N155UW

Part: BATTERY — NO TEST (ZONE 200) · airframe 36,815 hrs · 15,240 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR, EMERGENCY POWER SUPPLY UNIT 12WL BATTERY FAILED EMERGENCY LIGHTING SYSTEM TEST PER TASK CARD 26L00025010. MAINTENANCE REPLACED THE BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-61-00 AND TASK CARD 26L00025010 WITH NO DEFECTS NOTED.

Part: FMC — FROZEN (ZONE 100) · airframe 36,422 hrs · 15,081 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DEN DUE TO THE FLIGHT CREW REPORTING MULTIPLE FAILURE MESSAGES FOR AUTO THRUST, AUTOPILOT 1 AND 2, FMGC 1 AND 2 BEING FROZEN. THE AIRCRAFT WAS OVERWEIGHT AND LANDED SAFELY AT DEN. WHILE TAXING THE #1 AND #2 MAIN TIRES DEFLATED DUE TO THE FUSE PLUGS BEING MELTED DUIRNG THE EMERGENCY BRAKING UPON LANDING. PASSENGER WERE DEPLANED ON THE TAXIWAY AND BUSED TO THE GATE. MAINTENANCE REPLACED FMGC 1 (AALA202507074158) AND 2 (AALA202507070181) PER AMM 22-83-34 DUE BOTH UNITS BEING FROZEN. THE REPLACEMENT OF BOTH FMGC UNITS WERE DETERMINED TO BE THE CAUSE OF THE FAILURE MESSAGES FOR THE AUTOPILOT 1 AND 2, AS WELL AS THE AUTOHRUST. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: FMC — FROZEN (ZONE 100) · airframe 36,422 hrs · 15,081 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DEN DUE TO THE FLIGHT CREW REPORTING MULTIPLE FAILURE MESSAGES FOR AUTO THRUST, AUTOPILOT 1 AND 2, FMGC 1 AND 2 BEING FROZEN. THE AIRCRAFT WAS OVERWEIGHT AND LANDED SAFELY AT DEN. WHILE TAXING THE #1 AND #2 MAIN TIRES DEFLATED DUE TO THE FUSE PLUGS BEING MELTED DUIRNG THE EMERGENCY BRAKING UPON LANDING. PASSENGER WERE DEPLANED ON THE TAXIWAY AND BUSED TO THE GATE. MAINTENANCE REPLACED FMGC 1 (AALA202507074158) AND 2 (AALA202507070181) PER AMM 22-83-34 DUE BOTH UNITS BEING FROZEN. THE REPLACEMENT OF BOTH FMGC UNITS WERE DETERMINED TO BE THE CAUSE OF THE FAILURE MESSAGES FOR THE AUTOPILOT 1 AND 2, AS WELL AS THE AUTOHRUST. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: FITTING — WORN (ZONE 700) · airframe 35,911 hrs · 14,845 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING BORE WORN AT FR 45 BETWEEN S41L AND S42L. REPLACED FITTING PER EA 364459.

Part: FITTING — WORN (ZONE 700) · airframe 35,911 hrs · 14,845 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR AFT FITTING BORE WORN AT FR 45 BETWEEN S41R AND S42R. REPLACED FITTING PER EA 364457.

Part: WIRE — BROKEN (ZONE 800) · airframe 35,445 hrs · 14,648 cycles

AIRCRAFT WAS GROUNDED: CABIN 1L DOOR SLIDE ARMED LIGHT ON WITH DOOR OPEN, ALONG WITH A FLIGHT ATTENDANTS PANEL CATION LIGHT. MAINTENANCE NOTED THAT A CHECK DOOR PRESSURE MESSAGE DISPLAYS DURING MOVEMENT OF THE DOOR. MAINTENANCE FOUND CONNECTOR 360RH1A HAD 2 BROKEN WIRES ON THE 1L DOOR AND REPAIRED THEM PER ESPM 20-53-29. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 23-73-00 WITH NO FAULTS NOTED.

