N173US

Part: WARNING MESSAGE — ILLUMINATED (ZONE 700) · airframe 79,710 hrs · 30,857 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE FLIGHT CREW REPORTING ECAM MESSAGES FOR BRAKES-AUTO BRAKE FAULT AND BRAKE RELEASED. THE AIRCRAFT LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. (OPEN)

Part: DRIVE SHAFT — DEFECTIVE (ZONE 700) · airframe 79,710 hrs · 30,857 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE FLIGHT CREW REPORTING ECAM MESSAGES FOR BRAKES-AUTO BRAKE FAULT AND BRAKE RELEASED. THE AIRCRAFT LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202512297475 SUBMITTED ON 12/29/2025 BY TUL: MAINTENANCE REPLACED THE #2 WHEEL TACHOMETER 21GG, #2 WHEEL TACHOMETER DRIVE SHAFT (AALA202601057381), AXLE HARNESS 1M (AALA202601059757) AND THE BRAKE STEERING CONTROL UNIT (AALA202601052776). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO DEFECTS OR FAULTS NOTED.

Part: LANDING GEAR — FAULT MESSAGE (ZONE 100) · airframe 79,710 hrs · 30,857 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE FLIGHT CREW REPORTING ECAM MESSAGES FOR BRAKES-AUTO BRAKE FAULT AND BRAKE RELEASED. THE AIRCRAFT LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202512297475 SUBMITTED ON 12/29/2025 BY TUL: MAINTENANCE REPLACED THE #2 WHEEL TACHOMETER 21GG, #2 WHEEL TACHOMETER DRIVE SHAFT (AALA202601057381), AXLE HARNESS 1M (AALA202601059757) AND THE BRAKE STEERING CONTROL UNIT (AALA202601052776). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO DEFECTS OR FAULTS NOTED.

Part: TACHOMETER — WARNING MESSAGE (ZONE 700) · airframe 79,710 hrs · 30,857 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE FLIGHT CREW REPORTING ECAM MESSAGES FOR BRAKES-AUTO BRAKE FAULT AND BRAKE RELEASED. THE AIRCRAFT LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202512297475 SUBMITTED ON 12/29/2025 BY TUL: MAINTENANCE REPLACED THE #2 WHEEL TACHOMETER 21GG, #2 WHEEL TACHOMETER DRIVE SHAFT (AALA202601057381), AXLE HARNESS 1M (AALA202601059757) AND THE BRAKE STEERING CONTROL UNIT (AALA202601052776). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO DEFECTS OR FAULTS NOTED. ** (CLOSED)

Part: HARNESS — FAULT MESSAGE (ZONE 700) · airframe 79,710 hrs · 30,857 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE FLIGHT CREW REPORTING ECAM MESSAGES FOR BRAKES-AUTO BRAKE FAULT AND BRAKE RELEASED. THE AIRCRAFT LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202512297475 SUBMITTED ON 12/29/2025 BY TUL: MAINTENANCE REPLACED THE #2 WHEEL TACHOMETER 21GG, #2 WHEEL TACHOMETER DRIVE SHAFT (AALA202601057381), AXLE HARNESS 1M (AALA202601059757) AND THE BRAKE STEERING CONTROL UNIT (AALA202601052776). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO DEFECTS OR FAULTS NOTED.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 79,661 hrs · 30,837 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE INTERNAL DOUBLER BETWEEN FR 73 AND FR 74, BETWEEN S33L AND S33L. REPLACED DOUBLER PER SRM 51-72-11.

Part: SCREW — LOOSE (ZONE 800) · airframe 79,337 hrs · 30,701 cycles

AIRCRAFT WAS NOT GROUNDED: SCREW LOOSE ON 3L DISARM HANDLE. MAINTENANCE RE-SECURED LOOSE SCREW ON 3L DOOR DISARM HANDLE PER AMM 52-22-00.

Part: DOOR — STICKING (ZONE 800) · airframe 79,237 hrs · 30,661 cycles

AIRCRAFT WAS NOT GROUNDED: GATE AGENT SAYS L1 DOOR HARD TO OPEN, FEELS HEAVY. MAINTENANCE PERFORMED VISUAL INSPECTION AT THE PASSENGER ENTRY DOOR FOUND EXCESSIVE CORROSION COMPOUND AT THE HINGES, LUBE 3 POINTS OF CONTACT AT THOSE HINGES PINS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 79,126 hrs · 30,609 cycles

AIRCRAFT WAS GROUNDED: GATE AGENT REPORTS L1 DOOR DIFFICULT TO OPEN/MOVE. MAINTENANCE SERVICED L1 DOOR DAMPER AND ACCOMPLISHED LUBRICATION OF HINGE ARMS SUPPORT FITTINGS, DOOR OPERATES NORMAL NO DIFFICULTY NOTED OPERATING DOOR, OPS CHK GOOD IAW AMM 52-10-00 AND 12-22-52-640-016-A.

Part: TRIM PANEL — OUT OF POSITION (ZONE 800) · airframe 78,797 hrs · 30,477 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR CANNOT BE FULLY OPENED. MAINTENANCE FOUND THE L1 DOOR HINGE TRIM DAMAGED AND OUT OF POSITION, MAINTENANCE REPAIRED THE TRIM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE L1 DOOR WITH NO ISSUES NOTED.

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 78,368 hrs · 30,296 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD CABIN DOOR ECAM MESSAGE APPEARED AFTER TOUCHDOWN. AFTER EXITING RUNWAY AND SETTING BRAKES ECAM CLEARED ITSELF. **SUPPLEMENTAL REPORT FOR AALA202507147996: MAINTENANCE FOUND THE DETECTOR PROXIMITY SWITCH 11WLV2 OUT OF ADJUSTMENT AND ADJUSTED IT PER AMM 52-71-00. ** (CLOSED)

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 78,368 hrs · 30,296 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD CABIN DOOR ECAM MESSAGE APPEARED AFTER TOUCHDOWN. AFTER EXITING RUNWAY AND SETTING BRAKES ECAM CLEARED ITSELF. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: STRUT — FAULTED (ZONE 600) · airframe 78,357 hrs · 30,290 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO PHX DUE TO THE FLIGHT CREW REPORTING THAT UPON SELECTION OF FLAPS 2 AN ECAM MESSAGE FOR FLAPS LOCKED BETWEEN FLAPS 1 AND 2 ALONG WITH AN ALIGNMENT FAULT DISPLAYED. THE AIRCRAFT LANDED SAFELY AT PHX AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE ACCOMPLISHED TSM 27-51-00-810-818A, REPLACED THE RIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL TEST PER AMM 27-54-00-700-01 WITH NO FAULTS NOTED.

Part: HANDLE — LOOSE (ZONE 800) · airframe 78,229 hrs · 30,242 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ARM / DISARM HANDLE LOOSE ON 3L DOOR. MAINTENANCE TIGHTENED LOOSE 3L ARM/DISARM HANDLE PER AMM 52-21-00.

Part: RELAY — FAULTY (ZONE 800) · airframe 78,139 hrs · 30,202 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER CLOSING AIRCRAFT 1L DOOR, THERE WAS STILL A DOOR OPEN INDICATION ON THE DOOR SD SCREEN. MAINTENANCE REPLACED RELAY 12WN PER ESPM 20-46-50.

Part: WARNING LIGHT — ILLUMINATED (ZONE 800) · airframe 78,056 hrs · 30,172 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING 1L DOOR INDICATED OPEN WITH SLIDE ARMED. FLIGHT ATTENDANT CONFIRMED DOOR WAS CLOSED. ECAM CLEARED DURING TAXI TO GATE. **SUPPLEMENTAL REORT WILL BE SUBMITTED** (OPEN)

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 78,056 hrs · 30,172 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING 1L DOOR INDICATED OPEN WITH SLIDE ARMED. FLIGHT ATTENDANT CONFIRMED DOOR WAS CLOSED. ECAM CLEARED DURING TAXI TO GATE. MAINTENANCE ADJUSTED PROXIMITY SWITCH 13WV1 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-00.

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 78,010 hrs · 30,154 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FORWARD PASSENGER / CREW DOOR ECAM MESSAGE DISPLAYED DURING LANDING ROLL, INITIALLY STAYED ON FOR 2 SECONDS THEN DISAPPEARED. ECAM RETURNED AGAIN 3 SECONDS LATER, REMAINED ON FOR TAXI INTO GATE AND DID NOT SELF CLEAR. MAINTENANCE ADJUSTED DETECTOR PROXIMITY SENSOR 11WV1 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-00.

Part: COMPUTER — MALFUNCTIONED (ELAC) · airframe 77,513 hrs · 29,947 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA202504086274) AND 33CE4 (AALA202504080906) PER AMM 27-14-51. ALSO REPLACED THE #1 ELEVATOR AND AILERON COMPUTER (ELAC) PER AMM 27-93-34. (AALA202504087746) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CONTROL SERVO — MALFUNCTIONED (ZONE 600) · airframe 77,513 hrs · 29,947 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA202504086274) AND 33CE4 (AALA202504080906) PER AMM 27-14-51. ALSO REPLACED THE #1 ELEVATOR AND AILERON COMPUTER PER AMM 27-93-34. (AALA202504087746) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CONTROL SERVO — MALFUNCTIONED (ZONE 600) · airframe 77,513 hrs · 29,947 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA202504086274) AND 33CE4 (AALA202504080906) PER AMM 27-14-51. ALSO REPLACED THE #1 ELEVATOR AND AILERON COMPUTER PER AMM 27-93-34. (AALA202504087746) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WARNING HORN — INOPERATIVE (ZONE 800) · airframe 77,513 hrs · 29,946 cycles

AIRCRAFT IN BASE MAINTENANCE: EVACUATION ALARM AT DOOR 3L INOPERATIVE. REPLACED 3L DOOR LOUD SPEAKER FOR THE EVACUATION ALARM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER AMM 23-73-00-710-026-A.

Part: SPOILER — OUT OF ADJUST (ZONE 500) · airframe 77,513 hrs · 29,946 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING THE POST CHECK TEST FLIGHT THE FLIGHT CREW REPORTED THAT THE AIRCRAFT ROLLS LEFT WHEN SPOILERS DEPLOYED DURING TEST. MAINTENANCE FOUND THE SPOILERS 3 AND 4 ON THE LEFT WING AND SPOILERS 2, 3 AND 4 ON THE RIGHT WING OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE SPOILERS PER AMM 27-64-00-820-001-D.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 77,513 hrs · 29,946 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: PLATE — WORN (ZONE 500) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING SKIN LOWER SURFACE PYLON MOUNTING PLATE BETWEEN RIBS 7 AND 8 HAS ELONGATED / WORN SYSTEM TUBING FEED-THROUGH HOLES. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL OVERHANG LOWER SURFACE AT LEVEL RIB 10. REPAIRED SKIN PANEL PER EA 361777.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE FLOOR STRUCTURE PRESSURE DECK MEMEBRANE OPEN HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 361483.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING TOP SKIN PANEL OVER HANG LOWER SURFACE AT LEVEL RIB 15. REPAIRED SKIN PANEL PER EA 361778.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING TOP SKIN PANEL OVER HANG LOWER SURFACE AT LEVEL RIB 16. REPAIRED SKIN PANEL PER EA 361778.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #1 AILERON HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR70 AT 23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: ENCLOSURE — DELAMINATED (SLIDE) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 843 (R2) SLIDE ENCLOSURE IS DELAMINATED. REPLACED SLIDE ASSEMBLY PER TASK CARD 26C13053018.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11 SHEAR PLATE STR 23R BTW FR69 TO FR 70 AT AFT GALLEY AREA.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED PASSENGER / CREW DOOR CUTOUT FRAME AT FR 16 RIGHT AND DOOR STOP #7. REPAIRED FRAME PER EA 361438.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED PASSENGER / CREW DOOR CUTOUT UPPER CORNER FRAME AT FR 16 RIGHT AND DOOR STOP #7. REPAIRED UPPER CORNER FRAME PER EA 361438.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 58 AND S43L. REPAIRED STRINGER PER SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 55 AND FR 56 AT S39L. REPAIRED STRINGER PER SRM 53-00-13-300-001.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 57 AND S32L. REPAIRED STRINGER PER SRM 53-00-13-300-001.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE OPERATIONAL TEST OF THE DAMPING FUNCTION. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 57 AND S40L. REPLACED STRINGER PER SRM 53-00-13-300-001.

