N189UW

Part: DOOR LATCH — OUT OF ADJUST (ZONE 800) · airframe 77,934 hrs · 30,187 cycles

AIRCRAFT WAS NOT GROUNDED: INFLIGHT AFTER 1 HOUR 45 MINUTES FLIGHT DECK DOOR WOULD NOT OPEN. IT APPEARS THE TOP AND MIDDLE LOCK ARE THE ISSUE. WE USED THE UNLOCK SWITCH ON THE CENTER PEDESTAL FLIGHT DECK DOOR SWITCH. MAINTENANCE ADJUSTED FLIGHT DECK DOOR UPPER LATCH MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-21.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 800) · airframe 77,903 hrs · 30,174 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR JAMMING. MAINTENANCE FOUND THE FLIGHT DECK DOOR CENTER LATCH TENSION ABOVE MAX ENGAGENENT AND ADJUSTED THE LATCH PER AMM 52-51-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 77,231 hrs · 29,902 cycles

AIRCRAFT WAS GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 77,231 hrs · 29,902 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: ENGINE — OVERTEMP (ZONE 400 - NAC/P) · airframe 76,568 hrs · 29,624 cycles

AIRCRAFT IN BASE MAINTENANCE: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT IMMEDIATELY AFTER TAKEOFF AN ECAM HIGH EGT ON BOTH ENGINES MESSAGE DISPLAYED. THE ECAM DIRECTED THE FLIGHT CREW TO SHUT BOTH ENGINES DOWN. THE TEMPERATURE NORMALIZED AT THRUST REDUCTION ALT. THIS WAS A MAX THRUST- BLEEDS OFF TAKEOFF AT 30 DEGREES OUTSIDE AIR TEMPERATURE WITH A TAKEOFF WEIGHT OF 195,800. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202506099830: THE DFDR DATA DOWNLOAD DATA REFLECTED THAT #1 ENGINE WAS OVER THE LIMIT OF 950 FOR 34 SECONDS AND PEAKED AT 981 DEGREES FOR 2 SECONDS PLACING THE EVENT IN AREA C. MAINTENANCE REPLACED #1 ENGIINE PER TASK CARD 26L40071001. THE DFDR DATA DOWNLOAD DATA REFLECTED THAT #2 ENGINE WAS OVER THE LIMIT OF 950 FOR 29 SECONDS AND PEAKED AT 974 DEGREES FOR 2 SECONDS PLACING THE EVENT IN AREA B. MAINTENANCE ACCOMPLISHED A BORESCOPE OF #2 ENGINE AND PLACED IT ON MARGIN WATCH WITH NO FURTHER ACTION REQUIRED AT THIS TIME. (AALA202506133643)** (CLOSED)

Part: EGT INDICATION — ILLUMINATED (BOTH ENGINES) · airframe 76,568 hrs · 29,624 cycles

AIRCRAFT IN BASE MAINTENANCE: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT IMMEDIATELY AFTER TAKEOFF AN ECAM HIGH EGT ON BOTH ENGINES MESSAGE DISPLAYED. THE ECAM DIRECTED THE FLIGHT CREW TO SHUT BOTH ENGINES DOWN. THE TEMPERATURE NORMALIZED AT THRUST REDUCTION ALT. THIS WAS A MAX THRUST- BLEEDS OFF TAKEOFF AT 30 DEGREES OUTSIDE AIR TEMPERATURE WITH A TAKEOFF WEIGHT OF 195,800. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ENGINE — OVERTEMP (ZONE 400 - NAC/P) · airframe 76,568 hrs · 29,624 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO THE FLIGHT CREW REPORTING THAT IMMEDIATELY AFTER TAKEOFF AN ECAM HIGH EGT ON BOTH ENGINES MESSAGE DISPLAYED. THE ECAM DIRECTED THE FLIGHT CREW TO SHUT BOTH ENGINES DOWN. THE TEMPERATURE NORMALIZED AT THRUST REDUCTION ALT. THIS WAS A MAX THRUST- BLEEDS OFF TAKEOFF AT 30 DEGREES OUTSIDE AIR TEMPERATURE WITH A TAKEOFF WEIGHT OF 195,800. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. **ORIGINAL REPORT WAS AALA202506099830** THE DFDR DATA DOWNLOAD DATA REFLECTED THAT #1 ENGINE WAS OVER THE LIMIT OF 950 FOR 34 SECONDS AND PEAKED AT 981 DEGREES FOR 2 SECONDS PLACING THE EVENT IN AREA C. MAINTENANCE REPLACED #1 ENGIINE PER TASK CARD 26L40071001. THE DFDR DATA DOWNLOAD DATA REFLECTED THAT #2 ENGINE WAS OVER THE LIMIT OF 950 FOR 29 SECONDS AND PEAKED AT 974 DEGREES FOR 2 SECONDS PLACING THE EVENT IN AREA B. MAINTENANCE ACCOMPLISHED A BORESCOPE OF #2 ENGINE AND PLACED IT ON MARGIN WATCH WITH NO FURTHER ACTION REQUIRED AT THIS TIME. (AALA202506133643)