Part: WIRE HARNESS — OUT OF POSITION (ZONE 800) · airframe 35,039 hrs · 14,463 cycles

AIRCRAFT WAS GROUNDED: FLIGTH CREW REPORTED THAT THE L1 DOOR WILL NOT ARM. MAINTENANCE REMOVED, INSPECTED AND REROUTED WIRING HARNESS ON L1 SLIDE ASSEMBLY PER AMM 25-62-44. OA SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DEU — FAULTED (ZONE 100) · airframe 34,037 hrs · 14,015 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION L1 SLIDE LOW PRESSURE DISPLAYED. MAINTENANCE REPLACED DECODER ENCODER UNIT 300RH1 (DEU) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 34,037 hrs · 14,015 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION L1 SLIDE LOW PRESSURE DISPLAYED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 33,562 hrs · 13,792 cycles

AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT STATION FLASHLIGHT INOPERATIVE. REPLACED BATTERY AND BREAK-AWAY STRAP

Part: SLAT SYSTEM — WARNING MESSAGE (ZONE 500 - LH WI) · airframe 31,392 hrs · 12,833 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. ON DEPARTURE SLATS FAULT MESSAGE GOING FROM FLAPS 2 TO FLAPS 1. THE AIRCRAFT LANDED SAFELY AT DFW. MAINTENANCE ACCOMPLISHED AN OPERATIONAL CHECK OF THE SLAT SYSTEM PER AMM 27-84-00 WITH NO DEFECTS NOTED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 31,214 hrs · 12,750 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY L DOOR DIFFICULT TO OPEN AND CLOSE. LUBED DOOR.

Part: PIN — NOT SEATED (ZONE 200 - FUSE) · airframe 30,729 hrs · 12,532 cycles

AIRCRAFT IN BASE MAINTENNCE: SEAT ROW 13ABC SEAT MOUNTED EMERGENCY ISLE LIGHT INOPERATIVE. MAINTENANCE FOUND PINS B AND C AT CONNECTOR 726VC3-A NOT FULLY SEATED . RE-SEATED PINS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PIN — NOT SEATED (ZONE 200 - FUSE) · airframe 30,729 hrs · 12,532 cycles

AIRCRAFT IN BASE MAINTENNCE: SEAT ROW 11ABC SEAT MOUNTED EMERGENCY ISLE LIGHT INOPERATIVE. MAINTENANCE FOUND PINS B AND C AT CONNECTOR 726VC3-A NOT FULLY SEATED . RE-SEATED PINS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PIN — NOT SEATED (ZONE 200 - FUSE) · airframe 30,729 hrs · 12,532 cycles

AIRCRAFT IN BASE MAINTENNCE: SEAT ROW 12ABC SEAT MOUNTED EMERGENCY ISLE LIGHT INOPERATIVE. MAINTENANCE FOUND PINS B AND C AT CONNECTOR 726VC3-A NOT FULLY SEATED . RE-SEATED PINS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 29,730 hrs · 12,073 cycles

AIRCRAFT WAS NOT GROUNDED: L1 ENTRY DOOR SLIDE ARMED INDICATION ON ECAM DOOR PAGE. ADJUSTED L1 SLIDE GIRT BAR FOLDING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FASTENER — MISSING (DOOR SLIDE) · airframe 29,724 hrs · 12,069 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 DOOR SLIDE MISSING FASTENERS AT BOTTOM OF SLIDE. REPLACED SLIDE ASSMBLY.

Part: HINGE ARM — WORN (ZONE 300 - STABS) · airframe 29,724 hrs · 12,069 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER BEARING #1 RUDDER HINGE ARM HAS TWO EACH ELONGATED FASTENER HOLES. REPLACED HINGE ARM PER SRM 51-42-11.

Part: HINGE ARM — WORN (ZONE 300 - STABS) · airframe 29,724 hrs · 12,069 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER BEARING #3 RUDDER HINGE ARM HAS 7 EACH ELONGATED FASTENER HOLES. REPLACED HINGE ARM PER SRM 51-42-11.

Part: GIRT BAR — MISINSTALLED (ZONE 800 - DOORS) · airframe 29,725 hrs · 12,069 cycles

AIRCRAFT IN BASE MAINTENANCE: L4 SLIDE GIRT BAR INSTALLED INCORRECTLY. REMOVED L4 SLIDE GIRT BAR PER AMM 25-62-44-400-006-A STEP 4.A.6, REINSTALLED L4 SLIDE GIRT BAR PER AMM 25-62-44-400-006-A STEP 4.A.1.

