N156UW

Part: FORK — NONE (ZONE 100) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU THE LOWER LEFT-HAND FORK END FITTING BETWEEN FR 23 AND FR 24 AT S32L NEEDS TO BE REPLACED PER THE INSTRUCTIONS ON EA 369573. REPLACED FORK END FITTING PER EA 369573.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL FORWARD CORNER SHAPE FITTING AT FR 66 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.

Part: SPLICE — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL OUTBOARD UPPER SPLICE AT FR 66 AND S23R. REPLACED SPLICE PER SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 37,126 hrs · 15,489 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 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 37,126 hrs · 15,489 cycles

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

Part: WEB — CORRODED (ZONE 200) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB BETWEEN FR 69 AND FR 70 AT S23L. REPLACED WEB PER SRM 51-42-11.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 56 AND S42L. REPAIRED STRINGER PER EA 370128

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB BETWEEN FR 69 AND FR 70 AT S23R. REPLACED WEB PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y1162.5. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING AT FR 67 AND S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPLACED LOWER SLL PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOORBEAM AT FR 20 AND -Y765. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND -Y1292. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

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

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL SKIN PANEL AT FR 56, BETWEEN S41L AND S42L. REPAIRED SKIN PANEL PER EA 370128.

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: FLASHLIGHT AT LAVATORY D IS INOPERATIVE. REPLACED FLASHLIGHT PER TASK CARD 26C22025010.

Part: FORK — WORN (ZONE 100) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: THE AFT AVIONIC COMPARTMENT RACK 80VU LOWER RIGHT-HAND FORK END FITTING BETWEEN FR 23 AND FR 24 AT S32L IS WORN. REPLACED FORK END FITTING PER EA 369573.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN PANEL DOUBLER BETWEEN FR 56 AND FR 57 AT S41L. REPAIRED SKIN PANEL PER EA 370128.

Part: ATTACH FITTING — WORN (ZONE 700) · airframe 37,126 hrs · 15,489 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEG DOOR IS LOOSE. REPLACED LEG DOOR ATTACH FITTING ON THE NOSE LANDING GEAR DOOR IAW AMM 32-22-15.

Part: PLATE — LOOSE (ZONE 800) · airframe 36,787 hrs · 15,351 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR HANDLE APPEARS LOOSE. MAINTENANCE RE-SECURED 3L EMERGENCY EXIT DOOR ARM/DISARM UNIT GRIP PLATE HANDLE PER AMM 52-22-22.

Part: LEVER — LOOSE (ZONE 800) · airframe 35,348 hrs · 14,731 cycles

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

Part: LOCK — OUT OF ADJUST (ZONE 800) · airframe 35,348 hrs · 14,731 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT LAVATORY E DOOR INOPERATIVE AND STUCK CLOSED. FLIGHT ATTENDANTS RENDERED LAVATORY UNUSABLE FOR REMAINDER OF FLIGHT. **SUPPLEMEMTAL REPORT FOR AALA202504090064: MAINTENANCE ADJUSTED THE LAVATORY DOOR LOCK MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER CMM 25-43-24.** (CLOSED)

Part: DOOR — STUCK (ZONE 900) · airframe 35,348 hrs · 14,731 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY E DOOR INOPERATIVE AND STUCK CLOSED. FLIGHT ATTENDANTS RENDERED LAVATORY UNUSABLE FOR REMAINDER OF FLIGHT. **SUPPLEMEMTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 33,730 hrs · 13,996 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE DOING JOB CARD 26L00005005, FOUND EMERGENCY POWER SUPPLY UNIT 13WL INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38-000-002-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 33,730 hrs · 13,996 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE DOING JOB CARD 26L00005005, FOUND EMERGENCY POWER SUPPLY UNIT 13WL INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-000-001-A.