Part: OVEN — ODOR (ZONE 900) · airframe 75,249 hrs · 29,017 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT OVEN #2 IS PRODUCING STRONG CHEMICAL ODOR ON DESCENT NEAR 10,000 FT. MAINTENANCE REPLACED THE OVEN PER AMM 25-35-19.

Part: HANDLE — LOOSE (ZONE 800) · airframe 75,157 hrs · 28,980 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE 2R DOOR ARMING HANDLE IS LOOSE. MAINTENANCE SECURED HANDLE PER AMM 52-22-22.

Part: SENSOR — WARNING MESSAGE (ZONE 500 FUEL) · airframe 74,948 hrs · 28,879 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A LEFT WING OVERFLOW ECAM MESSAGE DISPLAYED AND TURNED OFF LEFT TRANSFER PER ECAM PROCEDURES. MAINTENANCE REPLACED THE LEFT HAND DUAL COMPENSATOR PER AMM 28-42-46 (AALA202412032271), AS WELL AS THE LEFT HAND OVERFLOW SENSOR PER AMM 28-46-16. (AALA202412031911). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: COMPENSATOR — WARNING MESSAGE (ZONE 500 FUEL) · airframe 74,948 hrs · 28,879 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A LEFT WING OVERFLOW ECAM MESSAGE DISPLAYED AND TURNED OFF LEFT TRANSFER PER ECAM PROCEDURES. MAINTENANCE REPLACED THE LEFT HAND DUAL COMPENSATOR PER AMM 28-42-46 (AALA202412032271), AS WELL AS THE LEFT HAND OVERFLOW SENSOR PER AMM 28-46-16. (AALA202412031911). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 74,596 hrs · 28,709 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE FORWARD MEGAPHONE IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DONT PASS EMERGENCY LIGHT TEST FOR MESSAGE EPSU EXT LOAD AFT L. AFT L DOOR 832 SLIDE REPLACED.

Part: SLIDE — INOPERATIVE (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DONT PASS EMERGENCY LIGHT TEST FOR MESSAGE EPSU EXT LOAD FWD L. FWD L DOOR 831 SLIDE REPLACED.

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640JB BOLT HOLES. REPLACED ACCESS PANEL PER TASK CARD 26C64057020.

Part: ACCESS PANEL — WORN (ZONE 500) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL TANK ACCESS PANEL 540JB BOLT HOLES WORN. REPLACED ACCESS PANEL PER TASK CARD 26C54057020.

Part: GAUGE — GLAZED (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: GLAZED GAUGE ON EMERGENCY OPERATION CYLINDER DOOR DAMPER AT EMERGENCY EXIT DOOR 843. REPLACED EMERGENCY OPERATION CYLINDER DOOR DAMPER AT EMERGENCY EXIT DOOR 843 PER AMM 52-22-14-000-001-A.

Part: SPLICE — WORN (ZONE 100) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR ON SPLICE LOCATED IN PASSENGER CABIN ON FLOOR BEAM Y765 BETWEEN FR 23R TO FR 24R. REPLACED SPLICE PER SRM 51-42-11-801.

Part: GAUGE — GLAZED (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 833 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE GUAGE GLAZED. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER ASSEMBLY PER AMM 52-22-14.