Part: FITTING — NONE (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT-HAND CONTINUITY FITTING AT FR 1 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EO 5319Y017-002. REPLACED LEFT HAND CONTINUITY FITTING PER EO 5319Y017-002.

Part: FITTING — CRACKED (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED AR FR 1 AND Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500 AILERON) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #5 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500 AILERON) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #4 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS OPERATIONAL TEST OF THE DAMPING FUNCTION. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING #1 AILERON HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y1292. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y765. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-72-11.

Part: FITTING — CRACKED (ZONE 200) · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING FASTENER HOLE AT FR 16 LEFT AT DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: ENCLOSURE — DELAMINATED (ZONE 800 SLIDE) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY DOOR 833 ESCAPE SLIDE ENCLOSURE IS DELAMINATED. REPLACED ESCAPE SLIDE ASSEMBLY PER TASK CARD 26C13053010.

Part: ENCLOSURE — DELAMINATED (ZONE 800) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY DOOR 834 ESCAPE SLIDE ENCLOSURE IS DELAMINATED. REPLACED SLIDE ASSEMBLY PER TASK CARD 26C15053012.

Part: DUMMY RAIL — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,511 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.

Part: HANDLE — CRACKED (ZONE 200) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SIDE SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12.

Part: HANDLE — CRACKED (ZONE 200) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SIDE SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #5 HINGE SUPPORT FRAME AS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON # 3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #4 HINGE SUPPORT FRAME AS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: STOP FITTING — DETERIORATED (ZONE 800) · airframe 77,512 hrs · 29,945 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 833 DOOR STOPS ARE DETERIORATED AT POSITIONS 3, 4 AND 5. REPLACED DOOR STOPS PER AMM 52-22-31.

Part: LEVER — LOOSE (ZONE 800) · airframe 77,494 hrs · 29,939 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE 3L DOOR ARMING LEVER IS LOOSE. MAINTENANCE TIGHTENED THE L3 DOOR ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 77,459 hrs · 29,926 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBRICATED COCKPIT DOOR.

Part: PRESSURE SWITCH — WARNING MESSAGE (FUEL SYSTEM) · airframe 76,658 hrs · 29,575 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SAN DUE TO THE FLIGHT CREW REPORTING AN FUEL FILTER CLOG ECAM SHORTLY AFTER TAKEOFF. THE FLIGHT CREW COMPLETED ECAM PROCEDURE AND LANDED SAFELY AT SAN WHERE THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE #2 ENGINE FUEL FILTER PER AMM 73-11-10. (AALA202410034354) AND REPLACED THE #2 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15. (AALA202410032818) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FUEL FILTER — CLOGGED (ZONE 400) · airframe 76,658 hrs · 29,575 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SAN DUE TO THE FLIGHT CREW REPORTING AN FUEL FILTER CLOG ECAM SHORTLY AFTER TAKEOFF. THE FLIGHT CREW COMPLETED ECAM PROCEDURE AND LANDED SAFELY AT SAN WHERE THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE #2 ENGINE FUEL FILTER PER AMM 73-11-10. (AALA202410034354) AND REPLACED THE #2 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15. (AALA202410032818) A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LEVER — LOOSE (ZONE 800) · airframe 76,492 hrs · 29,509 cycles

AIRCRAFT WAS NOT GROUNDED: THE ARMED LEVER AT THE 3L DOOR IS LOOSE. SECURED FASTENER ON 3L DOOR ARM LEVER

Part: HANDLE — LOOSE (L3 DOOR) · airframe 75,882 hrs · 29,244 cycles

AIRCRAFT WAS NOT GROUNDED: THE ARMING LEVER HANDLE AT 3L (AFT LEFT) DOOR IS LOOSE. SECURED L3 DOOR ARMING GRIP PLATE

Part: ENGINE — OVERTEMP (NR 2) · airframe 75,210 hrs · 28,960 cycles

AIRCRAFT WAS GROUNDED: AN MERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX. DURING TAKE OFF FROM PHX FLIGHT CREW REPORTED AT ROTATION AN ECAM ENGINE 2 EGT HI. THEN EGT OVERTEMP. FLIGHT CREW PULLED THRUST TO IDLE BUT DID NOT SHUT DOWN ENGINE AS EGT WENT BACK TO NORMAL TEMPS. THE AIRCRAFT LANDED SAFELY AT PHX AND WAS TOWED TO THE GATE. (OPEN)

Part: ENGINE — OVERTEMP (NR 2) · airframe 75,210 hrs · 28,960 cycles

AIRCRAFT WAS GROUNDED: AN MERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX. DURING TAKE OFF FROM PHX FLIGHT CREW REPORTED AT ROTATION AN ECAM ENGINE 2 EGT HI. THEN EGT OVERTEMP. FLIGHT CREW PULLED THRUST TO IDLE BUT DID NOT SHUT DOWN ENGINE AS EGT WENT BACK TO NORMAL TEMPS. THE AIRCRAFT LANDED SAFELY AT PHX AND WAS TOWED TO THE GATE. MAINTENANCE ACCOMPLISHED TSM 77-00-00-810-849-A AND ACCOMPLISHED AN ENGINE COMPRESSOR WASH PER TASK CARD 26L40072023.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 74,626 hrs · 28,698 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 2L ARMING LEVER LOOSE. TIGHTENED 2L ARMING HANDLE PER AMM 52-22-22.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 73,109 hrs · 27,983 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR "2L" ARMED/DISARMED LEVER LOOSE. ADJUSTED ARMED / DISARMED CONTROL HANDLE PER AMM 52-22-00.

Part: ENGINE — OVERTEMP (ZONE 400 - NAC/P) · airframe 73,091 hrs · 27,970 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. AFTER V1 ENGINE 2 EGT OVER LIMIT ECAM ILLUMINATED. PULLED POWER BACK TO CLIMB WHICH BROUGHT TEMPERATURE WITHIN LIMITS. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A BORESCOPE INSPECTION PER TASK CARD 26L40072006 AND A COMPRESSOR WASH PER TASK CARD 26L40072019 ON #2 ENGINE. THE #2 ENGINE WAS PLACED ON THE PERFORMANCE WATCH LIST AND RETURNED TO SERVICE.

Part: BOLT — LOOSE (ZONE 800 - DOORS) · airframe 73,072 hrs · 27,961 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR SLIDE ARMING LEVER BOLT LOOSE. RESECURED DOOR 3L SLIDE ARMING LEVER BOLT PER AMM 52-22-22.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 72,879 hrs · 27,874 cycles

AIRCRAFT WAS NOT GROUNDED: L3 EMERGENCY EXIT ARMING LEVER VERY LOOSE. RESECURED ARMING HANDLE.

Part: SLIDE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,595 hrs · 27,751 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR SLIDE IS IN RED FOR BOTTLE INDICATION. REPLACED R4 DOOR SLIDE ASSEMBLY PER JOBCARD 26L00025010.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 72,274 hrs · 27,611 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER LOOSE. MAINTENANCE SECURED LOOSE FASTENERS ON THE DOOR ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LEVER — STICKS (ZONE 800 - DOORS) · airframe 72,151 hrs · 27,551 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR ARMING LEVER STICKS. MAINTENANCE TIGHTENED ARMING HANDLE ON 2L DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-00.

Part: LEVER — LOOSE (L3 DOOR) · airframe 71,091 hrs · 27,077 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER LOOSE. MAINTENANCE RE-ADJUSTED THE 3L DOOR ARMING LEVER PER AMM 25-62-00.

Part: COMPUTER — FAULTED (FLT CONTROLS) · airframe 70,832 hrs · 26,950 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO A FLIGHT CONTROL SLATS LOCKED WING TIP BRAKE ON MESSAGE. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE #1 SLAT AND FLAP CONTROL COMPUTER PER AMM 27-80-00.

Part: SERVO — WARNING LIGHT (ZONE 700 - GEARS) · airframe 70,774 hrs · 26,923 cycles

AIRCRAFT WAS GROUNDED: DESCENDING THROUGH APPROXIMATELY 18000 FEET WHEEL NOSE WHEEL STEERING FAULT ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. AFTER LANDING, RESETS ATTEMPTED BUT UN-SUCCESSFUL. TOWED TO GATE. REMOVED AND REPLACED NOSE WHEEL STEERING SERVO-CONTROL PER AMM 32-51-51.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 70,617 hrs · 26,854 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR ARMING LEVER LOOSE. MAINTENANCE SECURED ARMING LEVER PER AMM 52-20-00.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 70,617 hrs · 26,854 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVERS LOOSE. MAINTENANCE SECURED ARMING LEVER PER AMM 52-20-00.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 70,199 hrs · 26,679 cycles

AIRCRAFT WAS GROUNDED: CABIN DOOR SLIDE 4L DOES NOT INDICATE ARMED WHEN AIRBORNE. AMBER SLIDE LIGHT FLASHES ON FLIGHT ATTENDANT PANEL. MAINTENANCE ADJUSTED L4 DOOR SLIDE ARMING PROXIMITY SENSOR 7WN1 PER AMM 52-71-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: NONE — ODOR (ZONE 100 - FUSE) · airframe 70,154 hrs · 26,658 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT A CHEMICAL SMELL IN CABIN DESCENDING INTO SLC. MAINTENANCE ISOLATED SOURCE OF ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 70,154 hrs · 26,658 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORT A CHEMICAL SMELL IN CABIN DESCENDING INTO SLC. MAINTENANCE ISOLATED SOURCE OF ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202208166031: MAINTENANCE CLEANED THE APU LOAD COMPRESSOR PER TASK CARD 26T31049006 AND ACCOMPLISHED PHASE 1 ENVIRONMENTAL CONTROL SYSTEM DECONTAMINATION PER TASK CARD 26L00021004 WITH NO ODORS BEING NOTED. ** (CLOSED)

Part: DOOR — OUT OF POSITION (ZONE 900 - LAV/G) · airframe 70,118 hrs · 26,642 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. FOUND MID LAVATORY DOOR OFF THE TRACK, RE-SEATED MID LAVATORY DOOR PER AMM 52-50-00.

