N977UY
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARMING HANDLE LOOSE. MAINTENANCE TIGHTENED 3R DOOR ARMING LEVER HANDLE PER AMM 52-22-22.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 2R DOOR DISARM HANDLE LOOSE. MAINTENANCE SECURED ARM/DISARM HANDLE PER AMM 25-23-46.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3R DOOR DISARM HANDLE LOOSE. MAINTENANCE SECURED ARM/DISARM HANDLE PER AMM 25-23-46.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3L DOOR DISARM HANDLE LOOSE. MAINTENANCE SECURED ARM/DISARM HANDLE PER AMM 25-23-46.
AIRCRAFT WAS GROUNDED: L1 DOOR SUPPORT ARM PIN DAMAGED WHERE IT ATTACHES TO THE DAMPER AND EMERGENCY OPERATION CYLINDER. REPLACED PIN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-11-14.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT JUMPSEAT 4L FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 10WL DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 11WL DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: EXIT DOOR 3L ARMING HANDLE LOOSE. MAINTENANCE TIGHTENED DOOR ARM HANDLE MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-20-00.
AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARM LEVER REPORTED LOOSE. REPLACED 3R DOOR ARMING LEVER / HANDLE PER AMM 52-22-22. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS IN BASE MAINTENANCE: DID NOT PASS OPERATIONAL TEST OF EMERGENCY POWER SUPPLY UNITS BY BUILT IN TEST EQUIPMENT CHECK. PERFORMED FAULT CONFIRMATION AND FAULT ISOLATION PER TSM 33-51-00-810-822-A AND REPLACED POWER-EMERGENCY SUPPLY (10WL) PER AMM 33-51-38-400-001-A.
AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23 LEFT BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM LOCATED BETWEEN FR 64 AND FR 66 AT +Y765 REPLACED FLOOR BEAM PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON JOINT COVER LOCATED AT LEVEL -Y81 BETWEEN FR 12 AND FR 16 IN FORWARD GALLEY AREA. REPLACED JOINT COVER PER SRM 51-72-11-911-001.
AIRCRAFT WAS IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM LOCATED AT +Y1292 AND AT LEVEL FR 16 IN FORWARD GALLEY AREA. REPLACED FLOOR BEAM PER SRM 51-72-11-911-001.
AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23R BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 66 AND +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.
QC REVIEWED THIS EVENT AND DETERMINED THAT THIS WAS NOT CPCP RELATED AND NOT A LEVEL 2 FINDING. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY. AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FRAME 71 ANGLE LOCATED BETWEEN STR 26 AND STR 31. REPLACED WITH NEW ANGLE PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME 71 ANGLE LOCATED BETWEEN STR 26 AND STR 31. REPLACED WITH NEW ANGLE PER SRM 51-42-11-801.
AIRCRAFT IN BASE MAINTENANCE: CORROSION IN FORWARD MAIN CABIN AREA ON RIGHT SEAT TRACK AT FR 20 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-15-11.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-13.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3R DOOR ARMING HANDLE IS LOOSE. SECURED ARM AND DISARM 3R DOOR YELLOW SQUARE HANDLE PART.
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN. LATCHING MECHANISM NOT MOVING WITH HANDLE. REMOVED AND REPLACED LATCHING MECHANISM.
AIRCRAFT WAS NOT GROUNDED: ROW 30 IN SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED IN SEAT EMERGENCY LIGHTS AT ROW 30 PER AMM 33-51-19.
AIRCRAFT WAS NOT GROUNDED: ROW 31 IN SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED IN SEAT EMERGENCY LIGHTS AT ROW 31 PER AMM 33-51-19.
AIRCRAFT WAS NOT GROUNDED: 3L SLIDE LEVER LOOSE. SECURED HANDLE.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THAT THE 3R DOOR ARMING LEVER IS LOOSE. MAINTENANCE ADJUSTED 3R DOOR HANDLE.
AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARMING LEVER IS LOOSE. SECURED DOOR ARMING LEVER ON 3R DOOR.
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS FLOOR SOFT AND POPS WHEN STEPPED ON AT SEAT ROW 19. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS FLOOR SOFT AND POPS WHEN STEPPED ON AT SEAT ROW 19. **SUPPLEMENTAL REPORT FOR AALA202306080309: REPLACED CENTER AILSE FLOOR PANEL AT SEAT ROW 19 PER AMM 53-00-00** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: #3 EMERGENCY FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED FLASHLIGHT PER AMM 33-51-19.
AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ILLUMINATED DURING CRUISE FOR 5 SECONDS. MAINTENANCE INSPECTED LAVATORY PER AMM 25-40-00 WITH NO FAULTS NOTED.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AT SEATS/ROW 11, 12, 13 A-C INOPERATIVE UPON INSPECTION. MAINTENANCE RE-SECURED WIRE CONNECTOR LOCATED ON FLOOR AT SEAT 12A, AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: MIDDLE LAVATORY DOOR JAMMED. RE-SECURED DOOR MID LAVATORY AND OPERATIONS CHECK PER AMM 25-45-19.
AIRCRAFT WAS NOT GROUNDED: DOOR R3 ARMING LEVER LOOSE. SECURED DOOR ARMING LEVER AS REQUIRED.
AIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001
AIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR PINTLE PIN WORN. REPLACED PINTLE PIN PER TASK CARD 26T00032001
AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY DOME LIGHT ABOVE LAST ROW IS INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202204229801: REPLACED LIGHT PER AMM 33-51-11. OPERATIONAL CHECK GOOD.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY DOME LIGHT ABOVE LAST ROW IS INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS GROUNDED: AT TOP OF DESCENT WE GOT AN ECAM MESSAGE FOR ENGINE 2 BLEED AIR LEAK PERFORMED PROCEDURE LEFT PACK COULD NOT HOLD CABIN PRESSURE AND CABIN WENT TO 10,000 FEET. REPLACED #2 ENGINE OVER PRESSURE VALVE AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 36-11-53-400.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR, # 6 HINGE BOLT RETAINER CRACKED. CUT OFF DAMAGED TAB LUG WITH ADJACENT TAB AND INSTALLED REPAIR ANGLE PER SRM 55-26-41-A.
AIRCRAFT IN BASE MAINTENANCE: SEAT ROW 5FD THE OXYGEN RELEASE PIN EYELET WAS NOT CLOSED AS INSTRUCTED BY ECO/AMM REFERENCES. CRIMPED OXYGEN GENERATOR FIRING PIN WITH OXYGEN MASK LANYARDS ATTACHED AT SEAT ROW 5FD PER AMM 35-21-42-400-001-A AND AMM 35-21-43-400-001-A
AIRCRAFT IN BASE MAINTENANCE: SEAT ROW 32DEF THE OXYGEN RELEASE PIN EYELET WAS NOT CLOSED AS INSTRUCTED BY ECO/AMM REFERENCES. CRIMPED OXYGEN GENERATOR FIRING PIN WITH OXYGEN MASK LANYARDS ATTACHED AT SEAT ROW 32DEF PER AMM 35-21-42-400-001-A AND AMM 35-21-43-400-001-A
AIRCRAFT IN BASE MAINTENANCE: SEAT ROW 2FD THE OXYGEN RELEASE PIN EYELET WAS NOT CLOSED AS INSTRUCTED BY ECO/AMM REFERENCES. CRIMPED OXYGEN GENERATOR FIRING PIN WITH OXYGEN MASK LANYARDS ATTACHED AT SEAT ROW 2FD PER AMM 35-21-42-400-001-A AND AMM 35-21-43-400-001-A
AIRCRAFT IN BASE MAINTENANCE: L2 DOOR DAMPER ASSIST CYLINDER PRESSURE LOW. SERVICED CYLINDER PER AMM 52-10-00-614-001-A.