Part: ROLLER — WORN (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 LOWER ROLLERS WORN (2 EACH) REPLACED ROLLERS PER AMM 52-11-31.

Part: ROLLER — WORN (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 LOWER ROLLERS WORN (2 EACH). REPLACED ROLLERS PER AMM 52-11-31.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNCTIONAL TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DAMPER — NO TEST (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DO NOT PASS OPERATIONAL TEST DOOR DAMPER DAMPING FUNCTION AT PASSENGER CREW DOOR 842. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 842

Part: FITTING — NO DISCREPANCY (ZONE 200 - FUSE) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356005. REPLACED LEFT HAND CONTINUITY FITTING PER EA 356005.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LATERAL WINDSHIELD FRAME CRACKED AT FRAME 4 RIGHT. REPLACED WINDSHIELD FRAME PER EA 356391.

Part: FITTING — NO DISCREPANCY (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356005. REPLACED RIGHT HAND CONTINUITY FITTING PER EA 356005.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LATERAL WINDSHIELD FRAME CRACKED AT FRAME 4 LEFT. REPLACED WINDSHIELD FRAME PER EA 356391.

Part: BELLCRANK — DEFORMED (ZONE 800) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ON FLEXIBLE CONTROL BELLCRANK AT PASSENGER CREW DOOR 842. REPLACED FLEXIBLE CONTROL BELLCRANKAT PASSENGER CREW DOOR 842 AND APPLIED PROTECTIVE TREATMENT.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER 31R AT LEVEL FRAME 65 RIGHT-HAND IN AFT CARGO COMPARTMENT. REPLACED STRINGER PER SRM 51-42-11-801.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT STR 23L. REPLACED SHEAR PLATE PER SRM 51-42-11-801

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23R BETWEEN FR 69 AND FR70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: DUMMY RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA DUMMY RAIL BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM +Y1292 LOCATED AT LEVEL FR 16 IN FORWARD GALLEY AREA. REPLACED FLOOR BEAM +Y1292 PER SRM 51-42-11-801.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOCATED AT RIB 10 ON RIGHT-HAND WING. PERFORMED TIME LIMITED REPAIR TRAILING EDGE TOP SKIN PANEL PER EA#356593.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: CORROSION AFT GALLEY FLOOR BEAM BETWEEN FR 68 AND FR 69 AT -Y1162. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FORWARD GALLEY AREA SEAT TRACK AT FR 20 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-15-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM LOCATED AT +Y765 AT LEVEL FR16 IN FORWARD GALLEY AREA. REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOCATED AT RIB 14 PLUS 13 INCH ON RIGHT-HAND WING. PERFORMED TIME LIMITED REPAIR TOP SKIN PANEL TRAILING EDGE PER EA#356593.

Part: FRAME ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME 71 ANGLE LOCATED BETWEEN STR 26 AND STR 31. REPLACED WITH NEW ANGLE PER SRM 51-42-11-801.

Part: FRAME — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB AFT FACE ON HORIZONTAL FLANGE RADIUS AT FR 68 AND S8R. REPAIRED FRAME PER SRM 53-41-12-300-012.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CENTER POST CRACKED BETWEEN FR 2 AND FR 3 AT Y0. REPLACED WINDSHIELD FRAME PER EA 356005.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CENTER POST CRACKED BETWEEN FR 2 AND FR 3 AT Y0. REPLACED WINDSHIELD FRAME PER EA 356005.

Part: SKIN — DEBONDED (RT TE FLAP TAB) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP TAB LOWER SURFACE SKIN PREVIOUS REPAIR DEBONDING AT 12.5 INCHES FROM TRACK 3B AND 5.5 INCHES FROM THE FRONT SPAR. REPAIRED FLAP TAB PER SRM 57-53-00-300-107.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 74,563 hrs · 28,690 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TOP SKIN TRAILING EDGE AT RIB 8. REPAIRED SKIN PER SRM 51-74-00-801,

Part: HANDLE — LOOSE (L3 DOOR) · airframe 74,362 hrs · 28,605 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARM/DISARM LEVER HANDLE IS LOOSE. MAINTENANCE SECURED LOOSE SCREW ON THE 3L DOOR ARM/DISARM LEVER HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22.