Part: SDAC — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,113 hrs · 26,639 cycles

AIRCRAFT WAS GROUNDED: SLIDE ARMED LIGHT DISAGREES WITH DOOR ARMED STATUS 4L DOOR. REPLACED #2 SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC) PER AMM 32-55-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900 - LAV/G) · airframe 70,113 hrs · 26,639 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLIGHT LAVATORY-SMOKE ON ECAM LASTED 5 SECOND AND SELF CLEARED, FORWARD LAVATORY SHOWED CLEAR BY FLIGHT ATTENDANTS NO FURTHER PROBLEMS. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED.

Part: PANEL — INOPERATIVE (ZONE 800 - DOORS) · airframe 70,106 hrs · 26,632 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE ARMED LIGHT DISAGREE WITH INDICATIONS AT 4L DOOR IN FLIGHT. REMOVED AND REPLACED SLIDE ARMED LIGHT PANEL PER AMM 52-73-22.

Part: SENSOR — FAULTY (ZONE 800 - DOORS) · airframe 70,068 hrs · 26,611 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER WE WERE AIRBORNE DOOR 4L WOULD NOT SHOW THAT IT IS ARMED. **SUPPLEMENTAL REPORT FOR AALA202208012865: TROUBLESHOT PER TSM 52-13-00 FOUND DOOR HANDLE PROXIMITY SENSOR (7WN1-A) FAULTING. REPLACED PROXIMITY SENSOR (7WN1-A) PER AMM 52-73-11** (CLOSED)

Part: NONE — NONE · airframe 70,068 hrs · 26,611 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER WE WERE AIRBORNE DOOR 4L WOULD NOT SHOW THAT IT IS ARMED. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 15WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL PER AMM 33-51-38.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #1 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #3 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #3 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #2 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #2 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #5 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 - STABS) · airframe 70,051 hrs · 26,603 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #6 ELEVATOR HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.

Part: STRINGER — CORRODED (ZONE 100 - FUSE) · airframe 70,004 hrs · 26,583 cycles

AIRCRAFT WAS GROUNDED: CORROSION FOUND UNDER FLOOR BOARDS AT AFT CARGO APPROXIMATELY 12 INCHES LEFT OF SELECTOR VALVE 2504MJ ON STRINGER. REPAIRED CORROSION PER 51-73-00 AND 53-41-13.

Part: HANDLE — UNSECURE (ZONE 900 - LAV/G) · airframe 69,877 hrs · 26,525 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR HANDLE DIFFICULT TO OPERATE. SECURED LAVATORY DOOR HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-45-21.

Part: PLATE — DEFECTIVE (ZONE 800 - DOORS) · airframe 69,864 hrs · 26,521 cycles

AIRCRAFT WAS GROUNDED: 3L ARMING LEVER NEEDS ADJUSTMENT. REPLACED L3 GRIP PLATE ONLY PER AMM 52-22-22.

Part: HOUSING — DETACHED (ZONE 200 - FUSE) · airframe 69,366 hrs · 26,291 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 29C EMERGENCY EXIT LIGHT HOUSING FELL ON FLOOR. REINSTALLED EMERGENCY EXIT LIGHT HOUSING AT SEAT 29C.

Part: NONE — OUT OF POSITION (ZONE 900 - LAV/G) · airframe 69,111 hrs · 26,176 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR DIFFICULT TO OPERATE. RE-POSITIONED / RE-SECURED UPPER DOOR TRIM. DOOR OPERATES NORMAL.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 68,651 hrs · 25,977 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 2L DOOR "ARM" LEVER FOR SLIDE IS LOOSE. SECURED 2L ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-10-00--010/410-001.

Part: DOOR — OUT OF POSITION (ZONE 800 - DOORS) · airframe 68,300 hrs · 25,834 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR OFF TRACK. REINSTALLED MID LAVATORY DOOR PER AMM 52-40-00.

Part: SLIDE — INOPERATIVE (ZONE 800 - DOORS) · airframe 67,807 hrs · 25,636 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT EXT LOAD AFT LEFT AND EMERGENCY POWER SUPPLY UNIT COMMUNICATION FORWARD LEFT IS SHOWN. PERFORMED TROUBLE SHOOTING PROCEDURE PER TSM 33-51-00-810-808-A, AND REPLACED EMERGENCY POWER SUPPLY UNIT FIN 10WL (AALA202110241758), EMERGENCY POWER SUPPLY UNIT FIN 13WL (AALA202110257875) PER AMM 33-51-38-400-001-A, REPLACED LEFT ESCAPE-SLIDE PACK ASSEMBLY FIN 7502MM PER AMM 25-62-44-400-006-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 67,807 hrs · 25,636 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT EXT LOAD AFT LEFT AND EMERGENCY POWER SUPPLY UNIT COMMUNICATION FORWARD LEFT IS SHOWN. PERFORMED TROUBLE SHOOTING PROCEDURE PER TSM 33-51-00-810-808-A, AND REPLACED EMERGENCY POWER SUPPLY UNIT FIN 10WL (AALA202110241758), EMERGENCY POWER SUPPLY UNIT FIN 13WL PER AMM 33-51-38-400-001-A, REPLACED LEFT ESCAPE-SLIDE PACK ASSEMBLY (AALA202110257822) FIN 7502MM PER AMM 25-62-44-400-006-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 67,807 hrs · 25,636 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT EXT LOAD AFT LEFT AND EMERGENCY POWER SUPPLY UNIT COMMUNICATION FORWARD LEFT IS SHOWN. PERFORMED TROUBLE SHOOTING PROCEDURE PER TSM 33-51-00-810-808-A, AND REPLACED EMERGENCY POWER SUPPLY UNIT FIN 10WL, EMERGENCY POWER SUPPLY UNIT FIN 13WL (AALA202110257875) PER AMM 33-51-38-400-001-A, REPLACED LEFT ESCAPE-SLIDE PACK ASSEMBLY (AALA202110257822) FIN 7502MM PER AMM 25-62-44-400-006-A.

Part: COUPLING — ELONGATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE ELONGATE HOLE IN INBOARD UPPER FLOOR BEAM COUPLING LOCATED ON FR 63 AT LEVEL OF S23L, Y1292. REPLACED COUPLING PER SRM 51-42-11-801 AND EA 331166.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOOR PANEL 251DG DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-013.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED TOP LAYER FLOOR PANEL 251AG IN PASSENGER CABIN (1EA). REPLACED FLOOR PANEL 251AG IN PASSENGER CABIN (1EA) WITH NEW REPLACEMENT PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED TOP LAYER FLOOR PANEL 232SF IN PASSENGER CABIN (1 EA). REPLACED FLOOR PANEL 232SF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL PER A321 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED TOP LAYER FLOOR PANEL 242LF IN PASSENGER CABIN (1EA). REPLACED FLOOR PANEL 242LF IN PASSENGER CABIN (1EA) WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED TOP LAYER FLOOR PANEL 241JF IN PASSENGER CABIN (1 EA). REPLACED FLOOR PANEL 241JF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL PER A321 53-02-00-300-011.

Part: COUPLING — ELONGATED (ZONE 200 - FUSE) · airframe 67,802 hrs · 25,634 cycles

AIRCRAFT IN BASE MAINTENANCE ELONGATE HOLE IN OUT BOARD UPPER FLOOR BEAM COUPLING LOCATED ON FR 63 AT LEVEL OF S23L, Y1292. REPLACED COUPLING PER SRM 51-42-11-801 AND EA 331166.

Part: PIN — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,356 hrs · 25,447 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PIN ON 5VDC SIDE OF LIGHT PER 20-48-14.

Part: LEVER — LOOSE (R2 DOOR) · airframe 65,899 hrs · 24,854 cycles

AIRCRAFT WAS NOT GROUNDED. 2R DOOR ARMING LEVER IS LOOSE. RE SECURED 2R DOOR ARMING LEVER.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 65,797 hrs · 24,815 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR R1 DOOR DAMPER REQUIRE SERVICING. SERVICED DOOR DAMPER ON DOOR R1, PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 65,797 hrs · 24,815 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR L1 DOOR DAMPER REQUIRE SERVICING. SERVICED DOOR DAMPER ON DOOR L1, PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 65,797 hrs · 24,815 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR R4 DOOR DAMPER REQUIRE SERVICING. SERVICED DOOR DAMPER ON DOOR R4, PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 65,797 hrs · 24,815 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR L4 DOOR DAMPER REQUIRE SERVICING. SERVICED DOOR DAMPER ON DOOR L4, PER AMM 52-10-00.

Part: SLIDE — UNSECURE (L4 DOOR) · airframe 65,602 hrs · 24,737 cycles

AIRCRAFT WAS NOT GROUNDED. SLIDE COVER AT DOOR 4L NOT SECURED. REPOSITIONED SLIDE OPERATIONS CHECK GOOD, PER AMM REF 52-10-00 DOOR 4L.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 65,424 hrs · 24,666 cycles

AIRCRAFT WAS NOT GROUNDED. FLOOR LEVEL EMERGENCY EXIT LIGHT COVER MISSING BY 2R DOOR (ROW 9D SEAT). REMOVED AND REPLACED SEAT MOUNTED EMERGENCY EXIT LOCATION LIGHT (ROW 9D SEAT), PER AMM 33-51-18.

Part: PINTLE PIN — CORRODED (LT MLG) · airframe 65,033 hrs · 24,507 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT MAIN LANDING GEAR REAR PINTLE PIN. REPLACED PINTLE PIN IAW TASK CARD 26T00032001.

Part: POWER SUPPLY — WRONG PART (EMERGENCY LIGHTS) · airframe 64,793 hrs · 24,415 cycles

AIRCRAFT IN BASE VISIT: WHILE ACCOMPLISHING J/C 26C00033004 FOUND AFT DOOR ESPU WOULD NOT TEST. FOUND ESPU HAD WRONG EFFECTIVITY IN IT. REPLACED ESPU PER AMM 33-51-38.

Part: BATTERY — FAULTY (FWD FLASHLIGHT) · airframe 64,305 hrs · 24,216 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 2R FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD PRACTICES.

Part: LENS — FAULTY (EMERGENCY LIGHT) · airframe 61,131 hrs · 22,964 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT ON AT 3L. MAINTENANCE REPLACED LIGHT LENS PER AMM 33-51-13-400-001-A.

Part: ARMING LEVER — LOOSE (R2 DOOR) · airframe 63,453 hrs · 23,894 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING LEVER OF DOOR 2R WAS VERY LOOSE. MAINTENANCE REATTACHED ARMING HANDLE PER STANDARD PRACTICES.

Part: HANDLE — FAULTY (L3 DOOR) · airframe 63,444 hrs · 23,890 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3L SLIDE ARMING LEVER LOOSE, ABOUT FALL OFF. MAINTENANCE RESECURED 3L DOOR SLIDE ARMING HANDLE PER AMM 52-22-22.

Part: MEGAPHONE — INOPERATIVE (FWD CABIN) · airframe 61,131 hrs · 22,964 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE INOPERABLE. MAINTENANCE REPLACED MEGAPHONE PER JOB CARD 26C00025003.