Part: TAB — DEBONDED (ZONE 500 - LH WI) · airframe 28,942 hrs · 11,705 cycles

AIRCRAFT WAS GROUNDED: LEFT WING OUTBOARD TRAILING EDGE FLAP TAB LOWER SURFACE PREVIOUS METAL REPAIR DEBONDED. MAINTENANCE REPLACED THE FLAP TAB PER AMM 27-54-62.

Part: ENGINE — STALLED (NR 1) · airframe 28,486 hrs · 11,501 cycles

AIRCRAFT WAS GROUNDED, ON FINAL, NR 1 ENGINE STALLED. AFTER CLEARING RUNWAY , THE TOWER ADVISED FLAMES & SMOKE. FLT CREW SHUT THE NR 1 ENGINE DOWN. MAINTENANCE DETERMINED THE SMOKE WAS DUE TO OIL LEAKING IN THE CNA, TAIL PIPE. : MAINTENANCE REPLACED THE NR 1 ENGINE IAW TASK CARD 26L40071001.

Part: TAILPIPE — LEAKING (ZONE 400 - NAC/P) · airframe 28,486 hrs · 11,501 cycles

AIRCRAFT WAS GROUNDED: ON FINAL ENGINE #1 STALLED. AFTER CLEARING RUNWAY , THE TOWER ADVISED FLAMES /SMOKE. FLIGHT CREW SHUT #1 ENGINE DOWN. MAINTENANCE DETERMINED THE SMOKE WAS DUE TO OIL LEAKING IN THE CNA /TAIL PIPE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DOOR — OUT OF POSITION (ZONE 900 - LAV/G) · airframe 27,472 hrs · 11,030 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR STUCK. PUT LAVATORY E DOOR BACK ON TRACK.

Part: ELECTRICAL BOX — FAILED (ZONE 100 - FUSE) · airframe 24,557 hrs · 9,766 cycles

AIRCRAFT WAS GROUNDED: CABIN PRESSURE SYSTEM 2 FAULT AFTER TAKE OFF AMBER SYSTEM NUMBER 2 ON ELECTRONIC CENTRALIZED AIRCRAFT MONITOR PRESSURE PAGE. SYSTEM NUMBER 1 GREEN BUT OUTFLOW VALVE APPEARED STUCK. UNABLE TO PRESSURIZE THE AIRCRAFT EVEN IN MANUAL MODE. FLIGHT DIVERTED TO LAX FLIGHT DID NOR DECLARE EMERGENCY AND WAS NOT OVERWEIGHT FOR LANDING. REMOVED ND REPLACED OUTFLOW ELECTRONIC MODULE 10HL1-A. ALSO REMOVED AND REPLACED CABIN PRESSURE CONTROLLER (AALA202109218017).

Part: CONTROLLER — FAILED (ZONE 100 - FUSE) · airframe 24,557 hrs · 9,766 cycles

AIRCRAFT WAS GROUNDED: CABIN PRESSURE SYSTEM 2 FAULT AFTER TAKE OFF AMBER SYSTEM NUMBER 2 ON ELECTRONIC CENTRALIZED AIRCRAFT MONITOR PRESSURE PAGE. SYSTEM NUMBER 1 GREEN BUT OUTFLOW VALVE APPEARED STUCK. UNABLE TO PRESSURIZE THE AIRCRAFT EVEN IN MANUAL MODE. FLIGHT DIVERTED TO LAX FLIGHT DID NOR DECLARE EMERGENCY AND WAS NOT OVERWEIGHT FOR LANDING. REMOVED ND REPLACED OUTFLOW ELECTRONIC MODULE 10HL1-A (AALA202109201661). ALSO REMOVED AND REPLACED CABIN PRESSURE CONTROLLER.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 24,551 hrs · 9,763 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE HAS HIGH RESISTANCE CAUSING NUMEROUS EMERGENCY LIGHT FAULTS. REPLACED SLIDE PER AMM 52-11-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD SYSTEM) · airframe 24,276 hrs · 9,640 cycles

AIRCRAFT WAS GROUNDED: DURING INITIAL CLIMB YELLOW HYDRAULIC RESERVOIR OVER HEAT ECAM MESSAGE OCCURRED. CREW ACCOMPLISHED ECAM NON-NORMAL PROCEDURE BUT THE OVERHEAT CONDITION PERSISTED SO THE CREW SHUT DOWN THE YELLOW HYDRAULIC PUMPS AND THE OVER HEAT CONDITION WENT AWAY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AT THE DESTINATION (DFW) WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TEST OF YELLOW HYDRAULIC SYSTEM PER AMM 29-13-0-710-002-A WITH NO FAULTS BEING NOTED.