Part: LEVER — LOOSE (L3 DOOR) · airframe 73,956 hrs · 28,420 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER LOOSE. RESECURED 3L DOOR ARMING LEVER IN REFERENCE WITH AMM 52-22-22. OPS CHECK GOOD.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 73,324 hrs · 28,146 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3L ARMED LEVER LOOSE. TIGHTENED AND SECURED DOOR ARM LEVER HANDLE AT 3L DOOR.

Part: DOOR SILL — OUT OF ADJUST (LAVATORY DOORWAY) · airframe 72,669 hrs · 27,854 cycles

AIRCRAFT WAS NOT GROUNDED: FWD LAV DOOR DIFFICULT TO OPEN AND CLOSE STICKS ON BOTTOM. MAINTENANCE ADJUSTED DOOR SILL PLATE.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 72,084 hrs · 27,578 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3L ARMING LEVER LOOSE. MAINTENANCE SECURED LOOSE ARMING LEVER.

Part: DOOR — STICKING (ZONE 900 - LAV/G) · airframe 71,835 hrs · 27,449 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS DIFFICULT TO OPEN. MAINTENANCE REPAIRED FORWARD LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 71,744 hrs · 27,403 cycles

AIRCRAFT WAS NOT GROUNDED: 3R LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE. MAINTENANCE ADJUSTED DOOR AND LUBED PER AMM 52-50-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 71,240 hrs · 27,164 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3L ARMING LEVER LOOSE. SECURED 3L DOOR ARMING LEVER.

Part: DAMPER — LEAKING (ZONE 800 - DOORS) · airframe 70,756 hrs · 26,942 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER AND EMERGENCY OPERATION CYCLINDER HAS HAD MULTIPLE REPORTS OF THE PRESSURE BEING LOW. **SUPPLEMENTAL REPORT FOR AALA202304170011: REPLACED L3 DOOR DAMPER AND EMERGENCY OPERATION CYCLINDER PER AMM 52-22-14 ** (CLOSED)

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 70,756 hrs · 26,942 cycles

AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ILLUMINATED ON FLIGHT ATTENDANTS PANEL. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,756 hrs · 26,942 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER AND EMERGENCY OPERATION CYCLINDER HAS HAD MULTIPLE REPORTS OF THE PRESSURE BEING LOW. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 70,561 hrs · 26,855 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-13-14.

Part: UNKNOWN — DEFECTIVE (ZONE 500 - LH WI) · airframe 70,519 hrs · 26,839 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED. WHEN EXTENDING FLAPS 10 SLATS DID NOT MOVE. ECAM ADVISORY SLAT FAULT. LANDED FLAPS 3, SLATS 0. 165 APPROACH SPEED 160K AIRPLANE FOR LANDING. THE AIRCRAFT LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT WING SLAT ACTUATOR #7 (AALA202303146082) AND THE #1 SLAT FLAP CONTROL COMPUTER (AALA202303149582). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: COMPUTER — UNKNOWN (ZONE 100 - FUSE) · airframe 70,519 hrs · 26,839 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED. WHEN EXTENDING FLAPS 10 SLATS DID NOT MOVE. ECAM ADVISORY SLAT FAULT. LANDED FLAPS 3, SLATS 0. 165 APPROACH SPEED 160K AIRPLANE FOR LANDING. THE AIRCRAFT LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT WING SLAT ACTUATOR #7 (AALA202303146082) AND THE #1 SLAT FLAP CONTROL COMPUTER (AALA202303149582). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 70,223 hrs · 26,701 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 15WL FAILED TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR — LACK OF LUBE (FWD LAVATORY) · airframe 70,062 hrs · 26,631 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKING DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED AND LUBED FORWARD LAVATORY DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,789 hrs · 26,514 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR ASSIST SLIDE BOTTLE PRESSURE LOW. MAINTENANCE SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 69,631 hrs · 26,440 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED THE L3 DOOR ASSIST BOTTLE PER AMM 52-11-14.

Part: RESERVOIR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,225 hrs · 26,251 cycles

AIRCRAFT WAS GROUNDED: CIDS PANEL CAUTION LIGHT IS ILLUMINATED. MAINTENANCE FOUND L3 DOOR, EMERGENCY DOOR OPENER/DAMPERNER LOW. CHARGED L3 DOOR EMERGENCY RESERVOIR PER AMM 52-22-00. CIDS PANEL CAUTION LIGHT EXTINGUISHED.