Part: WIRE HARNESS — CHAFED (ZONE 300 - STABS) · airframe 61,131 hrs · 22,964 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND CHAFING ON THE ELECTRICAL HARNESS FROM CONNECTOR 7120VC TO P11 AND P20 IN APU COMPARTMENT. REPLACED ELECTRICAL WIRING ON APU COMPARTMENT FROM CONNECTOR 7120 VCA PIN 20 TO CONECTOR PII PIN A AND FROM CONNECTOR 7120VCA PIN 4 TO CONECT OR PS PIN 2 IAW AWM 49-15-01 AND CMM 49-11-09 AND PERFORMED OPERATIONAL TEST OF THE APU IAW AMM 49-00-00-710-010-A. TEST IS OK

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 61,131 hrs · 22,964 cycles

CORROSION WAS FOUND ON THE AFT SERVICE DOOR LOWER SILL, FRAME 66, STRINGER 23R. REPLACED THE LOWER DOOR SILL IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 61,131 hrs · 22,964 cycles

FORWARD GALLEY FLOOR PANEL 232DF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-00-00.

Part: COUPLING — DAMAGED (FRAME 66) · airframe 61,131 hrs · 22,964 cycles

AFT GALLEY LOWER SILL, UPPER OTBD SPLICE COUPLING HAD AN ELONGATED HOLE AT FRAME 66, STRINGER 23R. REPLACED THE SPLICE COUPLING IAW SRM 51-72-11.

Part: ANGLE — DAMAGED (FRAME 67) · airframe 61,131 hrs · 22,964 cycles

AFT GALLEY, LOWER SILL ANGLE HAD AN ELONGATED HOLE AT FRAME 67, STRINGER 23R. REPLACED THE ANGLE IAW SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 61,131 hrs · 22,964 cycles

CRACKED INTERCOSTAL AT FRAME 16, STRINGER 10R. REPLACED THE INTERCOSTAL IAW SRM 51-72-11.

Part: WINDOW — DELAMINATED (GALLEY DOOR) · airframe 61,131 hrs · 22,964 cycles

FORWARD GALLEY DOOR OUTER WINDOW PANE DELAMINATED. REPLACED THE DOOR WINDOW IAW AMM 56-31-11-400-002-A.

Part: WINDOW — DELAMINATED (PAX DOOR) · airframe 61,131 hrs · 22,964 cycles

PASSENGER DOOR OUTER WINDOW PANE DELAMINATED. REPLACED THE WINDOW PANE IAW AMM 56-31-11-400-002-A0

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE FORWARD CARGO BAY SHEAR TIE, FRAME 33, BETWEEN STRINGERS 40R AND 41R. REPLACED THE SHEAR TIE IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 16, +Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 61,131 hrs · 22,964 cycles

A CRACKED INTERCOSTAL FITTING AT FRAME 16, STRINGER 10L AT THE NR 7 DOOR STOP FITTING. REPLACED THE INTERCOSTAL IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE FORWARD GALLEY FLOORBEAM. FRAME 16, +Y765. REPLACED THE FLOORBEAM IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 61,131 hrs · 22,964 cycles

PASSENGER CABIN FLOOR PANEL 241AF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV I.

Part: FLOOR PANEL — DEBONDED (FWD GALLEY) · airframe 61,131 hrs · 22,964 cycles

FORWARD GALLEY FLOOR PANEL 231AF UPPER LAYER DEBONDED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-283-003.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE LEFT AFT DOOR CUT OUT LOWER SILL AT FRAME 66, STRINGER 23L. REPLACED THE LOWER DOOR SILL IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 20, -Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DEBONDED (FWD GALLEY) · airframe 61,131 hrs · 22,964 cycles

FORWARD GALLEY FLOOR PANEL 222EF WAS DEBONDED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701, REV I.

Part: FLOOR PANEL — DEBONDED (FWD GALLEY) · airframe 61,131 hrs · 22,964 cycles

THE FORWARD GALLEY FLOOR PANEL 221EF WAS DEBONDED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE LEFT AFT DOOR CUTOUT LOWER SILL AFT CORNER FITTING AT FRAME 68, STRINGER 23L. REPLACED THE CORNER FITTING IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 70) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE AFT GALLEY FLOORBEAM, FRAME 70, -Y765. REPLACED THE FLOORBEAM IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 61,131 hrs · 22,964 cycles

THE AFT GALLEY FLOOR PANEL 261DF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 61,131 hrs · 22,964 cycles

THE AFT GALLEY FLOOR PANEL 262BG WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-600-011.

Part: FLOOR PANEL — DEBONDED (FWD GALLEY) · airframe 61,131 hrs · 22,964 cycles

FORWARD GALLEY FLOOR PANEL 232EF WAS DEBONDED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701, REV I.

Part: DUMMY RAIL — CORRODED (FRAME 16) · corrosion level 2 · airframe 61,131 hrs · 22,964 cycles

CORROSION ON FORWARD GALLEY DUMMY RAIL AT FRAMES 16, +Y503.2. REPLACED THE DUMMY RAIL IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FRAME 55) · airframe 61,131 hrs · 22,964 cycles

CORROSION FOUND ON THE SHEAR TIE, FRAME 55, STRINGERS 41L & 42L. REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 61,131 hrs · 22,964 cycles

NOSE LANDING GEAR LEFT AFT DOOR FORWARD HINGE HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE FITTING IAW AMM 32-22-13-410-001-A.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 61,131 hrs · 22,964 cycles

NOSE LANDING GEAR, LEFT AFT DOOR, AFT HINGE HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE IAW AMM 32-22-13-410-001-A.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 61,131 hrs · 22,964 cycles

NOSE LANDING GEAR, RIGHT AFT DOOR, FORWARD HINGE HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE IAW AMM 32-22-13-410-001-A.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 61,131 hrs · 22,964 cycles

NOSE LANDING GEAR, RIGHT AFT DOOR, AFT HINGE HAD EXCESSIVE PLAY AND WAS WORN. REPLACED THE HINGE IAW AMM 32-22-13-410-001-A.

Part: CLEAT — CRACKED (FRAME 35) · airframe 61,131 hrs · 22,964 cycles

FORWARD CARGO CLEAT WAS CRACKED AT FRAME 35.5, STRINGER 30L. REPLACED THE CLEAT IAW SRM 51-72-11, AND 51-42-11.

Part: STRINGER — CORRODED (FRAMES 55-56) · airframe 61,128 hrs · 22,963 cycles

CORROSION FOUND ON STRINGER 41L, BETWEEN FRAMES 55 AND 56. REPLACED STRINGER IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 61,128 hrs · 22,963 cycles

CORROSION FOUND ON STRINGER 42L, FRAMES 56 AND 57L. REPLACED STRINGER IAW SRM 51-42-11.

Part: COVER — DEFECTIVE (L4 DOOR SLIDE) · airframe 60,532 hrs · 22,714 cycles

L4 DOOR SLIDE UNPACKED. REINSTALLED THE DOOR SLIDE COVER ASSEMBLY IAW AMM 25-65-04. OK FOR SERVICE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 60,516 hrs · 22,708 cycles

EMERGENCY POWER SUPPLY 10WL FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PLATE — LOOSE (ARMING LEVER) · airframe 59,946 hrs · 22,468 cycles

THE R2 DOOR ARMING LEVER HAS A LOOSE PLATE, REPORTED BY THE FLIGHT ATTENDANT. SECURED THE ARMING LEVER. OK FOR SERVICE IAW AMM 52-22-22.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 59,475 hrs · 22,290 cycles

FLASHLIGHT AT THE R2 DOOR FLIGHT ATTENDANT JUMPSEAT NOT CHARGING. REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED OK.

Part: LEVER — LOOSE (R2 DOOR ARMING) · airframe 59,203 hrs · 22,178 cycles

R2 DOOR ARMING LEVER LOOSE. SECURED THE ARMING LEVER.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 58,968 hrs · 22,098 cycles

FORWARD CARGO FLOOR PANEL 131EF DELAMINLATED. REPLACED THE FLOOR PANEL IAW AMM 53-22-14. THE AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 58,968 hrs · 22,098 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD CARGO FLOOR PANEL 131AF DELAMINATED. REPLACED CARGO PANEL PER AMM 53-22-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 58,968 hrs · 22,098 cycles

BULK CARGO FLOOR PANEL 161AF DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-42-14. THE AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 58,968 hrs · 22,098 cycles

AFT CARGO FLOOR PANEL 151MK DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. THE AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 58,968 hrs · 22,098 cycles

AFT CARGO FLOOR PANEL 151LF DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. THE AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,211 hrs · 21,810 cycles

R4 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS)

DURING AN EMERGENCY LIGHT SYSTEM TEST, THE TEST FAILED WITH A MESSAGE FOR THE EMERGENCY POWER SUPPLY UNIT, R3 DOOR. REPLACED THE POWER SUPPLY UNIT AND BATTERY PACK IAW AMM 33-51-38.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,596 hrs · 21,567 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY FLASHLIGHT RED LIGHT NOT FLASHING AT DOOR STA 2R. REPLACED EMERGENCY FLASHLIGHT BATTERY PER 25-65-00.

Part: PIN — MISSING (L3 DOOR) · airframe 57,332 hrs · 21,468 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS THAT ARMING LEVER DOOR 3L IS LOOSE. REPLACED MISSING PIN IN ARMING HANDLE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 56,623 hrs · 21,179 cycles

R3 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED 12WL EMERGENCY POWER SUPPLY BATTERY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,623 hrs · 21,179 cycles

EMERGENCY LIGHT LENS AT THE L4 DOOR FOUND MISSING. REPLACED EMERGENCY LIGHT LENS IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,444 hrs · 21,100 cycles

12C FLOOR LEVEL EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW AMM.

Part: BRACKET — BENT (EMERGENCY LIGHT) · airframe 55,494 hrs · 20,742 cycles

SEAT 9D EMERGENCY LIGHT BRACKET BENT. REPLACED THE BRACKET.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,494 hrs · 20,742 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 9D. REPLACED MISSING LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,359 hrs · 20,699 cycles

EMERGENCY EXIT LIGHT LENS ROW 9 RIGHT IS MISSING. INSTALLED A NEW LENS. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,154 hrs · 20,623 cycles

ROW 9D RED ISLE MARKER LIGHT LENS MISSING. REPLACED THE LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,051 hrs · 20,585 cycles

R4 DOOR MISSING EMERGENCY EXIT LIGHT LENS. INSTALLED THE LENS. AIRCRAFT NOT GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,051 hrs · 20,585 cycles

CREW REPORTED THE L1 DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED THE LENS. AIRCRAFT NOT GROUNDED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,874 hrs · 20,516 cycles

FOUND EXIT LIGHT AT SEAT 22D INOPERATIVE. SECURED THE LIGHT AT 22D.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,317 hrs · 20,283 cycles

EPSU 10WL HAS A FAILED BATTERY. REPLACED THE BATTERY IAW AMM 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,284 hrs · 20,267 cycles

FOWARD EMERGENCY FLASHLIGHT STRAP BROKEN AND LED INOPERATIVE. REMOVED AND INSTALLED EMERGENCY LIGHT BATTERY AND REPLACED STRAP IAW AMM 25-60-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,088 hrs · 20,196 cycles

MISSING EMERGENCY LIGHT LENS ON SEAT 9E,F. REPLACED THE LENS IAW AMM 33-50-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,987 hrs · 20,158 cycles

9D LENS FOR EMERGENCY EXIT MISSING. INSTALLED A NEW LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,923 hrs · 20,135 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY SEAT LIGHT INOPERATIVE AT ROW 23 LEFT. REPLACED ROW 23 EMERGENCY LIGHT HOUSING PER AMM 33-50-00.

