALL. RECONNECTED, OPERATIONS CHECKED NORMAL.
FORWARD JUMP SEAT EXIT LIGHT COVER BROKEN FROM BRACKET. INSTALLED NEW LENS COVER, OK FOR SERVICE.
EMERGENCY EXIT LIGHT AT ROW 30 LT IS INOPERATIVE. CONNECTED & STOWED ELECTRICAL LEAD.
SEAT MOUNTED EMER EXIT LIGHT LENS BROKEN AT L2 DOOR. REPLACED LIGHT ASSEMBLY & OPERATIONS CHECKED NORMAL.
4R DOOR EMERGENCY EXIT LENS COVER MISSING. REPLACED MISSING EMER EXIT LENS AT DOOR 4R.
CREW REPORTED THE FLOOR LEVEL EMERGENCY LIGHT COVER BROKEN AT ROW 10. INSTALLED LENS ASSEMBLY.
DOOR L2 CHECK DOOR PRESS LIGHT ILLUMINATED. FOUND L2 DOOR DAMPNER EMERGENCY OPERATION CYLINDER LEAKING PRESS. REPLACED DOOR L2 DAMPNER CYLINDER IAW AMM 52-22-14-400-001-A.
TSI ISSUED, DUE TO PILOT REPORTS OF SEVERAL CHECK DOOR 2L PRESS MESSAGES. FOUND SCHRADER VLV ON DOOR 2L DAMPENER TO BE LEAKING. REPLACED SCHRADER VLV, OPERATIONS & LEAK CHECKED GOOD. BITE TEST GOOD IAW AMM 23-73-00-740-005.
L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.
2L DOOR WHITE PRESS LIGHT ILLUMINATED. SERVICED DOOR DAMPER ASSIST BOTTLE IAW AMM 52-10-00-614-001-A. NO LEAKS DETECTED.
PREPARING FOR PUSH BACK, FLIGHT ATTENDANT REPORTED AFTER ALL DOORS ARMED, CIDS PANEL INDICATED LOW DOOR PRESS ON 2L DOOR. SERVICED 2L DOOR ASSIST BOTTLE IAW AMM 25-02-49-040, OK FOR SERVICE.
2L DOOR ASSIST BOTTLE LOW PRESS. SERVICED 2L DOOR ASSIST BOTTLE IAW A321AMM 52-10-00-614-001-A.
2L DOOR ASSIST BOTTLE LOW PRESS. SERVICED 2L DOOR ASSIST DAMPER IAW AMM 52-22-000614-002-A.
THE 3R DOOR SLIDE DOES NOT SHOW ARMED. R & R INFLATION RESERVOIR, ESCAPE SLIDE INFLATION, IAW AMM 25-63-49-400-001A.
FLOOR LEVEL EMERGENCY EXIT LIGHT AT FLOOR LEVEL ROW ROW 22 ACFT RT MISSING LENS COVER. REPLACED LIGHT.