Part: SENSOR — FAULTED (NLG STEERING) · airframe 23,344 hrs · 9,264 cycles

AIRCRAFT WAS GROUNDED: DURING DESCENT FLIGHT CREW REPORTED A NOSE WHEEL STEERINNG FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. FLIGHT CREW RESET THE SYSTEM UPON LANDING WHICH CLEARED THE FAULT AND THE AIRCRAFT TAXIED TO THE GATE. REPLACED NOSE WHEEL STEERING FEEDBACK SENSOR 4GC AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-51-19 AND 32-51-00.

Part: SLIDE — LOW PRESSURE (AFT RIGHT DOOR) · airframe 23,233 hrs · 9,219 cycles

AIRCRAFT WAS GROUNDED: AFT RIGHT SLIDE LOW PRESSURE. REPLACED R4 DOOR SLIDE PER 26L00025010.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 23,163 hrs · 9,194 cycles

AIRCRAFT NOT GROUNDED - R4 DOOR DAMPER REQUIRES SERVICE. SERVICED R4 DOOR DAMPER PER AMM 52-22-00, LEAK CHECKS GOOD, OKAY FOR SERVICE.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR HINGE FITTING HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 52-82-32-400-C01 AND CMM 52-82-32-400-805-801.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR HINGE FITTING HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 52-82-32-400-C01 AND CMM 52-82-32-400-805-801.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,590 hrs · 8,966 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: HINGE FITTING — WORN (LT ELEVATOR) · airframe 22,590 hrs · 8,966 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 (LT ELEVATOR) · airframe 22,590 hrs · 8,966 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 FITTING — WORN (LT ELEVATOR) · airframe 22,590 hrs · 8,966 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 — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY / WEAR AT RIB 2 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 22,590 hrs · 8,966 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,266 hrs · 8,823 cycles

AIRCRAFT WAS NOT GROUNDED: 4R JUMPSEAT FLASHLIGHT INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-65-00.

Part: FAN — FAILED (E&E BAY) · airframe 21,431 hrs · 8,496 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS SHORTLY BEFORE LANDING, ELECTRICAL SMELL OCCURRED IN THE COCKPIT. SHORTLY AFTER LANDING VENT EXTRACT ECAM APPEARED. FOLLOW ECAM PROCEDURE AND SELECTED EXTRACT TO OVERIDE. MAINTENANCE TROUBLESHOT IAW JOB CARD 26L00021001, FOUND AVIONICS EXTRACT FAN TO BE SOURCE OF ODOR. NO EVIDENCE OF ENGINE OR APU INGESTION. NO EVIDENCE OF OIL, HYDRAULIC, FUEL LEAK, BLEED OR ECS CONTAMINATION. REMOVED AND REPLACED AVIONICS EXTRACT FAN IAW AMM 21-26-51, OPS CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 21,028 hrs · 8,346 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS SMOKE IN LAV ECAM MSG INDICATION FOR APPROXIMATELY 5 SECONDS. PASSENGER STATED THAT SHE WAS USING PERFUME IN RIGHT AFT LAV. MAINTENANCE ACCOMPLISHED OPS TEST IAW AMM 26-17-00-710-001. NO FAULTS.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 21,017 hrs · 8,342 cycles

AIRCRAFT NOT GROUNDED: PILOT REPROTS SMOKE IN LAVATORY ALERT IN FLIGHT: NO RESIDUE FOUND IN LAV. SUSPECT PASSENGER VAPING. MAINTENANCE COMPLIED WITH TSM 26-17-00-810-804A. NO EVIDENCE OF SMOKE CONDITION NOTED. CLEANED LAV SMOKE DETECTOR FLEECE FILTERS.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CONDITION LED DID NOT ILLUMINATE DURING PERIODIC SERVICE CHECK, BATTERY DISCHARGED. REPLACED FLASHLIGHT BATTERY PER CMM 25-60-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R4 DOOR CUTOUT LOWER SILL PLATE AT FR 68 AND S23R. REPLACED SILL PLATE PER EA 295833.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L4 DOOR LOWER SILL PLATE BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PLATE PER SRM 51-72-11 AND EA 295553.