Part: MECHANISM — FAULTED (NR 2 ENGINE) · airframe 33,707 hrs · 13,981 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED AN ENGINE 2 COMPRESSOR STALL ECAM MOMENTARY AND ENGINE 2 COMPRESSOR VANE ECAM MESSAGE DURING FLIGHT. MAINTENANCE REPLACED THE #2 ENGINE BLEED VALVE STOP MECHANISM PER AMM 75-31-20. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 33,511 hrs · 13,896 cycles

AIRCRAFT WAS NOT GROUNDED: ILLUMINATED EXIT SIGN ON DOOR 3L DOES NOT ILLUMINATE. REPLACED DOOR 3L EMERGENCY EXIT SIGN ASSEMBLY.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 33,387 hrs · 13,832 cycles

AIRCRAFT WAS NOT GROUNDED: ACCOMPLISHING PS CHECK EMERGENCY LIGHTING TEST FAULTED 13WL BATTERY. INSTALLED SERVICEABLE 13WL BATTERY IAW AMM 33-51-38. OPS CHECKS GOOD.

Part: VALVE — LEAKING (APU OIL) · airframe 33,345 hrs · 13,810 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED DIRTY SOCK SMELL IN THE DESCENT FROM 10000 FEET TO LANDING FROM MID CABIN TO THE AFT GALLEY. MAINTENANCE REPLACED THE APU LUBE MODULE CAP VALVE PER CMM 49-90-57. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 33,345 hrs · 13,810 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED DIRTY SOCK SMELL IN THE DESCENT FROM 10000 FEET TO LANDING FROM MID CABIN TO THE AFT GALLEY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SENSOR — OUT OF RIG (NR 2 ENGINE) · airframe 33,218 hrs · 13,755 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT DURING DESCENT AT FL 340 TO FL300 IN OPEN DECENT GOT ECAM ENGINE 2 VANE STALL WHICH WENT AWAY APPROXIMATELY 30 SECONDS, THEN GOT ENGINE 2 STALL ECAM WHICH WENT AWAY APPROXIMATELY 5-10 SECONDS, WENT TO MANAGED DESCENT AND NORMAL PARAMETERS FROM THERE ON. MAINTENANCE FOUND THE #2 ENGINE VARIABLE BLEED VALVE SENSOR OUT OF RIG AND ADJUSTED IT PER AMM 75-31-70. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED,

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 32,789 hrs · 13,557 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT LED DOES NOT FLASH. REPLACED FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT PER AMM 25-65-00.

Part: TRANSMITTER — READS LOW (NR 1) · airframe 32,367 hrs · 13,377 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TPA , AFTER TAKEOFF #1 ENGINE OIL QUANTITY DROPPED 7 QUARTS, .OIL QUANTITY REMAINED AT 8 QTS.VIB N1 2.9 N2 1.9 TECH ADVISED RETURN TO TPA. THE AIRCRAFT LANDED SAFELY AT TPA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE #1 ENGINE OIL QUANTITY TRANSMITTER PER AMM 79-31-15 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: HANDLE — LOOSE (L2 DOOR) · airframe 32,272 hrs · 13,336 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT L-2 DOOR ARM/DISARM HANDLE IS LOOSE. RE-SECURED EMERGENCY EXIT L-2 DOOR ARM/DISARM HANDLE.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 32,158 hrs · 13,287 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 2R NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT BATTERY.

Part: HANDLE — LOOSE (L2 DOOR) · airframe 31,553 hrs · 13,020 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 2L ARM/DISARM HANDLE LOOSE. RESECURED ARM HANDLE HAND GRIP.

Part: SHIM — OUT OF ADJUST (C/P DOOR STRIKER) · airframe 31,358 hrs · 12,928 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR WILL NOT OPEN W/DOOR UNLOCK LIGHT. RESHIMMED CENTER STRIKER.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 30,990 hrs · 12,744 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR: SLIDE ARMING HANDLE IS LOOSE. SECURED SLIDE ARMING HANDLE AT L2 DOOR.