AIRCRAFT IN BASE MAINTENANCE: L3 DOOR DAMPER ASSIST CYLINDER PRESSURE LOW. SERVICED CYLINDER PER AMM 52-10-00-614-001-A.
AIRCRAFT WAS NOT GROUNDED # 1 OVEN VENT FAN - FORWARD GALLEY NOISY ALSO "PLASTIC" ODOR COMING FROM THE OVEN, **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED # 1 OVEN VENT FAN - FORWARD GALLEY NOISY ALSO "PLASTIC" ODOR COMING FROM THE OVEN, **SUPPLEMENTAL REPORT FOR AALA202111238914: REPLACED FORWARD GALLEY #1 OVEN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-35-19.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISES DOOR 3R ARMING LEVER IS LOOSE. SECURED 3R ARMING HANDLE PER AMM 52-22-00.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS ARMING LEVER AT 3L/R LOOSE. TIGHTENED SCREW ON ARMING HANDLE TAB ON 3L/R USING STANDARD MAINTENANCE PRACTICES.
AIRCRAFT WAS GROUNDED: FOUND SLIDE PACK AFT MOUNTING STUD / QUICK RELEASE PIN PULLED THOUGH COMPOSITE. / BROKEN REPLACED MOUNT STUD / QUICK RELEASE PIN PER AMM 25-62-44 AND AMM 25-62-00.
AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER IS NOT SECURE AND LOOSE. TIGHTENED HARDWARE ON ARMING LEVER AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: APU FIRE BOTTLE DISCHARGE LIGHT CAME ON DURING FLIGHT AND LIGHT EXTINGUISHES UPON LANDING. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: APU FIRE BOTTLE DISCHARGE LIGHT CAME ON DURING FLIGHT AND LIGHT EXTINGUISHES UPON LANDING. REPLACED ENGINE / APU FIRE PANEL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-12-00.
AIRCRAFT WAS NOT GROUNDED: APU AGENT DISCHARGE LIGHT ON OVERHEAD PANEL ILLUMINATED IN CRUISE AND WENT OUT ON LANDING. MAINTENANCE VERIFIED THAT THE BOTTLE HAD NOT DISCHARGED AND INDICATED GOOD. A SATISFACTORY OPERATIONAL CHECK OF THE APU FIRE TEST SYSTEM WAS ACCOMPLISHED WITH NO DEFECT NOTED PER AMM 26-13-00.
AIRCRAFT WAS GROUNDED: 1L DOOR SLIDE DOES NOT STAY ARMED. ACCOMPLISHED L1 DOOR SLIDE REPLACEMENT PER JOB CARD 26L00025010.
AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, EMERGENCY POWER SUPPLY UNIT 15WL FAULTED. REPLACED BATTERY PER AMM 33-51-38-000-002-A, 33-51-38-400-002-A AND 33-51-00-710-001-A.
AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, EMERGENCY POWER SUPPLY UNIT 14WL FAULTED. REPLACED BATTERY PER AMM 33-51-38-000-002-A, 33-51-38-400-002-A AND 33-51-00-710-001-A.
AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF EMERGENCY LIGHTS, EMERGENCY POWER SUPPLY UNIT 12WL FAULT. REPLACED BATTERY PER AMM 33-51-38-000-002-A, 33-51-38-400-002-A AND 33-51-00-710-001-A.
AIRCRAFT IN BASE MAINTENANCE: WHILE PERFORMING OPERATIONAL TEST OF ESCAPE - L1 DOOR FAILED. CLEANED L1 DOOR MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-10-00-100-801-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT SEAT TRACK Y-765 AND FR20. ACCOMPLISHED SEAT TRACK SPLICE REPAIR IAW A321 SRM 53-11-15-300-008.