Part: FLAP — DELAMINATED (ZONE 600 - RH WI) · airframe 69,167 hrs · 26,222 cycles

AIRCRAFT WAS GROUNDED: RIGHT WING OUTBOARD TRAILING EDGE FLAP ASSEMBLY HAS DELAMINATION ON THE TRAILING EDGE AT FLAP RIB 5 NEAR FLAP TRACK 3C. REPAIRED FLAP PER EA 339273.

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 68,779 hrs · 26,043 cycles

AIRCRAFT WAS NOT GROUNDED: R3 EMERGENCY POWER SUPPLY UNIT FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 68,768 hrs · 26,038 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY TEST OF EMERGENCY LIGHTS OPERATIONAL CHECK, FOUND EMERGENCY POWER SUPPLY UNIT 12WL BATTERY FAULT. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: ADIRU — INOPERATIVE (ZONE 100 - FUSE) · airframe 68,536 hrs · 25,939 cycles

AIRCRAFT WAS GROUNDED: IN CRUISE FLIGHT, #2 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) ECAM FAULT. FLIGHT CREW ACCOMPLISHED ECAM ACTIONS AND FIRST OFFICERS #3 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) WAS SELECTED. ALL FIRST OFFICERS INSTRUMENTS BLANKED AUTO PILOT OFF, AUTO THRUST OFF UNABLE TO REINSTATE ANY AIR DATA INERTIAL REFERENCE UNIT (ADIRU) ON FIRST OFFICERS SIDE REGARDLESS OF SWITCH POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #2 AIR DATA INERTIAL REFERENCE UNIT (AALA202206284284) AND #3 AIR DATA INERTIAL REFERENCE UNIT (AALA202206280681) PER AMM 34-12-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: ADIRU — INOPERATIVE (ZONE 100 - FUSE) · airframe 68,536 hrs · 25,939 cycles

AIRCRAFT WAS GROUNDED: IN CRUISE FLIGHT, #2 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) ECAM FAULT. FLIGHT CREW ACCOMPLISHED ECAM ACTIONS AND FIRST OFFICERS #3 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) WAS SELECTED. ALL FIRST OFFICERS INSTRUMENTS BLANKED AUTO PILOT OFF, AUTO THRUST OFF UNABLE TO REINSTATE ANY AIR DATA INERTIAL REFERENCE UNIT (ADIRU) ON FIRST OFFICERS SIDE REGARDLESS OF SWITCH POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #2 AIR DATA INERTIAL REFERENCE UNIT (AALA202206284284) AND #3 AIR DATA INERTIAL REFERENCE UNIT (AALA202206280681) PER AMM 34-12-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 68,324 hrs · 25,831 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION LIGHT ILLUMINATED. MAINTENANCE ACCOMPLISHED CIDS BITE CHECK PER AMM 23-73-00. CIDS 1 AND PFR INDICATED LEFT AFT EXIT BOTTLE.. CHARGED LEFT AFT EXIT DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-22-00-614-002. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 68,081 hrs · 25,718 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORT CIDS CAUTION LIGHT ON PANEL. MAINTENANCE FOUND THE LEFT AFT EMERGENCY EXIT DOOR DAMPER PRESSURE LOW, SERVICED DAMPER PER AMM 52-20-00 AND CAUTION LIGHT EXTINGUISHED ON FLIGHT ATTENDANTS PANEL.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 67,721 hrs · 25,560 cycles

AIRCRAFT WAS NOT GROUNDED: CAUTION LIGHT ILLUMINATED ON FLIGHT ATTENDANT CIDS PANEL. L3 DOOR ASSIST BOTTLE LOW. SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-20-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 67,656 hrs · 25,539 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON. 3L DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: HINGE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 67,555 hrs · 25,492 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS IN THE DOOR JAM. RE-ADJUSTED DOOR HINGE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — LOOSE (ZONE 900 - LAV/G) · airframe 67,302 hrs · 25,390 cycles

AIRCRAFT WAS NOT GROUNDED: L1 LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE. TIGHTENED AND LUBED LAVATORY DOOR.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 67,227 hrs · 25,361 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT EMERGENCY POWER SUPPLY UNIT (POSITION 12WL) AT R3 DOOR WILL NOT TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AT POSITION 12WL PER AMM 33-51-38 PAGE BLOCK 0401.