Part: POWER SUPPLY — FAULTY (ZONE 200 - FUSE) · airframe 30,782 hrs · 12,639 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAULTED DURING OPERATIONAL CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38.

Part: HANDLE — UNSECURE (ZONE 800 - DOORS) · airframe 30,582 hrs · 12,550 cycles

AIRCRAFT WAS NOT GROUNDED: 2L ARMING LEVER LOOSE. SECURED 2L ARMING HANDLE.

Part: PIVOT — CRACKED (ZONE 400 - NAC/P) · airframe 29,523 hrs · 12,091 cycles

AIRCRAFT IN BASE MAINTENANCE: #2 ENGINE OUTBOARD THRUST REVERSER PIVOT FITTING CRACKED AT FASTENER 6 AND 7. REPLACED PIVOT FITTING PER GOODRICH CMM 78-32-36 REPAIR 71.

Part: SLIDE — DEFORMED (ZONE 800 - DOORS) · airframe 29,524 hrs · 12,091 cycles

AIRCRAFT IN BASE MAINTENANCE: DEFORMATION PASSENGER CREW DOOR 841 ESCAPE SLIDE AT FORWARD GALLEY AREA. REPLACED PASSENGER CREW DOOR 841 ESCAPE SLIDE AT FORWARD GALLEY AREA.

Part: SLIDE — DEFORMED (ZONE 800 - DOORS) · airframe 29,524 hrs · 12,091 cycles

AIRCRAFT IN BASE MAINTENANCE: DEFORMATION PASSENGER CREW DOOR 832 ESCAPE SLIDE AT AFT GALLEY AREA. REPLACED PASSENGER CREW DOOR 832 ESCAPE SLIDE.

Part: DOOR — BINDING (AFT LAVATORY) · airframe 27,907 hrs · 11,366 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR JAMMED. MAINTENANCE UNJAMMED AFT LEFT LAVATORY DOOR.

Part: CHIP DETECTOR — LEAKING (ZONE 400 - NAC/P) · airframe 27,069 hrs · 11,010 cycles

AIRCRAFT WAS GROUNDED: JUST AFTER LEVEL OFF AT CRUISE ENGINE 1 OIL QUANTITY LOW ADVISORY. LEVEL RANGE BETWEEN 2.5 - 3.5 QTS. WE IDLE ENG 1 FOR DURATION OF FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BZN WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE THE LEFT ENGINE MASTER CHIP DETECTOR LEAKING OIL AND REPLACED IT PER AMM 79-21-50. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SCREW — LOOSE (ZONE 800 - DOORS) · airframe 27,020 hrs · 10,989 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR WILL NOT OPEN IN FLIGHT FROM THE INSIDE. LATCH OPERATES NORMALLY. INSPECTED FLIGHT DECK DOOR AND FOUND DOOR JAMB SCREWS LOOSE, SECURED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-00.

Part: DOOR LATCH — INOPERATIVE (ZONE 800 - DOORS) · airframe 27,015 hrs · 10,986 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR WOULD NOT OPEN FROM INSIDE THE FLIGHT DECK IN FLIGHT. OPENED AT THE GATE BY MOVING FLIGHT DECK DOOR SWITCH TO UNLOCK POSITION. REPLACED FLIGHT DECK DOOR LATCH MECHANISM PER AMM 52-51-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR LATCH — INOPERATIVE (ZONE 800 - DOORS) · airframe 27,015 hrs · 10,986 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR LOCKED FROM THE INSIDE, PILOTS CANNOT GET OUT. HAD TO CRAWL THROUGH DEPRESS DOOR MAINTENANCE REPLACED FLIGHT DECK DOOR LATCH MECHANISM PER AMM 52-51-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOLT — LOOSE (ZONE 800 - DOORS) · airframe 26,735 hrs · 10,872 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT DOOR L2 ARMING LEVER LOOSE. TIGHTENED ARMING LEVER BOLT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: NONE — NONE · airframe 25,109 hrs · 10,164 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR HARD TO OPEN, DOOR LOCK LIGHT DOES NOT GO OUT SOMETIMES. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LATCH — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 25,109 hrs · 10,164 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR HARD TO OPEN, DOOR LOCK LIGHT DOES NOT GO OUT SOMETIMES. **SUPPLEMENTAL REPORT FOR AALA202112305886: ADJUSTED FLIGHT DECK DOOR LATCH MECHANISM PER AMM 52-51-00** (CLOSED)