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON L4 DOOR SILL BEAM AT FR68, BUTT LINE Y-1500. REPAIRED WITH NESTED ANGLE REINFORCEMENT PER EA 328360.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR SILL BEAM AT FR68 AND RBL -Y1500. REPAIRED PER SRM 53-41-14-300-001 AND EA 328360.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAILED AT LOCATION 10WL DURING PS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 10WL PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAILED AT LOCATION 13WL DURING PS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 13WL PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAILED AT LOCATION 15WL DURING PS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 15WL PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAILED AT LOCATION 11WL DURING PS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 11WL PER AMM 33-51-38.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAILED AT LOCATION 14WL DURING PS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 14WL PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: AUXILIARY POWER UNIT DISCHARGE LIGHT ON DURING CRUISE. OPERATIONS TEST OF AUXILIARY POWER UNIT FIRE AND OVERHEAT DETECTION SYSTEM, PER AMM 26-13-00-710-001-A. ACCOMPLISHED AUXILIARY POWER UNIT FIRE DETECTION UNIT TEST PER AMM 26-13-34-710-051-A. OPEN AUXILIARY POWER UNIT COMPARTMENT AND CHECK AUXILIARY POWER UNIT AND CHECKED AUXILIARY POWER UNIT FIRE DETECTION LOOPS, NO DEFECTS FOUND.
AIRCRAFT WAS NOT GROUNDED: APU AGENT DISCHARGE LIGHT ILLUMINATED. MEL AUTHORIZED. ACCOMPLISHED BITE AND OPS TEST OF APU FIRE PROTECTION SYSTEM PER AMM 26-22-00-710-004A. NO DEFECTS NOTED.
AIRCRAFT WAS NOT GROUNDED: APU DISCHARGE LIGHT ILLUMINATED. PERFORM OPERATIONAL TEST OF APU FIRE EXTINGUISHER LOP/SQUIB IAW AMM 26-22-00-710-001-A. NO FAULTS NOTED. MEL REMOVED.
AIRCRAFT WAS GROUNDED: APU AGENT DISCHARGE LIGHT ILLUMINATED WITH APU RUNNING. ACCOMPLISHED TSM 26-22-00-810-806-A. REMOVED AND REPLACED APU FIRE BOTTLE EXTING 11WF IAW AMM 26-22-41.
AIRCRAFT WAS NOT GROUNDED. R4 FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. REPLACE BATTERY ON R4 FLASHLIGHT.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY WHITE LIGHT AT 20C INOPERATIVE. FOUND CONNECTOR OFF AT SIDEWALL, RECONNECTED OPERATIONS CHECKS NORMAL, PER AMM 33-51-00.
AIRCRAFT WAS NOT GROUNDED. DOOR 3R INTERIOR ARMING HANDLE LOOSE. SECURED ARM/DISARM OUTER HANDLE, PER AMM 52-22-22.
AIRCRAFT NOT GROUNDED - L4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L4 DOOR ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT NOT GROUNDED - EMERGENCY FLASHLIGHT INOPERATIVE, RIGHT FORWARD FLIGHT ATTENDANT POSITION. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-65-00.
AIRCRAFT WAS NOT GROUNDED: LEFT EMERGENCY LIGHT LENS BROKEN ON SEAT. MAINTENANCE REPLACED LIGHT PER AMM 33-51-19.
AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO CLT DUE TO THE #2 ENGINE FAILURE / COMPRESSOR STALL AND EGT OVER TEMPERATURE 5 MINUTES AFTER TAKE OFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED #2 ENGINE ASSY IAW J/C 26L40071004 DUE TO 7TH STAGE BLADE FAILURE.
AIRCRAFT WAS NOT GROUNDED: 4R DOOR FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-65-00.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT L1 DOOR INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-65-00.
RIGHT ELEVATOR NR 1 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.
LEFT ELEVATOR NR 1 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.
THE LEFT ELEVATOR NR 2 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.
LEFT ELEVATOR NR 3 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.
RIGHT ELEVATOR NR 2 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.
RIGHT ELEVATOR NR 3 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.