Part: SEAT TRACK — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 14 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT FR 69 AND +Y1732. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 20,903 hrs · 8,296 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT FR 69 AND +Y1732. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: LIGHT — BROKEN (CABIN) · airframe 20,715 hrs · 8,228 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT MOUNTED ON SEAT 22D WAS BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT AT SEAT 22D PER AMM 33-51-19.

Part: LIGHT — INOPERATIVE (ROW 34) · airframe 20,264 hrs · 8,056 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 34 EMERGENCY DOME LIGHT INOPERATIVE. MAINTENANCE RESECURRED GND WIRE FOR ROW 34 EMERGENCY DOME LIGHT (210WL) PER ESPM 20-44-71 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 18,672 hrs · 7,450 cycles

ECAM DISPLAYED FOR LAVATORY SMOKE FOR A FEW SECONDS. NO SMOKE OR ODOR OBSERVED. CIDS SHOWED LAVATORY A SMOKE, THEN DISPLAYED LAV SMOKE. TROUBLESHOT IAW TSM 26-17-00. CLEANED THE SMOKE DETECTOR FILTER, THE SYSTEM OPS CHECKED SATISFACTORY.

Part: LIGHT — DAMAGED (SEAT 12L) · airframe 15,821 hrs · 6,362 cycles

DURING ACCOMPLISHING A WAKE-UP CHECK, NOTED A SEAT MOUNTED EMERGENCY LIGHT AT 12L IS DAMAGED. REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT IAW AMM 33-51-18. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 15,591 hrs · 6,282 cycles

AIRCRAFT WAS NOT GROUNDED: MISSING EMERGENCY EXIT LIGHT COVER AT 4L. MAINTENANCE REPLACED LENS AT EXIT 4L.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,426 hrs · 6,219 cycles

AIRCRAFT WAS GROUNDED. ODOR DETECTED INSIDE THE MAIN CABIN AROUND SEAT ROWS 15 TO 19. ALL FOUR FLIGHT ATTENDANTS REPORTEDLY WENT TO HOSPITAL DUE TO HEADACHES. NO PASSENGER ILLNESS. ACCOMPLISHED JOB CARD 26L00021001. NO NOTICEABLE ODOR FOUND. OPERATIONAL CHECK GOOD.

Part: PANEL — INOPERATIVE (L3 DOOR) · airframe 15,333 hrs · 6,179 cycles

AIRCRAFT RETURNED TO GATE FOR AN L3 DOOR ECAM, DOOR OPEN INDICATION INOPERATIVE. REPLACED THE SLIDE ARMED PANEL FOR THE L3 DOOR IAW 52-73-21-400-003. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (DOOR) · airframe 15,312 hrs · 6,170 cycles

DOOR SLIDE LIGHT ILLUMINATED WITH SLIDE ARMED. ADJUSTED PROXIMITY SENSOR IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 14,652 hrs · 5,925 cycles

AIRCRAFT WAS GROUNDED. DURING CHECK INSPECTION, FOUND CARGO PANEL 151 MK DELAMINATED. REPLACED CARGO PANEL 151MK PER AMM 53-42-14.

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY SMOKE) · airframe 13,189 hrs · 5,391 cycles

FWD LAVATORY SMOKE ECAM WARNING ILLUMINATED BRIEFLY FOR 3-4 SECONDS, ACCOMPANIED BY A MASTER LIGHT. NO EVIDENCE OF FIRE OR SMOKE IN LAVATORY. PERFORMED A BITE TEST IAW AMM 26-17-00. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,883 hrs · 5,271 cycles

WHITE AISLE EMERGENCY LIGHT AT 20C LENS MISSING. REPLACED EMERGENCY LIGHT LENS AT 20C, OPS CHECK GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 12,553 hrs · 5,149 cycles

R4 DOOR EXIT LIGHT LENS COVER BROKEN. REPLACED EXIT LIGHT LENS COVER AT R4 DOOR IAW A321 AMM 33-51-19. AIRCRAFT NOT GROUNDED.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 11,538 hrs · 4,747 cycles

EMERGENCY LIGHT LENS COVER COMING OFF WALL. REMOVED & REPLACED LENS IAW GPM.