Part: LENS — MISSING (CABIN) · airframe 53,923 hrs · 20,135 cycles

AIRCRAFT WAS NOT GROUNDED. MISSING EMERGENCY LIGHT LENS AT ROW 9 RIGHT. REPLACED EMERGENCY LIGHT COVER PER AMM 33-50-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,865 hrs · 20,110 cycles

LENS ON SEAT 9D MISSING, OPEN SOCKET. INSTALLED NEW LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,281 hrs · 19,895 cycles

EMERGENCY EXIT MARKER AT DOOR R4 MISSING LENS. INSTALLED LENS IAW AMM 33-51-13.

Part: LENS — MISSING (CABIN) · airframe 53,023 hrs · 19,792 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 9D EMERGENCY LIGHT COVER LENS MISSING. INSTALLED LENS AT SEAT 9D.

Part: FLASHLIGHT — UNSECURE (CABIN) · airframe 53,023 hrs · 19,792 cycles

AIRCRAFT WAS NOT GROUNDED: AFT F/A JUMPSEAT FLASHLIGHT INOPERATIVE. RESECURED FLASHLIGHT AT AFT F/A JUMPSEAT AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: STRUT — OUT OF ADJUST (RT WING TE FLAP) · airframe 52,780 hrs · 19,705 cycles

FLIGHT CREW REPORTED RECIEVEING A FLAP LOCKED ALIGNMENT FAULT DURING APPROACH INTO CLT. DECLARED AN EMERGENCY AND LANDED. MAINTENANCE ACCOMPLISHED TSM 27-51-00-810-818-A AND ADJUSTED THE RIGHT FLAP INTERCONNECTING STRUT IAW AMM 27-51-44. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 27-54-00.

Part: TARGET — OUT OF ADJUST (L4 DOOR) · airframe 52,754 hrs · 19,698 cycles

DURING LANDING. L4 DOOR SHOWED OPEN ON ECAM. FLIGHT ATTENDANT SAID IT LOOK CLOSED. MAINTENANCE ADJUSTED THE TARGETS FOR SENSORS 15WV1 AND 17WV1 AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 52-71-00-820-001-A01, 527-71-00-820-002-A01 AND 52-71-00-710-001-A.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 52,754 hrs · 19,698 cycles

L4 DOOR EMERGENCY EXIT LIGHTS FLASH ON AND OFF AT REGULAR INTERVALS DURING FLIGHT. MAINTENANCE SECURED POWER SUPPLY CONNECTOR AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW TSM 33-51-00-810-819A AND AMM 33-51-00-710-001.

Part: CONNECTOR — LOOSE (ZONE 200 - FUSE) · airframe 52,754 hrs · 19,698 cycles

R4 DOOR EMERGENCY EXIT LIGHTS FLASH ON AND OFF AT REGULAR INTERVALS DURING FLIGHT. MAINTENANCE SECURED THE POWER SUPPLY CONNECTOR AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW TSM 33-51-00-810-819A AND AMM 33-51-00-710-001.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 52,617 hrs · 19,650 cycles

AFT CARGO BAY CENTER FLOOR PANEL 151GF DAMAGED. REPLACED THE FLOOR PANEL IAW AMM 53-42-17.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,534 hrs · 19,617 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 3L IS MISSING THE LENS. INSTALLED LENS IAW AMM 33-51-18.

Part: PLATE — MISSING (CABIN) · airframe 51,782 hrs · 19,344 cycles

AIRCRAFT WAS NOT GNDED. FLOOR LEVEL EMER LIGHT PLATE MISSING, LIGHT BULBS BENT. REPLACED PLATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,517 hrs · 19,232 cycles

AIRCRAFT WAS NOT GNDED. SEAT 9D FLOOR LEVEL EMER LIGHT INOPERATIVE. REPLACED EMER LIGHT COVER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 51,331 hrs · 19,156 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT LENS IS MISSING AT ROW 8L. INSTALLED NEW EMER LIGHT LENS AT ROW 8L.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 51,331 hrs · 19,156 cycles

AIRCRAFT WAS NOT GNDED. DOOR 4R ARM & DISARM LEVER NOT WORKING PROPERLY. REMOVED DEBRIS FROM GIRT ASSEMBLY & OPERATED ARM & DISARM LEVER SEVERAL TIMES. OPERATIONAL CHECKED NORMAL.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 51,088 hrs · 19,064 cycles

AIRCRAFT IN BASE MX. FLOOR PANEL 214EF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,088 hrs · 19,064 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE AFT HOLE HAVE CRACK INDICATIONS. REPAIRED IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,088 hrs · 19,064 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE AFT 2 HOLES HAVE CRACK INDICATIONS. REPAIRED IAW EO 5315Y066.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,545 hrs · 18,828 cycles

CORROSION ON SEALING ANGLE LOCATED AT FLOOR NEAR LAVATORY A & L1 DOOR FRAME.

Part: RESERVOIR — INOPERATIVE (L3 DOOR) · airframe 50,545 hrs · 18,828 cycles

MID DOOR LT SLIDE PSI INDICATION INOPERATIVE. REPLACED 3L DOOR INFLATION RESERVOIR & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-62-49.

Part: LIGHT — MALFUNCTIONED (ZONE 800) · airframe 48,668 hrs · 18,079 cycles

DOOR WON'T ARM WITH STATUS LIGHT CONTINUOUS ON. REPLACED THE L3 DOOR LIGHT ASSEMBLY.

Part: PROXIMITY SENSOR — FAULTY (L3 DOOR) · airframe 48,621 hrs · 18,062 cycles

L3 DOOR SHOWS ARMED WHEN DISARMED. R & R THE L3 ARM HANDLE PROXIMITY SENSOR 6WN1.

Part: RESERVOIR — FAULTY (EVAC SLIDE) · airframe 48,346 hrs · 17,951 cycles

2R DOOR SLIDE PRESS FAULT INDICATION ON CIDS. R & R 2R SLIDE RESERVOIR ASSEMBLY IAW AMM 25-62-49 401 WITH GOOD OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 48,033 hrs · 17,836 cycles

SEAT 34C EMER LIGHT LENS COVER MISSING. INSTALLED LENS AT SEAT 34C IAW 33-51-19. GOOD OPERATIONAL CHECK.

Part: COVER — MISSING (CABIN) · airframe 47,143 hrs · 17,476 cycles

EMERGENCY LIGHT COVER 10C OFF. REPLACED EMER LIGHT COVER AT ROW 10C. OK FOR SERVICE.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 46,583 hrs · 17,254 cycles

CREW REPORTED A SMOKE DETECTOR FAULT. REPLACED SDCU FOR TROUBLESHOOTING. REPLACED LAVATORY SMOKE DETECTORS 5WQ & 4WH. OPERATIONS CHECKED SATISFACTORY IAW AMM 26-17-34, 26-16-15 & 26-17-15.

Part: LEVER — LOOSE (R3 DOOR) · airframe 45,791 hrs · 16,947 cycles

THE 3R DOOR ARMING LEVER LOOSE. SECURED AS REQUIRED, CHECKS OK.

Part: LEVER — LOOSE (R2 DOOR) · airframe 45,784 hrs · 16,944 cycles

THE 2R SLIDE ARMED LEVER LOOSE. SECURED 2R SLIDE ARMED LEVER.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 45,561 hrs · 16,862 cycles

MID FLIGHT ATTENDANT FLASHLIGHT STRAP BROKEN. REPLACED FLASHLIGHT STRAP AT MID FLIGHT ATTENDANT IAW AMM 33-51-00.

Part: COVER — BROKEN (CABIN) · airframe 45,160 hrs · 16,696 cycles

THE EXIT LIGHT COVER BROKEN AT SEAT 8D. REPLACED LIGHT COVER, OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 44,865 hrs · 16,563 cycles

CREW REPORTED EMERGENCY EXIT LIGHTS & SIGNS WERE TURNING ON & OFF RANDOMLY. MX PERFORMED CIDS RESET IAW AMM 23-73-00-740-005. EMERGENCY EXIT LIGHTS & SIGNS CHECKED GOOD, NO FAULTS NOTED & ACFT OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 44,647 hrs · 16,459 cycles

CREW REPORTED THE EXIT DOOR LIGHT COVER MISSING AT 4L DOOR. MX INSTALLED EXIT DOOR LIGHT COVER AT 4L DOOR, OPERATIONS CHECKED GOOD.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 43,733 hrs · 16,054 cycles

WRONG EMERGENCY LIGHT LENS OVER 8C. MAINTENANCE REPLACED EMERGENCY LIGHT LENS.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 43,401 hrs · 15,924 cycles

CIDS CAUTION LIGHT IS ILLUMINATED. FOUND DOOR 3R DOOR DAMPER LOW. SERVICED 3R DOOR DAMPER BOTTLE IAW AMM 52-50-00-614-002A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 43,362 hrs · 15,910 cycles

R3 DOOR ASSIST BOTTLE PRESSURE IS LOW. SERVICED R3 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 43,318 hrs · 15,892 cycles

CIDS CAUTION LIGHT DOOR BOTTLE EXIT R3. SERVICED R3 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 43,229 hrs · 15,850 cycles

MASTER CAUTION LIGHT ON CIDS PANEL. SERVICED DOOR R3 ASSIST BOTTLE IAW AMM 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 43,120 hrs · 15,806 cycles

EMERGENCY DOOR ASSIST BOTTLE HAS LOW PRESSURE AT R3 DOOR. SERVICED ASSIST BOTTLE IAW AMM 52-22-00-614-002-A.

Part: TURBINE WHEEL — FAILED (LT ENGINE) · airframe 43,041 hrs · 15,780 cycles

LOST LT ENGINE ON TAKEOFF. REJECTED TAKEOFF AT 80 KNOTS AND RETURNED TO GATE. ON INSPECTION, DEBRIS WAS NOTED IN TAILPIPE OF NR 1 ENGINE. R & R NR 1 ENGINE. NO EVIDENCE OF BIRD STRIKE OR FOD, INTERNAL TURBINE DAMAGED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 42,944 hrs · 15,728 cycles

EMERGENCY EXIT LIGHT OVER R2 DOOR APPEARS TO BE INOPERATIVE. RESET MID EMERGENCY POWER SUPPLY UNIT AND PERFOMRED BITE TEST, NO FAULTS FOUND.

Part: CYLINDER — LOW (R4 DOOR) · airframe 42,879 hrs · 15,699 cycles

FORWARD CIDS PANEL HAS "CAUTION" BUTTON MESSAGE. SERVICED EMERGENCY EXIT DOOR DAMPER AT R4 IAW AMM 52-22-00-614-002-A.

Part: DIRECTOR — FAULTY (CIDS) · airframe 42,422 hrs · 15,524 cycles

F/A REPORTED SMOKE DETECTOR LIGHTS IN THE CABIN. REPLACED CIDS DIRECTOR IAW MM 23-73-34-400-001A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 42,373 hrs · 15,508 cycles

CIDS PANEL SHOWS LOW BOTTLE PRESSURE AT R3 DOOR. SERVICED R3 DOOR ASSIST BOTTLE IAW MM 52-22-00-614-002.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DURING CABIN EMERGENCY LIGHTING OPERATIONAL TEST, EMERGENCY LIGHTS WERE FOUND INOP ON SEAT POSITIONS 25, 30 AND 34 LEFT SIDE AT PAX CABIN. PERFORMED TROUBLESHOOTING IAW TSM 31-51-00-810-801-A AND REPLACED EPSU (13WL) IAW AMM 33-51-38-400-001-A AND PERFORMED OPS TEST IAW AMM 33-51-00-710-001-A. TEST OK.