Part: SWITCH — MISSING (ZONE 800 - DOORS) · airframe 67,219 hrs · 25,359 cycles

AIRCRAFT IN BASE MAINTENANCE: L3 DOOR FRAME EVACUATION RESET PUSH BUTTON SWITCH MISSING. INSTALLED SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-00-710-026

Part: ATTACH FITTING — WORN (ZONE 700 - GEARS) · airframe 67,219 hrs · 25,359 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD ACTUATOR ATTACH FITTING HAS MIGRATED BUSHING / BORE WORN BEYOND LIMITS. REPLACED ATTACH FITTING PER EA 333151.

Part: FRAME — CRACKED (ZONE 100 - FUSE) · airframe 67,219 hrs · 25,359 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON RIGHT HAND FRAME FOOT COUPLING FASTENER HOLE AT FR 43 BETWEEN S21R AND S22R NOTED DURING ROTO-TEST INSPECTION. REPAIRED FRAME FOOT COUPLING PER EA 332940

Part: LOCK — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 67,173 hrs · 25,340 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY A DOOR JAMS. CLEAN AND LUBED DOOR LOCK PER AMM 25-40-00.

Part: LOCK — STICKING (ZONE 800 - DOORS) · airframe 67,170 hrs · 25,338 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY A DOOR JAMS, DIFFICULT TO OPEN AND CLOSE. CLEAN AND LUBE LAVATORY A DOOR LOCK, OPERATIONS CHECK GOOD PER AMM 25-40-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 67,147 hrs · 25,329 cycles

AIRCRAFT WAS GROUNDED: 4L DOOR ASSIST BOTTLE PRESSSURE 1600 PSI. SERVICED 4L DOOR ASSIST BOTTLE IAW AMM 52-10-00, OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 67,091 hrs · 25,309 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DOES NOT OPEN OR CLOSE SMOOTHLY. LUBRICATED FORWARD LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 67,065 hrs · 25,295 cycles

AIRCRAFT WAS NOT GROUNDED: 1ST CLASS LAVATORY DOOR DIFFICULT TO OPEN AT ALTITUDE. ADJUSTED AND LUBRICATED LAVATORY DOOR PER AMM 25-40-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — FAILED (ZONE 200 - FUSE) · airframe 66,988 hrs · 25,266 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PANEL FAILS EMERGENCY LIGHT SYSTEM TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202111226295), 13WL PER A321 AMM 33-51-38-0401 EMERGENCY LIGHT BUILT IN TEST EQUIPMENT TEST GOOD PER A321 AMM 33-51-00-710-001A.

Part: POWER SUPPLY — FAILED (ZONE 200 - FUSE) · airframe 66,988 hrs · 25,266 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PANEL FAILS EMERGENCY LIGHT SYSTEM TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL, 13WL (AALA202111225626) PER A321 AMM 33-51-38-0401 EMERGENCY LIGHT BUILT IN TEST EQUIPMENT TEST GOOD PER A321 AMM 33-51-00-710-001A.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,860 hrs · 25,300 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING PS CHECK FOUND L4 DOOR ASSIST BOTTLE AT 1500 PSI AT AMBIENT TEMP AT 20C. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,860 hrs · 25,300 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING PS CHECK FOUND L3 DOOR ASSIST BOTTLE AT 1500 PSI AT AMBIENT TEMP AT 20C. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001-A.