Part: STRIKER — STICKING (ZONE 800 - DOORS) · airframe 24,864 hrs · 10,066 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR TOP DEADBOLT DOES NOT RETRACT WHEN DOOR HANDLE TURNED. **SUPPLEMENTAL REPORT FOR AALA202112036884: REPLACED FLIGHT DECK DOOR TOP STRIKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-12-400-001-A ** (CLOSED)

Part: NONE — NONE · airframe 24,864 hrs · 10,066 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR TOP DEADBOLT DOES NOT RETRACT WHEN DOOR HANDLE TURNED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)

Part: FLASHLIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 24,309 hrs · 9,827 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT INOPERATIVE AFT RIGHT FLIGHT ATTENDANT JUMPSEAT. REMOVED AND REPLACED FLASHLIGHT AT RIGHT AFT FLIGHT ATTENDANT JUMPSEAT.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 22,966 hrs · 9,248 cycles

AIRCRAFT WAS GROUNDED: MID RIGHT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY IAW AMM 33-51-38.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 22,746 hrs · 9,141 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANTS FLASHLIGHT INOPERATIVE FORWARD JUMPSEAT. REMOVED AND REPLACED FORWARD OUTBOARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT BATTERY, PER AMM 25-22-42.

Part: CONTROL PANEL — DEFECTIVE (FIRE SUPPRESSION) · airframe 22,523 hrs · 9,045 cycles

AIRCRAFT WAS NOT GROUNDED. AT TOP OF DESCENT THE APU DISCHARGE LIGHT ILLUMINATED. REPLACED FIRE PANEL 1WD AND ACCOMPLISHED A SATISACTORY OPERATIONAL CHECK PER AMM 26-12-12.

Part: ATTACH FITTING — WORN (NLG DOOR) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEG DOOR ATTACHMENT FITTING HAS EXCESSIVE PLAY / WEAR. REPLACED FITTING PER AMM 32-22-15-400-802-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE — WORN (NLG DOOR) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD HINGE ASSEMBLY HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ASSYEMBLY PER CMM 52-82-32.

Part: HINGE — WORN (NLG DOOR) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND FORWARD DOOR AFT HINGE ASSEMBLY HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ASSYEMBLY PER CMM 52-82-32.

Part: HINGE — WORN (NLG DOOR) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE ASSEMBLY HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ASSYEMBLY PER CMM 52-82-32.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE — WORN (NLG DOOR) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR AFT HINGE ASSEMBLY HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ASSYEMBLY PER CMM 52-82-32.

Part: WIRE HARNESS — CHAFED (NR 2 ENGINE) · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE - CHAFING WIRING FAN CASE AT 5 OCLOCK ON ENGINE 2. REPAIRED IDG POWER FEEDER HARNESS 4210KS ON ENGINE 2 IAW ESPM 20-53-21 PB0202 CONFIG 1 AND ESPM 20-53-29.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,449 hrs · 9,010 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,449 hrs · 9,010 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR CUT OUT LOWER SILL BETWEEN FR 61 AND FR 62 AT S38R. REPAIRED SILL PER SRM A321 53-41-49-300-003.