SEAT ROW 34 ABC SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. FOUND A WIRE BROKEN AT THE WALL CONNECTOR. TERMINATED THE WIRES IAW ESPM 20-44-11, AND AWM 33-51-08. R & R THE EPSU AT 15WL IAW AMM 33-51-38. OPS TESTED GOOD.
PASSENGER DOOR UPPER CORNER PLATE, AFT POSITION, INNER SKIN WORN. REPLACED THE UPPER PLATE IAW SRM 51-72-11-001
CORROSION FOUND ON THE LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-400-001-A.
CORROSION ON AFT GALLEY LEFT LOWER SILL, BETWEEN FRAMES 66 AND 68. REPLACED THE SILL IAW SRM 51-72-11.
CORROSION ON THE TORQUE LINK UPPER AND LOWER FITTING BORE, ON THE NOSE LANDING GEAR. REPLACED THE NOSE LANDING GEAR ASSEMBLY IAW JC 26L71032003.
AIRCRAFT IN BASE MAINTENANCE: DEFORMED ESCAPE SLIDE PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA. MAINTENANCE REPLACED ESCAPE SLIDE PER AMM 25-62-44-400-802-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
THE AIRCRAFT IS IN BASE MAINTENANCE. DEFORMED SLIDE PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACED SLIDE PASSENGER CREW DOOR 832 AT AFT GALLEY AREA PER AMM 25-62-44-400-006-A.
DELAMINATION FOUND ON FLOOR PANEL 152RG, BETWEEN FRAMES 50 - 53. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, IRM 9701, REVISION I, AND DRAWING D53674094.
A CRACK WAS FOUND ON THE LOWER SKIN, OTBD FIXED LEADING EDGE RIB 15 ON THE RT WING. REPAIRED THE SKIN IAW SRM 57-41-11-300-013, AND DRAWING D574-59073.
CORROSION FOUND ON THE AFT GALLEY, LEFT LOWER SILL, CENTER FITTING BETWEEN FRAMES 66 AND 68. REPLACED THE FITTING IAW SRM 51-72-11.
LEFT FORWARD HINGE BEARING OF MAIN LANDING GEAR DOOR WAS LOOSE. REPLACED THE HINGE IAW SRM 51-44-11-001.
AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON INBOARD FLAP TAB LOCATED AT STA RIB 4 TO RIB 6. REPAIRED INBOARD FLAP TAB ON RIGHT HAND WING PER EA 287340.
CORROSION WAS FOUND ON THE LOWER SILL FRAME 62, STRINGER 38R IN THE BULK CARGO BAY. REPAIRED THE SILL IAW SRM 53-41-49-300-003.
SHEAR PLATE FOUND CRACKED AT FRAMES 69 TO 70, STRINGER 23L. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DWG D5347112420200.
CRACK INDICATION FOUND ON THE SHEAR PLATE BETWEEN FRAMES 69-70, STRINGER 23R IN THE AFT GALLEY AREA. REPLACED SHEAR PLATE IAW SRM 51-72-11.
CORROSION FOUND ON THE LOWER SILL BETWEEN FRAMES 66 - 68, STRINGER 23R, IN THE AFT GALLEY. REPLACED THE LOWER SILL IAW SRM 51-72-11, AND DRAWING D53480505.
DELAMINATION FOUND ON FLOOR PANEL 131EF, FRAMES 28 - 31, Y765 TO -Y765 IN THE FORWARD CARGO COMPARTMENT. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, PARA 2, FIGURE 20109, AND IRM 9701 REV I.
FORWARD GALLEY FLOOR PANEL 222EF DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLOOR PANEL.
AIRCRAFT WAS GROUNDED. FORWARD GALLEY FLOOR PANEL 221EF WAS DELAMINATED AFT OF FLIGHT DECK DOOR. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801A.
CORROSION FOUND ON THE SEAT TRACK AT FRAME 16, Y+254. THE AIRCRAFT WAS GROUNDED. REPLACED THE SEAT TRACK IAW 51-42-11.