Part: LIGHT — CRACKED (CABIN) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CRACKED LIGHT EMERGENCY OF DOOR FRAME 221SW AND 222SW. REPLACED LIGHT EMERGENCY OF DOOR FRAME 221SW AND 222SW IAW A321 AMM 33-51-16-400-001-ASTEP 7.(A).6.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, S23R, -Y1722.8. REPLACED WEB BETWEEN FR20 TO FR24, S23R, -Y1722.8 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53114392.

Part: DAMPER — LOW PRESSURE (PAX DOOR) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LOW PRESSURE ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 841. REPLACED THE DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 841 IAW A321 AMM 52-11-14-000-001-B, 52-11-14 -400-001-B, 52-11-14-200-001-A & 52-11-14-820-002-A.

Part: SUPPORT FITTING — CORRODED (PAX DOOR) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CORROSION ON FITTING AT RIGHT AFT PASS/CREW DOOR OF SLIDE SUPPORT. REPLACED SLIDE SUPPORT FITTING AT RIGHT AFT PASS/CREW DOOR IAW A321 CMM 52-13-15-400.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - GALVANIC CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 TO FR 68 STR 23L (SHAPE, SILL). REPLACED CENTER FITTING (SHAPE SILL) LOCATED BETWEEN FR 66 TO FR 68, STR 23L IAW A321 SRM A321 51-72-11 PAGE 1-2 AND DRAWING D53480505.

Part: FUEL DOOR — ELONGATED (LT WING) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - ELONGATED HOLE ON LOWER LEFT WING FUEL DOOR 540HB BETWEEN RIB 13 TO RIB 14 & BETWEEN S8L TO S11L. REPLACED LEFT WING FUEL DOOR 540HB IAW A321 SRM 57-27-11.

Part: RIB — CRACKED (LE SLAT) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CRACK IN LEFT WING SLAT NR 2, TRACK RIB 5. REPAIRED ATTACH FITTING OF LEFT WING SLAT NR 2 TRACK RIB 5 IAW A321 SRM 57-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, S23R, -Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53372500.

Part: FUEL DOOR — ELONGATED (RT WING) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - ELONGATED HOLE ON LOWER RIGHT WING FUEL DOOR 640KB BETWEEN RIB 15 TO RIB 16 AND BETWEEN S8R TO S11R. REPLACED RIGHT WING FUEL DOOR 640KB IAW A321 SRM 57-27-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151PF BETWEEN FR58 TO FR59 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151PF IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF IAW A321 AMM 53-12-12.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 152MF BETWEEN FR56 TO FR58 & BETWEEN -Y970.8 TO -Y765. REPLACED FLOOR PANEL 152MF IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CABIN SEAT TRACK CORRODED FROM FR 36 TO FR 41 AT Y 765. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53372500.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151LF BETWEEN FR56 TO FR58 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 151LF IAW A321 SRM 53-02-00 FIGURE 209 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y1732 TO Y765. REPLACED FLOOR PANEL 261BG IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO -Y254. REPLACED FLOOR PANEL 231BF IAW A321 SRM 53-12-00, FIGURE 206 & IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CABIN SEAT TRACK CORRODED FROM FR 41 TO FR 47 AT Y -1292. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11, AIRBUS DRAWING D53371112 AND EA 503994.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 261DF IAW A321 SRM 53-02-00 FIG 209, IRM 9701 REV G & EA 503993.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y1732 TO -Y254. REPLACED FLOOR PANEL 222CF IAW A321 SRM 53-12-00, FIGURE 206 & IRM 9701 REV G.

Part: HINGE FITTING — CORRODED (LT ELEVATOR) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - EXCESSIVE PLAY ON NR 6 LEFT ELEVATOR HINGE ARM FITTING AT HORIZONTAL STABILIZER STA 589, RIB 13. REPLACED NR 6 LEFT ELEVATOR HINGE ARM FITTING IAW A321 AMM 55-16-42.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR28 TO FR29, S42L. REPAIRED STRINGER 42L BETWEEN FR28 TO FR29 IAW A321 SRM 53-21-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46+15 INCHES, S23L, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46+15 INCHES, S23L, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53372500.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR47.2 TO FR47.4, -Y1732. REPLACED FLOORBEAM BETWEEN FR47.2 TO FR47.4, -Y1732 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53459000.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON ANGLE BETWEEN FR47.2 TO FR47.4, S28R. REPLACED ANGLE BETWEEN FR47.2 TO FR47.4, S28R IAW A321 SRM 51-72-11, AIRBUS DRAWING D53456593 & D53456593.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234930.

Part: STOP FITTING — CRACKED (LE SLAT) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - BROKEN STOP BOLT FITTING LOCATED ON RIGHT WING AREA SLAT NR 2 TRACK NR 5 AT RIB 4. PERFORMED PERMANENT REPAIR LOCATED ON FITTING, SLAT 2 TRACK 5 AT RIB 4 RIGHT WING IAW A321 SRM 57-40-00, PARAGRAPH 5AA FIG 235.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR47.4 TO FR47.5, -Y1732. REPLACED FLOORBEAM BETWEEN FR47.4 TO FR47.5, -Y1732 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53459000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234930.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR62+17 INCHES TO FR63+18 INCHES, -Y1292. REPLACED SEAT RAIL BETWEEN FR62+17 INCHES TO FR63+18 INCHES, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47.1 TO FR47.4, Y765. REPLACED SEAT TRACK BETWEEN FR47.1 TO FR47.4, Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472550.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR62+17 TO FR64, Y1292. REPLACED SEAT RAIL BETWEEN FR62+17 TO FR64, Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR62+17 TO FR64, -Y765. REPLACED SEAT RAIL BETWEEN FR62+17 TO FR64, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47.5 TO FR62+17 INCHES, Y1292. REPLACED SEAT TRACK BETWEEN FR47.5 TO FR62+17 INCHES, Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472771.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47.5 TO FR62+17 INCHES, -Y765. REPLACED SEAT TRACK BETWEEN FR47.5 TO FR62+17 INCHES, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472771.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - CABIN SEAT RAIL CORRODED BETWEEN SR 47 AND FR 63 AT Y -1292. REMOVED AND REPLACED SEAT RAIL IAW A321 SRM A321 51-72-11AND AIRBUS DRAWINGS D53472771 & D53472650.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - GALVANIC CORROSION ON FLOORBEAM -Y254 LOCATED AT LEVEL FR 21 FWD PAX CABIN. REPLACED FLOORBEAM LOCATED AT LEVEL FR 12 TO FR 24 -Y254 FWD PAX CABIN IAW A321 SRM 51-72-11 AND DRAWING D53112816 AND D53115054.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53110984 & D53112829.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53112812.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON WEB AT FR16, S23R. REPLACED WEB AT FR16, S23R IAW A321 SRM 51-72-11, AIRBUS DRAWING D53114392 & D53918262.

Part: SKIN — WORN (LE SLAT) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - WEAR ON LEFT WING AT NR 2 SLAT LOWER SKIN UPPER SURFACE BETWEEN WS 407 TO WS 732 & BETWEEN RIB 8 TO RIB 13. REPAIRED LEFT WING AT NR 2 SLAT LOWER SKIN UPPER SURFACE IAW EA 503997.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, -Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, -Y254 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53111462 & D53115054.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, -Y503.2. REPLACED RAIL DUMMY AT FR16, -Y503.2 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53112825 & D53112826.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - WEAR ON NR 2 RIGHT ELEVATOR HINGE FITTING BETWEEN HORIZONTAL STABILIZER STA 193 TO STA 228 & BETWEEN RIB 4 TO RIB 5. REPLACED NR 2 RIGHT ELEVATOR HINGE FITTING IAW A321 SRM 51-72-11 & AMM 55-16-42.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR23, -Y1584. REPLACED SEAT TRACK BETWEEN FR20 TO FR23, -Y1584 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53112851.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379.5. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y1379.5 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53110984 & D53112829.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53115054 & D53110984.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A321 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR18 TO FR20, Y1292. REPLACED SEAT TRACK BETWEEN FR18 TO FR20, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53110984 & D53115054.

Part: LEVER — WORN (TE FLAP) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - WEAR ON LEFT WING BRACKET-LEVER ASSEMBLY AT INBOARD FLAP TAB HINGE 1A AT FRONT SPAR BETWEEN RIB 3 TO RIB 4. REPLACED LEFT WING LEVER ASSEMBLY BRACKET AT INBOARD FLAP TAB HINGE 1A IAW A321 CMM 57-52-23.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON UPPER INBOARD COUPLING AT FR67+16 INCHES, -Y1162. REPLACED UPPER INBOARD COUPLING AT FR67+16 INCHES, -Y1162 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472780 & D53472089.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A321 SRM 51-72-11 & TYPICAL REPAIR TR320-2528-10-0011G.

Part: LEVER — WORN (TE FLAP) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - WEAR ON RIGHT WING BRACKET-LEVER ASSEMBLY AT INBOARD FLAP TAB HINGE NR 1A AT FRONT SPAR BETWEEN RIB 3 TO RIB 4. REPLACED RIGHT WING LEVER ASSEMBLY BRACKET AT INBOARD FLAP TAB HINGE NR 1A IAW A321 CMM 57-52-23.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON UPPER INBOARD COUPLING AT FR66+5 INCHES, Y1292. REPLACED UPPER INBOARD COUPLING AT FR66+5 INCHES, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472815.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON UPPER OUTBOARD COUPLING AT FR66+5 INCHES, Y1292. REPLACED UPPER OUTBOARD COUPLING AT FR66+5 INCHES, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472815.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR67, -Y318 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472814.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474180.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, Y1162. REPLACED COUPLING AT FR67+16 INCHES, Y1162 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472780.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66+5 INCHES, Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66+5 INCHES, Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66+5 INCHES, -Y765 IAW A321 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - L4 DOOR SILL CORRODED FROM FR 66 TO FR 68 AT S23L. REMOVED AND REPLACED SILL IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 AND EA 503967.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y464. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y464 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, -Y765 IAW A321 SRM 51-72-11.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474180.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR67+16 INCHES, Y1162. REPLACED COUPLING AT FR67+16 INCHES, Y1162 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, -Y1162 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y512 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN Y1292 TO Y1162. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN Y1292 TO Y1162 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SILL BETWEEN FR66 TO FR68, S23R. REPLACED SILL BETWEEN FR66 TO FR68, S23R IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503971.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER INBOARD COUPLING AT FR67+16 INCHES, -Y1162. REPLACED LOWER INBOARD COUPLING AT FR67+16 INCHES, -Y1162 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472780 & D53472089.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - ELONGATED HOLE ON COUPLING AT FR66, S23R. REPLACED COUPLING AT FR66, S23R IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503971.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+5 INCHES, Y1162 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM BETWEEN FR64 TO FR66+5 INCHES, Y765. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66+5 INCHES, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472831.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,043 hrs · 15,351 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN -Y1292 TO -Y1162. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES & BETWEEN -Y1292 TO -Y1162 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y765 TO -Y1732. REPLACED FLOOR PANEL 262BG IAW A321 SRM 53-02-00, IRM 9701 REV G & EA 503992.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A321 SRM 53-02-00, FIGURE 209 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,043 hrs · 15,351 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR52 TO FR56 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 151GFF IAW A321 SRM 53-02-00, PAR 8H, FIGURE 209 & IRM 9701 REV G.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 41,716 hrs · 15,208 cycles

CIDS CAUTION LIGHT ILLUMINATED. SERVICED R3 EMERGENCY EXIT DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 41,002 hrs · 14,888 cycles

CIDS PANEL CAUTION LIGHT ON. SERVICED 3R DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 40,930 hrs · 14,855 cycles

CIDS CAUTION LIGHT ILLUMINATED RED FOR R3 DOOR. SERVICED R3 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 40,930 hrs · 14,855 cycles

CIDS CAUTION LIGHT ILLUMINATED RED FOR R1 DOOR. SERVICED R1 DOOR ASSIST BOTTLE.