Part: BEARING — EXCESS PLAY (ENGINE MOUNT) · airframe 22,251 hrs · 8,929 cycles

AIRCRAFT WAS GROUNDED: WHILE ACCOMPLISHING TASK CARD 26T41571002 RIGHT ENGINE AFT MOUNT OUTBOARD LINK UPPER BEARING HAS EXCESSIVE PLAY AND WEAR. REPLACED AFT ENGINE MOUNT ASSEMBLY PER AMM 71-22-11.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 22,220 hrs · 8,919 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4L SLIDE PRESSURE LOW. MAINTENANCE REPLACED ESCAPE SLIDE PER JOBCARD 26L00025010.

Part: PRESSURE SWITCH — FAULTED (FUEL PUMP) · airframe 22,185 hrs · 8,902 cycles

AIRCRAFT NOT GROUNDED: RT TANK FUEL PUMP #1 INOP, MSG FLASHED ON, SEVERAL TIMES IN FLIGHT. MEL 28-4A, RT WING TANK PUMP. ***SUPPLEMENTAL ACTION SECT. 4 AND 5: REMOVED AND REPLACED RH FUEL PUMP PRESS. SWITCH (24QA) IAW AMM 28-21-15.***(CLOSED)

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 22,185 hrs · 8,902 cycles

AIRCRAFT NOT GROUNDED: CHECK CABIN DOOR PRESSURE AT 4L MESSAGE ON FLIGHT ATTENDANT PANEL. ACCOMPLISHED RESET AT SYST, NO FAULT AT THIS TIME IAW AMM 53-73-00. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (L4 DOOR SLIDE) · airframe 21,921 hrs · 8,795 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR CHECK SLIDE PRESSURE MESSAGE DISPLAYED. MAINTENANCE RESET SLIDE INDICATION PER AMM 52-73-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER BETWEEN FR 56 AND FR 57 AT S43L. REPAIRED STRINGER PER EA 296535.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR PANEL 261FF. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT WET AREA SHEAR PLATE CRACKED BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL CENTER SHAPE FITTING PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED SILL PER SRM 53-41-14-300-001.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 20,523 hrs · 8,241 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,979 hrs · 8,034 cycles

AIRCRAFT WAS GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131AF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-22-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,979 hrs · 8,034 cycles

AIRCRAFT WAS GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL

Part: SMOKE WARNING — FALSE INDICATION (LAVATORY) · airframe 17,386 hrs · 6,957 cycles

DURING CLIMB, RECIEVED A TRANSITORY LAVATORY SMOKE ECAM, ON SHUTDOWN AT THE GATE, RECEIVED A SMOKE MAINTENANCE STATUS MESSAGE. THE AIRCRAFT WAS GROUNDED. PERFORMED A RESET IAW AMM 26-16-00, FAULT CLEARED. NO 10-DAY HISTORY. OK FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 17,284 hrs · 6,915 cycles

EMERGENCY LIGHT COVER AT THE L4 DOOR WAS MISSING. REPLACED THE COVER IAW AMM 33-51-13.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,063 hrs · 6,835 cycles

AIRCRAFT WAS NOT GROUNDED. BOTH AFT EMERGENCY FLASHLIGHTS BATTERIES ARE DEAD. REPLACED BATTERIES IN BOTH AFT GALLEY FLASHLIGHTS.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 16,606 hrs · 6,670 cycles

EMERGENCY LIGHT POWER SUPPLY TEST FAILED. REPLACED THE POWER SUPPLY, AND BATTERY IAW AMM 33-51-38.

Part: INDICATION SYS — INOPERATIVE (L1 DOOR) · airframe 16,573 hrs · 6,655 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS CIDS CAUTION FOR DOOR 1L "CHECK SLIDE PRESSURE". PRESSURE INDICATION ON GAUGE IS IN THE GREEN. 1L SLIDE BOTTLE INDICATION INOPERATIVE. ACCOMPLISHED TSM TASK 25-62-00-810-801A. NO FAULTS FOUND.