CORROSION FOUND ON THE SEAT TRACK AT FRAME 16, Y-254. THE THE AIRCRAFT WAS GROUNDED. REPLACED THE SEAT TRACK.
CORROSION FOUND ON THE FORWARD GALLEY SEAT TRACK AT FRAME 16, Y-1292. THE AIRCRAFT WAS GROUNDED. REPAIRED THE SEAT TRACK IAW EA 285569.
L4 DOOR, EMERGENCY EXIT LIGHT MISSING THE LENS. MAINTENANCE INSTALLED THE LENS IAW AMM 33-51-13-400-001-A, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AFT CARGO FLOOR PANEL 151PF SPONGY. REPLACED AFT CARGO FLOOR PANEL IAW AMM 53-42-00.
R4 DOOR, FORWARD CIDS PANEL INDICATED CHECK SLIDE PRESSURE. REMOVED AND REPLACED THE SLIDE IAW JC 26L00025010 AND REPLACED THE L1 EMERGENCY LIGHT BATTERY PACK IAW MM 33-51-38. SYSTEM CHECKED GOOD.
ARMING LEVER ON THE R3 DOOR IS LOOSE. SECURED THE HANDLE. OPS CHECKED OK.
SEAT 22 LEFT, MOUNTED EMERGENCY LIGHT FOUND BROKEN. REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-51-18.
AIRCRAFT GROUNDED. CENTER AISLE FLOOR PANEL 241AF AT ROW 13 SOFT AND SPONGY. REPLACED CABIN FLOOR PANEL 241AF AT ROW 13 AS PER SRM TASK #53-32-12-400-002 CHECK GOOD. AIRCRAFT OK FOR SERVICE.
EMERGENCY LIGHT LENS MISSING AT THE R3 DOOR. INSTALLED A LENS.
AIRCRAFT WAS GROUNDED: GREEN ENGINE 1 PUMP FAILURE AFTER POWER REDUCTION ON TAKEOFF, AN EMERGENCY WAS DECLARED, THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY AND WAS TOWED TO THE GATE. **SUPPLEMENTAL REPORT TO UPDATE SECTIONS 4 AND 5. MAINTENANCE REPLACED PUSH BUTTON SWITCH PER ESPM 20-45-17. (SEE ALSO AALA201709069005 AND AALA201709089015)
AIRCRAFT WAS GROUNDED: GREEN ENGINE 1 PUMP FAILURE AFTER POWER REDUCTION ON TAKEOFF, AN EMERGENCY WAS DECLARED, THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED PRESSURE SWITCH 1074GK PER AMM 29-11-17. (CLOSED) SEE ALSO AALA201709089014 (PUSHBUTTON SWITCH) AND AALA201709089015 (WIRE)
AIRCRAFT WAS GROUNDED: GREEN ENGINE 1 PUMP FAILURE AFTER POWER REDUCTION ON TAKEOFF, AN EMERGENCY WAS DECLARED, THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE FOUND BROKEN WIRES (8P057 AND 8P073) TO CONNECTOR 107(4)GK-A AND REPLACED PER AMM 70-71-24. (SEE ALSO AALA201709069005 AND AALA201709089014)
AIRCRAFT WAS GROUNDED. DELAMINATION ON AFT CARGO FLOOR PANEL 151MK. REPLACED CARGO FLOOR PANEL PER AMM 53-42-14.
AIRCRAFT WAS GROUNDED. DELAMINATION ON AFT CARGO BIN FLOOR PANEL 151LF. REPLACED CARGO FLOOR PANEL PER AMM 53-42-14.
AIRCRAFT WAS GROUNDED. DELAMINATION ON AFT CARGO FLOOR PANEL 151GF. REPLACED CARGO FLOOR PANEL PER AMM 53-42-14.
EXIT LIGHT COVER NEAR THE L4 DOOR SLIDE BUSTLE IS MISSING. INSTALLED EXIT LIGHT LENS COVER AT 4L DOOR IAW AMM.