Part: LENS — BROKEN (CABIN) · airframe 39,291 hrs · 14,235 cycles

THE 4L DOOR PLASTIC "EXIT" LENS IS BROKEN & DETACHED. REPLACED EMERGENCY EXIT LENS AT 4L DOOR.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 38,875 hrs · 14,055 cycles

FIRST OFFICER'S OXYGEN MASK QUICK DONNING LEVER BROKE ON DEPLOYMENT, CAUSING CONTINUOUS FLOW OF OXYGEN. MAINTENANCE REMOVED AND REPLACED F/O'S OXYGEN MASK.

Part: FIRE BOTTLE — LOW PRESSURE (LAVATORY) · airframe 38,494 hrs · 13,908 cycles

MID LAV FIRE EXTINGUISHER BOTTLE GAUGE SHOWING RED. REPLACED MID LAV TRASH BIN FIRE EXTINGUISHER BOTTLE IAW AIRBUS MAINTENANCE MANUAL 26-25-41-401.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,460 hrs · 13,896 cycles

AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT DOES NOT BLINK PER PREFLIGHT CHECK. REPLACED BATTERY IN FLASHLIGHT. OPS CHECKED GOOD.

Part: HANDLE — BROKEN (R1 DOOR) · airframe 38,402 hrs · 13,872 cycles

R1 ENTRY/EXIT DOOR HANDLE ON THE INSIDE OF CABIN BROKEN. REMOVED AND REPLACED HANDLE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,324 hrs · 13,848 cycles

AFT EMERGENCY FLASHLIGHT APPEARS TO BE INOP. REPLACED LT AFT EMERGENCY FLASHLIGHT BATTERY.

Part: STRAP — DEFECTIVE (R3 DOOR) · airframe 37,671 hrs · 13,614 cycles

R3 DOOR SAFETY BARRIER STRAP WILL NOT RETRACT. REPLACED R3 DOOR SAFETY BARRIER STRAP PER AIRBUS MAINTENANCE MANUAL 25-65-41.

Part: LENS — MISSING (CABIN) · airframe 36,576 hrs · 13,240 cycles

FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING MISSING RED LENS. REPLACED LENS ON SEAT 9D. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 36,184 hrs · 13,100 cycles

EMERGENCY LIGHT ROW 9D MISSING LENS. REPLACED EMERGENCY LIGHT LENS.

Part: BOTTLE — LOW PRESSURE (RT DOOR) · airframe 35,776 hrs · 12,964 cycles

MX - LAX - EES - FORWARD RIGHT ENTRY DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED FORWARD RT DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 33,867 hrs · 12,274 cycles

FLT 1412 - LAX-PHL - EMERGENCY EGRESS SYSTEM - CID LIGHT ON AGAIN. 3R DOOR BOTTLE PRESSURE LOW AGAIN (HAPPENED LAST 3 DAYS). REMOVED AND REPLACED R3 DOOR ASSIST BOTTLE. SERVICED RESERVOIR TO CORRECT PRESSURE. DOOR OPERATION CHECKS GOOD.

Part: BOTTLE — LOW PRESSURE (DOOR) · airframe 33,863 hrs · 12,273 cycles

FLT 1412 - LAX-PHL - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ON. SERVICED R1 & R3 DOOR ASSIST BOTTLE IAW AMM 52-22-00. REFER TO LOGPAGE 7228089 FOR R3 DOOR ASSIST BOTTLE CORRECTIVE ACTION.

Part: BATTERY — FAULTY (CABIN) · airframe 33,423 hrs · 12,100 cycles

LOG PAGE 4652493 - FLT#1471-TPA - EEL - EMERGENCY LIGHT TEST FAULTED MID RIGHT BATTERY. MAINTENANCE REPLACED BATTERY I/A/W AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: CONTROL VALVE — DEFECTIVE (AC BAY) · airframe 32,431 hrs · 11,725 cycles

FLT 1433 - CLT - BURNING SMELL - NOTICEABLE BURNING PLASTIC ODOR THROUGHOUT CABIN, MOST PRONOUNCED IN THE AREA OF ROWS 5 & 6. MAINTENANCE REMOVED AND REPLACED THE FLOW CONTROL VALVE IAW AIRBUS MAINTENANCE MANUAL 21-51-51-04.

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - C11 - MAJOR REPAIR - CORROSION ON FORWARD CARGO SKIN CLIP AT FR35.3 BETWEEN S41L TO S42L. REPLACED FORWARD CARGO SKIN CLIP AT FR35.3 BETWEEN S41L TO S42L IAW A321 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - C11 - MAJOR REPAIR - CORROSION ON FORWARD CARGO SKIN CLIP AT FR35.3 BETWEEN S42L TO S43L. REPLACED FORWARD CARGO SKIN CLIP AT FR35.3 BETWEEN S42L TO S43L IAW A321 SRM 51-72-11.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - MAJOR REPAIR - C11 CHECK - CORROSION ON FRAME TO SKIN TIE CLIP AT FR 35.2, S41L - S42L. REPLACED FRAME TO SKIN TIE CLIP AT FR 35.2, S41L - S42L IAW A321 SRM 51-72-11 AND 51-42-1.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - MAJOR REPAIR - C11 - CORROSION ON FRAME TO SKIN TIE CLIP AT FR 34, S41L - S42L. REPLACED SKIN TIE CLIP AT FR 34, S41L - S42L IAW A321 SRM 51-72-11 AND 51-42-11.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - MAJOR REPAIR - C11 CHECK - CORROSION ON FRAME TO SKIN TIE CLIP AT FR 35.2, S42L - S43L. REPLACED FRAME TO SKIN TIE CLIP AT FR 35.2, S42L - S43L IAW A321 SRM 51-72-11 AND 51-42-11.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - MAJOR REPAIR - C11 - CORROSION ON FRAME TO SKIN TIE CLIP AT FR 35.5, S41L - S42L. REPLACED SKIN TIE CLIP AT FR 35.5, S41L - S42L IAW A321 SRM 51-72-11 AND 51-42-11.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 32,419 hrs · 11,721 cycles

PIT - MAJOR REPAIR - C11 - CORROSION ON FRAME TO SKIN TIE CLIP AT FR 35.5, S42L - S43L. REPLACED SKIN TIE CLIP AT FR 35.5, S42L - S43L IAW A321 SRM 51-72-11 AND 51-42-11.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 31,409 hrs · 11,318 cycles

FLT NR 1547- EMERGENCY EXIT LIGHT LENS MISSING AT SEAT 16C. MAINTENANCE INSTALLED EMERGENCY EXIT LIGHT LENS.

Part: CONNECTOR — DEFECTIVE (BLEED AIR SYS)

FLT 1026 TPA-CLT - ENGINE ANOMALY - AS FLIGHT WAS NEARING TOP OF CLIMB, AIRCRAFT EXPERIENCED NR 2 ENGINE BLEED FAULT. DESCENDED FROM FL370 TO FL350. SHORTLY THEREAFTER, EXPERIENCED NR 1 ENGINE BLEED FAULT WITH BOTH PACKS RUNNING OFF OF ENGINE 1 BLEED. CABIN ALTITUDE GRADUALLY BEGAN TO CLIMB AT 700 FT PER MINUTE. CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED EXPEDITED DESCENT TO FL 240. FIRST OFFICER WAS ABLE TO RESTORE BOTH ENGINE BLEEDS AND AUTO PRESSURIZATION SYSTEM BEGAN TO LOWER THE CABIN AT 750 FT PER MINUTE. CREW REQUESTED 13,000 FT AND OPERATIONS WERE NORMAL REMAINDER OF FLIGHT. OXYGEN MASKS NEVER DEPLOYED. MAINTENANCE REPLACED NR 1 AND 2 PRESSURE REGULATING VALVES IAW AIRBUS MAINTENANCE MANUAL 36-11-52; REPLACED NR 1 FAN AIR VALVE CONTROL THERMOSTAT IAW AMM 36-11-43; REPLACED NR 2 BLEED PRV CONTROL SOLENOID IAW AMM 36-11-55; REPLACED BACK SHELLS ON NR 2 ENGINE ECS HARNESS CONNECTOR 4207KS IAW AMM 71-52-43.

Part: SOLENOID — FAILED (BLEED AIR SYS) · airframe 30,184 hrs · 10,876 cycles

FLT 1026 TPA-CLT - ENGINE ANOMALY - AS FLIGHT WAS NEARING TOP OF CLIMB, AIRCRAFT EXPERIENCED NR 2 ENGINE BLEED FAULT. DESCENDED FROM FL370 TO FL350. SHORTLY THEREAFTER, EXPERIENCED NR 1 ENGINE BLEED FAULT WITH BOTH PACKS RUNNING OFF OF ENGINE 1 BLEED. CABIN ALTITUDE GRADUALLY BEGAN TO CLIMB AT 700 FT PER MINUTE. CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED EXPEDITED DESCENT TO FL 240. FIRST OFFICER WAS ABLE TO RESTORE BOTH ENGINE BLEEDS AND AUTO PRESSURIZATION SYSTEM BEGAN TO LOWER THE CABIN AT 750 FT PER MINUTE. CREW REQUESTED 13,000 FT AND OPERATIONS WERE NORMAL REMAINDER OF FLIGHT. OXYGEN MASKS NEVER DEPLOYED. MAINTENANCE REPLACED NR 1 AND 2 PRESSURE REGULATING VALVES IAW AIRBUS MAINTENANCE MANUAL 36-11-52; REPLACED NR 1 FAN AIR VALVE CONTROL THERMOSTAT IAW AMM 36-11-43; REPLACED NR 2 BLEED PRV CONTROL SOLENOID IAW AMM 36-11-55; REPLACED BACK SHELLS ON NR 2 ENGINE ECS HARNESS CONNECTOR 4207KS IAW AMM 71-52-43.