Part: FLOOR PANEL — CRACKED (AFT CABIN) · airframe 10,820 hrs · 4,454 cycles

GROUND CREW REPORTS A SIX INCH CRACK EMMINATING FROM A PREVIOUS REPAIR ON AFT COMPARTMENT FLOOR PANEL 151GF. AIRCRAFT GROUNDED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14.

Part: LENS — MISSING (CABIN) · airframe 10,440 hrs · 4,292 cycles

AIRCRAFT WAS NOT GROUNDED: AFT PAX DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED EXIT LIGHT LENS AT AFT PAX DOOR IAW 33-51-18.

Part: LENS — MISSING (CABIN) · airframe 10,440 hrs · 4,292 cycles

ACFT WAS NOT GROUNDED: FORWARD PAX DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED EXIT LIGHT LENS AT FORWARD PAX DOOR IAW 33-51-18.

Part: TRANSFER SYS — FAULTED (FUEL SYSTEM) · airframe 10,093 hrs · 4,152 cycles

AIRCRAFT WAS NOT GNDED. AT CRUISE ALTITUDE WE GOT FUEL ACT XFR FAULT AT FL340. FOLLOWED ECAM & QRH PROCEDURES TO XFR ACT TANK FUEL. FUEL TRANSFERRED NORMAL AT LOWER ALTITUDE FL270. ACCOMPLISHED AN ACT AUTO TRANSFER PRESSURIZATION AIR LEAK TEST IAW AMM 28-28-00-710-004A. FOUND NO LEAKS & SYS OPERATIONAL CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.

Part: LATCH — BROKEN (L3 DOOR) · airframe 9,603 hrs · 3,953 cycles

AIRCRAFT WAS GNDED. DOOR 3L ARMING LEVER BROKEN. REPLACED ARM & DISARM LATCH ASSEMBLY IAW AMM 52-22-22-000-001.

Part: SLIDE RAFT — UNSERVICEABLE (ZONE 800) · airframe 9,251 hrs · 3,813 cycles

AIRCRAFT WAS NOT GNDED. WHILE ACCOMPLISHING A SCHEDULED SLIDE TIME CHANGE, INSPECTION NOTICED THAT THE SAFETY WIRE ON THE CABLE RELEASE PAWL WAS BROKEN ON THE SLIDE THAT WAS BEING INSTALLED. THE DEFECTIVE SLIDE WAS REMOVED & RETURNED TO THE STOCKROOM & A SERVICEABLE SLIDE WAS PUT IN ITS PLACE.

Part: HANDLE — BROKEN (R1 DOOR) · airframe 8,725 hrs · 3,599 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR ASSIST HANDLE BROKEN. R & R HANDLE TRIM COVER.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 8,175 hrs · 3,376 cycles

AFTER TAKEOFF, WE RECEIVED AFT CARGO FIRE INDICATION BEFORE WE COULD COMPLETE ECAM ACTION. ECAM FOR FIRE DISAPPEARED & WAS REPLACED BY SMOKE AFT CARGO DETECTOR FAULT. FLIGHT WAS DIVERTED & AN EMER WAS DECLARED BY THE FLIGHT CREW & LANDED WITH NO INCIDENT. REPLACED THE AFT CARGO SMOKE DETECTOR NR 6 WH IAW TASK 26-16-15-000-001-A, 26-16-15-400-001-A, 26-16-00-710-001-A & OK FOR SERVICE.

Part: VALVE — LEAKING (R4 DOOR) · airframe 7,126 hrs · 2,968 cycles

FLIGHT ATTENDANT CIDS PANEL DISPLAYED 4R CHECK DOOR PRESS. FOUND FILLING VLV LEAKING PROFOUNDLY AROUND O RING. REPLACED VLV IAW AMM 52-22-00-610-801-A & SERVICE TO PROPER LEVEL.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 7,115 hrs · 2,963 cycles

CIDS PANEL MSG, CHECK DOOR PRESS FOR 4R DOOR. SERVICED 4R DOOR ASSIST BOTTLE IAW AMM 52-22-00-614-00-2A.