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. RETURNED TO CLT. ENGINE 1 HYDRAULIC PUMP LOW PRESSURE ON CLIMB OUT. NO SYSTEM LOSS. OVER WEIGHT LANDING ACCOMPLISHED IN CLT 182.7 LBS/FLAPS FULL/100 FPM VERTICAL SPEED AT TOUCHDOWN. MAINTENANCE REPLACED HYDRAULIC PRESSURE TRANSDUCER (1065GN). ACCOMPLISHED SATISFACTORY LEAK CHECK AND OPERATIONAL CHECK PER MM 29-32-11.
AIRCRAFT WAS GROUNDED. DIVERTED TO MCO. EMERGENCY DECLARED. FLIGHT CREW REPORTED FAILURE OF NR 1 HYDRAULIC GREEN PUMP INFLIGHT AND LOSS OF GREEN SYSTEM PRESSURE. ACCOMPLISHED TSM 29-11-00-810 FOR LOSS OF PRESSURE NR 1 PUMP. REMOVED AND REPLACED CASE DRAIN FILTER IAW 29-11-43 WITH NO DEBRIS FOUND. REMOVED AND REPLACED NR 1 PUMP IAW 29-11-31. ACCOMPLISHED OPERATIONAL TEST IAW AMM 29-11-00 AND 29-11-51. LEAK CHECK GOOD. SYSTEM CHECKS NORMAL.
R4 DOOR EXIT LIGHT LENS BROKEN. REPLACED EMERGENCY LIGHT LENS.
FIVE EMERGENCY EXIT ROW LIGHTS WERE INOPERATIVE WHEN TESTED. TROUBLESHOT AND FOUND EPSU 11WL FAULTED , REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-51-38-000-001-A.
FIVE EMERGENCY EXIT ROW LIGHTS WERE INOPERATIVE WHEN TESTED. TROUBLESHOT AND FOUND THE EPSU 11WL FAULTED, REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 11WL IAW AMM 33-51-38-000-001-A.
AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED EMERGENCY LIGHT LENS ON R1 DOOR AS REQUIRED.
CREW REPORT THE L4 DOOR SHOWS LOW PRESSURE. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00. AIRCRAFT WAS GROUNDED.
L4 DOOR SHOWING LOW DOOR PRESSURE. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00. AIRCRAFT WAS GROUNDED.
L4 DOOR CYLINDER HAS PREVIOUS HISTORY FOR REQUIRING SERVICING. REPLACED DOOR DAMPER DIAPHRAGM PER AMM 32-22-00-860-002-A. NO LEAKS NOTED. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT #1 STATUS DISPLAY INDICATES CHECK DOOR PRESSURE AT 4L DOOR. MAINTENANCE SERVICED 4L DOOR ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. 4 L DOOR INDICATES NOT ARMED AT DOOR. ECAM UP FRONT INDICATES NORMAL MAINTENANCE SERVICED L4 DOOR ASSIST BOTTLE PER MM 52-10-00.
AIRCRAFT WAS GROUNDED. BROKEN SLIDE ARM-DISARM LEVER AT DOOR 3R. MAINTENANCE REPLACED ARM-DISARM UNIT PER AMM 52-22-22.
AIRCRAFT WAS NOT GROUNDED. WHEN 4L DOOR CLOSED, FORWARD FLIGHT ATTENDANT MONITOR SAYS CHECK DOOR PRESSURE. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. DOOR 4L PRESSURE LOW. MAINTENANCE SERVICED DOOR 4L ASSIST BOTTLE PER AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. CIDS CAUTION ON FLIGHT ATTENDANT PANEL FOR DOOR 4L SERVICED 4L DOOR ASSIST BOTTLE PER 52-10-00.
AIRCRAFT WAS NOT GROUNDED: DOOR BOTTLE AFT 4L LOW PRESSURE. SERVICED DOOR ASSIST BOTTLE AT DOOR 4L PER AMM 52-10-00.