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 30,184 hrs · 10,876 cycles

FLT 1026 TPA-CLT - ENGINE ANOMALY - AS FLIGHT WAS NEARING TOP OF CLIMB, AIRCRAFT EXPERIENCED NR 2 ENGINE BLEED FAULT. DESCENDED FROM FL370 TO FL350. SHORTLY THEREAFTER, EXPERIENCED NR 1 ENGINE BLEED FAULT WITH BOTH PACKS RUNNING OFF OF ENGINE 1 BLEED. CABIN ALTITUDE GRADUALLY BEGAN TO CLIMB AT 700 FT PER MINUTE. CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED EXPEDITED DESCENT TO FL 240. FIRST OFFICER WAS ABLE TO RESTORE BOTH ENGINE BLEEDS AND AUTO PRESSURIZATION SYSTEM BEGAN TO LOWER THE CABIN AT 750 FT PER MINUTE. CREW REQUESTED 13,000 FT AND OPERATIONS WERE NORMAL REMAINDER OF FLIGHT. OXYGEN MASKS NEVER DEPLOYED. MAINTENANCE REPLACED NR 1 AND 2 PRESSURE REGULATING VALVES IAW AIRBUS MAINTENANCE MANUAL 36-11-52; REPLACED NR 1 FAN AIR VALVE CONTROL THERMOSTAT IAW AMM 36-11-43; REPLACED NR 2 BLEED PRV CONTROL SOLENOID IAW AMM 36-11-55; REPLACED BACK SHELLS ON NR 2 ENGINE ECS HARNESS CONNECTOR 4207KS IAW AMM 71-52-43.

Part: REGULATOR VALVE — FAILED (BLEED AIR SYS) · airframe 30,184 hrs · 10,876 cycles

FLT 1026 TPA-CLT - ENGINE ANOMALY - AS FLIGHT WAS NEARING TOP OF CLIMB, AIRCRAFT EXPERIENCED NR 2 ENGINE BLEED FAULT. DESCENDED FROM FL370 TO FL350. SHORTLY THEREAFTER, EXPERIENCED NR 1 ENGINE BLEED FAULT WITH BOTH PACKS RUNNING OFF OF ENGINE 1 BLEED. CABIN ALTITUDE GRADUALLY BEGAN TO CLIMB AT 700 FT PER MINUTE. CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED EXPEDITED DESCENT TO FL 240. FIRST OFFICER WAS ABLE TO RESTORE BOTH ENGINE BLEEDS AND AUTO PRESSURIZATION SYSTEM BEGAN TO LOWER THE CABIN AT 750 FT PER MINUTE. CREW REQUESTED 13,000 FT AND OPERATIONS WERE NORMAL REMAINDER OF FLIGHT. OXYGEN MASKS NEVER DEPLOYED. MAINTENANCE REPLACED NR 1 AND 2 PRESSURE REGULATING VALVES IAW AIRBUS MAINTENANCE MANUAL 36-11-52; REPLACED NR 1 FAN AIR VALVE CONTROL THERMOSTAT IAW AMM 36-11-43; REPLACED NR 2 BLEED PRV CONTROL SOLENOID IAW AMM 36-11-55; REPLACED BACK SHELLS ON NR 2 ENGINE ECS HARNESS CONNECTOR 4207KS IAW AMM 71-52-43.

Part: REGULATOR VALVE — FAILED (BLEED AIR SYS) · airframe 30,184 hrs · 10,876 cycles

FLT 1026 TPA-CLT - ENGINE ANOMALY - AS FLIGHT WAS NEARING TOP OF CLIMB, AIRCRAFT EXPERIENCED NR 2 ENGINE BLEED FAULT. DESCENDED FROM FL370 TO FL350. SHORTLY THEREAFTER, EXPERIENCED NR 1 ENGINE BLEED FAULT WITH BOTH PACKS RUNNING OFF OF ENGINE 1 BLEED. CABIN ALTITUDE GRADUALLY BEGAN TO CLIMB AT 700 FT PER MINUTE. CREW DID NOT DECLARE AN EMERGENCY BUT REQUESTED EXPEDITED DESCENT TO FL 240. FIRST OFFICER WAS ABLE TO RESTORE BOTH ENGINE BLEEDS AND AUTO PRESSURIZATION SYSTEM BEGAN TO LOWER THE CABIN AT 750 FT PER MINUTE. CREW REQUESTED 13,000 FT AND OPERATIONS WERE NORMAL REMAINDER OF FLIGHT. OXYGEN MASKS NEVER DEPLOYED. MAINTENANCE REPLACED NR 1 AND 2 PRESSURE REGULATING VALVES IAW AIRBUS MAINTENANCE MANUAL 36-11-52; REPLACED NR 1 FAN AIR VALVE CONTROL THERMOSTAT IAW AMM 36-11-43; REPLACED NR 2 BLEED PRV CONTROL SOLENOID IAW AMM 36-11-55; REPLACED BACK SHELLS ON NR 2 ENGINE ECS HARNESS CONNECTOR 4207KS IAW AMM 71-52-43.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,119 hrs · 10,851 cycles

FLT 770 - MCO - EEL - FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN FORWARD CABIN EMERGENCY FLASHLIGHT.

Part: ACTUATOR — LEAKING (R2 DOOR) · airframe 29,215 hrs · 10,578 cycles

LOG PAGE 8550961 - FLT 723-CLT - EMERGENCY EGRESS SYSTEM - CIDS CAUTION ILLUMINATED AFTER LANDING. FOUND LEAK AT SCHRADER VALVE BOSS, PIN HOLE ON FLAT FACING PRESSURE INDICATOR ALSO LEAKING AT BOSS OF PRESSURE GAUGE. REPLACED R2 DOOR ASSIST ACTUATOR PER AIRBUS MAINTENANCE MANUAL 52-22-14-04.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 29,214 hrs · 10,577 cycles

LOG PAGE 8550957 - FLT 987-PHL - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED R2 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (MID DOOR) · airframe 29,208 hrs · 10,574 cycles

LOG PAGE 8550955 - FLT 771-CLT - EMERGENCY EQUIPMENT - CIDS LIGHT ILLUMINATED. MAINTENANCE SERVICED RIGHT MID DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-11-14-04.

Part: BOTTLE — LOW PRESSURE (MID DOOR) · airframe 29,208 hrs · 10,574 cycles

LOG PAGE 8550956 - FLT 771-SFO - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ON AFTER LANDING. MAINTENANCE SERVICED RIGHT FORWARD MID ENTRY DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: LENS — MISSING (CABIN) · airframe 28,850 hrs · 10,442 cycles

FLT 910 - CLT-ORD - EMERGENCY LIGHTS - EMERGENCY LIGHT LENS ROW 9 RIGHT SIDE MISSING. INSTALLED NEW LENS ON ROW 9 RIGHT SIDE.

Part: LENS — MISSING (CABIN) · airframe 28,810 hrs · 10,422 cycles

FLT 937 - MSP-PHX - EMERGENCY LIGHTS - RED LENS IS MISSING FROM EMERGENCY LIGHT AT SEAT 10D. INSTALLED MISSING RED LENS ON SEAT 10D.

Part: LENS — WRONG PART (CABIN) · airframe 28,810 hrs · 10,422 cycles

FLT 937 - MSP-PHX - EMERGENCY LIGHTS - RED LENS ON EMERGENCY LIGHT AT SEAT 8C SHOULD BE A CLEAR LENS. REPLACED EMERGENCY LIGHT RED LENS TO CLEAR LENS AT SEAT 8C.

Part: LENS — MISSING (CABIN) · airframe 28,743 hrs · 10,391 cycles

FLT 939 - CLT - EEL - RED COVER MISSING AT 2R DOOR FLOOR LEVEL LIGHTING. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT LENS ON SEAT 9D IAW AIRBUS MAINTENANCE MANUAL 33-51-00.

Part: CONTROL UNIT — FAULTY (LANDING GEAR) · airframe 25,908 hrs · 9,419 cycles

FLT 41437 - CLT-LAX - AIR TURNBACK - THE FLIGHT CREW EXPERIENCED A LOUD, CONSTANT NOISE WITH EXCESSIVE VIBRATION AFTER TAKEOFF. THE AIRCRAFT WAS UNABLE TO CLIMB MORE THAN 500 FEET PER MINUTE AND UNABLE TO REACH SPEEDS BEYOND 280 KTS. AFTER A FLY-BY, IT WAS DETERMINED THAT THE NOSE GEAR DOORS HAD NOT RETRACTED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT. OPERATIONAL CHECK WAS GOOD. (S)

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 25,865 hrs · 9,407 cycles

FLT NR 732 SFO-CLT - EMERGENCY LANDING, LEAVING CRUISE, NR 1 ENGINE HAD POSSIBLE COMPRESSOR STALL OR OTHER VIBRATION. COULD NOT MAINTAIN POWER. OPERATED AT REDUCED THRUST WITH NO INDICATION OF VIBRATION. MAINTENANCE FOUND THE NR 1 ENGINE BEYOND LIMITS DURING BOROSCOPE. REMOVED AND REPLACED NR 1 ENGINE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 23,847 hrs · 8,739 cycles

TPA - EEL - AFT LEFT EMERGENCY EXIT POWER SUPPLY FAILED DURING SYSTEM TEST DURING WEEKLY CHECK. MAINTENANCE RESECURED MISALIGNED PIN IN ATTACH CONNECTOR AT AFT EPSU. TEST SEVERAL TIMES, SHOWED "TEST OK" MESSAGE EACH TIME.

Part: SKIN — CORRODED (FUSELAGE)

CORRODED RIVET TAILS ON FUSELAGE FORWARD CARGO COMARTMENT BETWEEN FRM 24-35 STRINGER 38L AND 38R. APPROXIMATELY 500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT MFG 4/23/2001. (K)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 1 · airframe 21,672 hrs · 21,672 cycles

FR 66 AT Y1732 HAS CORROSION. INSTALLED FILLER/DOUBLER PER SRM 53-41-14; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

CLT - THE L2 DOOR ESCAPE SLIDE INFLATION RESERVOIR PRESSURE WAS FOUND TO BE LOW. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE RESERVOIR. OK FOR SERVICE. (M)

Part: GUST DAMPER — FAILED (RT/LT ELEVATOR)

ON ARRIVAL, ELEVATORS COULD MOVE UNDAMPED FROM STOP-TO-STOP. ON INVESTIGATION, THE HYDRAULIC GUST DAMPERS WERE FOUND FULLY DISCHARGED AND INEFFECTIVE. THE RIGHT ELEVATOR NR 1 HINGE BRACKET ASSY WAS FRACTURED, REF IPC 55-50-01-05. THE RIGHT ELEVATOR FDR POSITION TRANSMITTER ROD WAS BROKEN AND SOME DAMAGE TO THE SKIN HAD OCCURRED DUE TO OVER-TRAVEL. INVESTIGATION CONTINUES. ON RECOVERY FROM STORAGE, ELEVATOR GUST DAMPERS SHOULD BE CHECKED FOR CHARGE AND LEAKAGE PRIOR TO FERRY FLIGHT (S/N E73).

Part: GUST DAMPER — FAILED (RT/LT ELEVATOR)

ON ARRIVAL, ELEVATORS COULD MOVE UNDAMPED FROM STOP-TO-STOP. ON INVESTIGATION, THE HYDRAULIC GUST DAMPERS WERE FOUND FULLY DISCHARGED AND INEFFECTIVE. THE RIGHT ELEVATOR NR 1 HINGE BRACKET ASSY WAS FRACTURED, REF IPC 55-50-01-05. THE RIGHT ELEVATOR FDR POSITION TRANSMITTER ROD WAS BROKEN AND SOME DAMAGE TO THE SKIN HAD OCCURRED DUE TO OVER-TRAVEL. INVESTIGATION CONTINUES. ON RECOVERY FROM STORAGE, ELEVATOR GUST DAMPERS SHOULD BE CHECKED FOR CHARGE AND LEAKAGE PRIOR TO FERRY FLIGHT (S/N E48).