Part: SEAL — LEAKING (R4 ASSIST BOTTLE) · airframe 4,165 hrs · 1,786 cycles

EXCESSIVE R4 DOOR ASSIST BOTTLE SERVICING, TECHNICAL SERVICE ITEM. PERFORMED LEAK CHECK OF R4 EMER OPERATION CYLINDER IAW AMM 52-10-00-790-001A & FOUND FILLING VLV LEAKING AT BASE. R & R FILLING VLV SEAL & CLEANED DEBRIS FROM VLV BASE AREA. RECHARGED CYLINDER IAW AMM 52-10-00-614-001A. LEAK CHECKED AFTER SEVERAL HOURS GOOD.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 4,165 hrs · 1,786 cycles

DOOR SLIDE 4R INDICATES DISARMED ON FLIGHT ATTENDANTS CIDS PANEL, BUT INDICATES ARMED ON DOOR & ECAM DOOR PAGE. FLIGHT ATTENDANT REPORT TO CAPTAIN WAS INCORRECT. CIDS SHOWS DOOR ASSIST BOTTLE. LEAK CHECKED BOTTLE, NONE FOUND. SERVICED BOTTLE IAW AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 4,082 hrs · 1,754 cycles

THE R4 DOOR ASSIST BOTTLE PRESS LOW. SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 4,024 hrs · 1,729 cycles

R4 DOOR ASSIST BOTTLE NEEDS SERVICED. SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 3,810 hrs · 1,631 cycles

FLIGHT ATTENDANT ADVISED CHECK DOOR PRESS ON DOOR 4R. SERVICED DOOR ASSIST BOTTLE & MSG CLEARED. OK FOR SERVICE.

Part: LENS — BROKEN (CABIN) · airframe 3,581 hrs · 1,539 cycles

THE EMER LIGHT WHITE LENS AT SEAT 3C LENS BROKEN OFF. REPLACED LIGHT AT SEAT 3C EMER LIGHTING. OPERATIONS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 3,515 hrs · 1,513 cycles

CREW RECEIVED A CHECK DOOR PRESS ON DOOR 4R MSG ON CIDS PANEL. SERVICED DOOR ASSIST BOTTLE AS REQUIRED. DOOR 4R CHECKED OK IAW TASK AMM 52-22-00-614-022-A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 3,384 hrs · 1,461 cycles

THE 4R DOOR ASSIST BOTTLE HAS LOW PRESS. SERVICED 4R DOOR ASSIST BOTTLE. CHECKED OK IAW AMM 52-22-00-614-002A.

Part: FILTER — CLOGGED (SMOKE DETETCOR) · airframe 2,918 hrs · 1,280 cycles

CREW REPORTED A SMOKE LAVATORY DETECTOR INOPERATIVE. FOUND LAVATORY L SMOKE DETECTOR FILTER CLOGGED, CLEANED FILTER. TROUBLE SHOT SYS IAW TSM 26-17-00-810-815A. SYSTEM OPERATIONS CHECKED GOOD IAW AMM 26-17-00-710-001A.

Part: UNKNOWN — ODOR (CABIN) · airframe 2,850 hrs · 1,252 cycles

FLIGHT ATTENDANT REPORTED A CABIN ODOR. PERFORMED JOB CARD 26L00021001 TROUBLESHOOT CABIN AIR QUALITY & PERFORMED ENG RUN. ISOLATED THE PACKS & BLEED SOURCES FOR EXTENDED PERIOD OF TIME. NO ODORS DETECTED REGARDLESS OF BLEED SOURCE, PACK OR TEMPERATURE SELECTED. NO HISTORY LAST 30 DAYS.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 2,471 hrs · 1,073 cycles

CIDS PANEL REPORT SLIDE 4R PRESS LOW. SERVICED 4R DOOR ASSIST BOTTLE IAW AMM 52-22-00-614. FAULT CLEARED, OK FOR SERVICE.

Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 2,293 hrs · 987 cycles

CREW REPORTED A CLASS II MX STATUS MSG SMOKE. MX FOUND ALL LAVATORY SMOKE DETECTOR FILTERS DIRTY. REPLACED FILTERS, OPERATIONS CHECK OF LAVATORY SMOKE DETECTION SYS OK IAW AMM 26-17-15-100-003-A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 2,237 hrs · 955 cycles

REPORTED THE AFT 4R SLIDE DOOR ASSIST PRESS LOW. SERVICED ASSIST DOOR BOTTLE FOR AFT 4R DOOR IAW 52-22-00-614-002A, OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 1,957 hrs · 833 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 8C DAMAGED. R & R LIGHT ASSEMBLY, OPERATIONS CHECKED GOOD.