Part: LIGHT — BROKEN (CABIN) · airframe 14,778 hrs · 5,976 cycles

SEAT ROWS 8 ABC & 30 ABC EMERGENCY LIGHTS FOUND BROKEN. REPLACED THE EMERGENCY LIGHTS IAW AMM.

Part: HANDLE — MISSING (L1 DOOR ASSIST) · airframe 14,266 hrs · 5,779 cycles

L1 DOOR ASSIST HANDLE MISSING. REPLACED THE HANDLE IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,198 hrs · 5,755 cycles

LEFT AFT DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED A LENS IAW AMM.

Part: COVER — MISSING (INDICATOR LIGHT) · airframe 13,973 hrs · 5,670 cycles

MISSING SMALL EXIT LIGHT COVER AT THE R4 DOOR BETWEEN SLIDE BUSSEL AND TRASH CAN. REINSTALLED THE DOOR SLIDE INCICATOR LIGHT COVER.

Part: MOTOR — BURNED OUT (BLOWER VENT) · airframe 13,031 hrs · 5,319 cycles

BLOWER VENT HAD FLOOR RUMBLE, THEN A HIGH PITCHED NOISE, AND AN ECAM CAUTION. RUMBLE AND NOISE STOPPED, AND A BURNED OUT MOTOR ODOR. REPLACED FWD AVIONICS BLOWER MOTOR IAW SMM 21-26-01.

Part: HANDLE — LOOSE (L2 DOOR) · airframe 13,024 hrs · 5,317 cycles

L2 DOOR ARMING LEVER ABOUT TO FALL OFF. TIGHTENED LOOSE FASTENERS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,472 hrs · 5,088 cycles

THE L4 DOOR EXIT SIGN LENS MISSING. INSTALLED NEW LENS.

Part: FAN — FAILED · airframe 11,703 hrs · 4,773 cycles

DURING DECENT, APPROX. 14,000FT HAD A RUMBLING VIBRATION SEEM TO BE IN THE NOSE OF THE AIRCRAFT FOLLOWED BY A RUBBERY/ ELECTRIC ODOR FOLLOWED BY VENT EXTRACT FAULT. MAINTENANCE REPLACED THE EXTRACT FAN IAW AMM 21-26-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (R4 DOOR) · airframe 10,370 hrs · 4,261 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4R EXIT LIGHT LENS COVER MISSING. INSTALLED LENS COVER ON 4R DOOR EXIT LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: LATCH — LACK OF LUBE (ZONE 800) · airframe 10,029 hrs · 4,144 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L GIRT BAR AFT SIDE FLOOR ATTACH POINT LATCH, FOR SLIDE ARMING, DOES NOT SPRING TO LOCK POSITION. MAINTENANCE CLEANED AND LUBRICATED THE DOOR 1L GIRT BAR AFT SIDE FLOOR ATTACH POINT LATCH SPRING PLATE AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: ENGINE — FAULTY (NR 1) · airframe 9,631 hrs · 3,989 cycles

AIRCRAFT WAS GNDED. DURING CRUISE NR 1 ENG EXPERIENCED COMPRESSOR STALL ACCOMPANIED BY HIGH EXHAUST GAS TEMPERATURES. ENG WAS SHUT DOWN. FLIGHT DIVERTED, EMER WAS DECLARED. R & R NR 1 EN IAW JOB CARD 26L40071001.

Part: LENS — BROKEN (CABIN) · airframe 9,429 hrs · 3,916 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT LENS BROKEN ON SEAT 1A-C. REPLACED LIGHT ASSEMBLY AT SEAT 1A-C IAW AMM 33-51-18.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 189 hrs · 78 cycles

LAVATORY SMOKE ALARM WENT OFF IN FLIGHT. F/A CHECKED ALL LAVS, NO ODOR OR SMOKE FOUND. ACCOMPLISHED BITE CHECK ON CIDS SYS. NO FAULTS DETECTED.