CIDS PANEL DISPLAYED AN AMBER WARNING CHECK L4 DOOR PRESSURE WARNING. SERVICED THE L4 DOOR ASSIST BOTTLE IAW AMM 52-10-00.
FLIGHT ATTENDANT CIDS PANEL MESSAGE FOR L4 DOOR BOTTLE LOW. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.
FORWARD FLIGHT ATTENDANT PANEL SHOWS L4 DOOR LOW PRESSURE. SERVICED DOOR ASSIST BOTTLEAND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
L4 DOOR PRESSURE LOW. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 12-14-00.
AFTER PUSHBACK, NR 1 FLIGHT ATTENDANT ADVISED THAT 4L DOOR LOW PRESSURE ANNUNCIATED ON FORWARD FLIGHT ATTENDANT PANEL. SERVICED L4 DOOR DAMPER IAW AMM 52-10-00.
CID SCREEN INDICATES CHECK DOOR PRESSURE AT THE L4 DOOR. MAINTENANCE SERVICED DAMPER AT L4 DOOR IAW AMM 52-10-00.
AIRCRAFT WAS NOT GROUNDED. MISSING AFT RIGHT EXIT DOOR LIGHT COVER. REPLACED LIGHT COVER.
AIRCRAFT WAS NOT GROUNDED. MISSING AFT LEFT EXIT DOOR LIGHT COVER. REPLACED LIGHT COVER.
SOFT FLOORBOARD IN THE FORWARD ENTER WAY INTO THE CABIN. AIRCRAFT WAS GROUNDED. REPLACED FORWARD ENTRY WAY FLOORBOARD IAW TASK 53-12-12-0401.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT LIGHT COVER LENS CRACKED AT SEAT 10C. R & R EMERGENCY SEAT LIGHT ASSY AT SEAT 10C IAW CMM 25-22-50. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.
ACFT WAS NOT GROUNDED, DURING TAKEOFF AN ECAM MESSAGE REFLECTING AUTOFLIGHT, AUTOTHRUST FAULTS APPEARED AND THE CREW ABORTED THE TAKEOFF AT APPROXIMATELY 80 KNOTS AND RETURNED TO THE GATE WITH NO ADDITIONAL INCIDENTS. MAINTENANCE WAS UNABLE TO DUPLICATE, NO PFR FAULTS WERE NOTED. AN ACCOMPLISHED SATISFACTORY LANDING CONFIDENCE CHECK WAS ACCOMPLISHED IAW AMM-22-97-00 WITH NO FAULTS BEING NOTED.
AIRCRAFT WAS NOT GNDED. FORWARD CARGO FLOOR PANEL 131AF DELAMINATED. REPLACED FLOOR PANEL 131AF IAW AMM 53-22-14.
AIRCRAFT WAS NOT GNDED. DISARMING LEVER AT 3R LOOSE. SECURE 3R DOOR ARMING LEVER.
DIVERTED & ACFT WAS GNDED. VENT EXTRACT FAULT. RUMBLE & BURNT BEARING SMELL WAS NOTED DURING FLIGHT. CREW DECLARED AN EMER & DIVERTED WHERE THE ACFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE EXTRACT FAN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-51.
AIRCRAFT WAS NOT GNDED. EMER LIGHT LENS MISSING AT SEAT 3L. REPLACED EMER LIGHT AT SEAT 3L IAW AMM 33-51-00.
FLIGHT ATTENDANTS REPORT, R3 DOOR ARMING LEVER IS LOOSE. SECURED LOOSE ARMING LEVER. OPERATIONAL CHECKED GOOD.
AIRCRAFT WAS NOT GNDED. NR 1 FUEL PUMP RT WING FAULTED AFTER TAKEOFF. LOW PRESS INDICATED ON FUEL ECAM PAGE. REPLACED RT WING NR 1 FUEL PUMP. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 28-21-51.