Part: FLOOR PANEL — NONE (ZONE 100 - FUSE) · airframe 66,987 hrs · 25,265 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 251HF IS DELAMINATED ON TOP CORNER. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-013.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 66,987 hrs · 25,265 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL, 251XF DELAMINATED ON CORNER. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-013.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 66,987 hrs · 25,265 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN CENTER FLOOR PANEL 231QF HAS SURFACE DELAMINATION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 66,987 hrs · 25,265 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN CENTER FLOOR PANEL 231QF HAS SURFACE DELAMINATION. **SUPPLEMENTAL REPORT FOR AALA202111094329: REPLACED FLOOR PANEL PER AMM 53-00-00.** (CLOSED)

Part: TUBE — CRACKED (FIRE BOTTLE) · airframe 66,946 hrs · 25,245 cycles

AIRCRAFT WAS NOT GROUNDED: #2 ENGINE PYLON FIRE AGENT DISCHARGE TUBE FORWARD OF COMPRESSION ROD IS CRACKED. REPLACED FIRE AGENT DISCHARGE TUBE PER AMM 26-21-49.

Part: SLIDE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,882 hrs · 25,218 cycles

AIRCRAFT WAS NOT GROUNDED: R1 PASSENGER DOOR SLIDE RESERVOIR BOTTLE BELLOW LIMITS. REMOVED AND REPLACED R1 SLIDE PER JOB 26L00025010.

Part: BUSTLE — OUT OF POSITION (ZONE 800 - DOORS) · airframe 66,848 hrs · 25,206 cycles

AIRCRAFT WAS NOT GROUNDED: 4R DOOR SLIDE BUSTLE COVER FALLING OFF. RESECURED 4R DOOR BUSTLE COVER.

Part: BOTTLE — LOW PRESSURE (L3 DOOR DAMPER) · airframe 66,740 hrs · 25,169 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER LOW PRESSURE. SERVICED L3 DOOR DAMPER PER AMM 52-22-00-614-002-A.

Part: OIL COOLER — LEAKING (APU) · airframe 66,541 hrs · 25,093 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL IN AFT CABIN. MAINTENANCE FOUND APU LEAKING OIL**SUPPLEMENTAL REPORT FOR AALA202108120940: REPLACED APU OIL COOLER ASSEMBLY AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 49-91-44** (CLOSED)

Part: OIL SYSTEM — LEAKING (APU) · airframe 66,541 hrs · 25,093 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL IN AFT CABIN. MAINTENANCE FOUND APU LEAKING OIL**SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LIGHT — MISSING (SEAT 9D) · airframe 66,517 hrs · 25,079 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY SEAT LIGHT AT 9D MISSING. INSTALLED EMERGENCY LIGHT AT SEAT 9D AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-19.

Part: BRAKE — WEAK (MLG) · airframe 66,386 hrs · 25,025 cycles

AIRCRAFT WAS GROUNDED: DURING TAXI IN WHILE ATTEMPTING TO BRAKE AIRCRAFT REQUIRED MORE PEDAL TRAVEL THAN NORMAL AND HAD A SPONGY FEEL. FOUND RESERVOIR PISTON ON 2624 GM FULLY DEPRESSED BELOW THE RED BAND . ACCOMPLISHED FILLING AND BLEEDING OF THE LOW PRESSURE CONTROL SYSTEM OF THE ALTERNATE BREAKING. OPS CHECKS NORMAL REF AMM 32-43-00-612-001-A .

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 65,941 hrs · 24,827 cycles

AIRCRAFT WAS GROUNDED: FWD CABIN EXIT SIGN LIGHTS AND EXIT MARKER LIGHTS NOT FUNCTIONING PROPERLY. REPLACED LH FWD EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-38, OPS CHECK GOOD.

Part: ACTUATOR — LOW PRESSURE (EMERGENCY EXIT) · airframe 65,814 hrs · 24,775 cycles

AIRCRAFT WAS NOT GROUNDED: CAUTION LIGHT ON CIDS PANEL. SERVICED 3L EMERGENCY EXIT DOOR ACTUATOR PER TASK CARD 26L80052003.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 65,810 hrs · 24,772 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ASSIST BOTTLE SHOWING LOW PRESSURE. SERVICED DOOR ASSIST BOTTLE IAW WORKCARD 26L80052003, OPS CHECK GOOD.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 65,782 hrs · 24,760 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT COVER AT 9D DAMAGE. REMOVED AND REPLACED 9D EMERGENCY EXIT LIGHT COVER.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 65,607 hrs · 24,687 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT CABIN INTERCOMMUNICATION DATA SYSTEM PANEL SHOWS L1 LOW PRESSURE. L1 DOOR PRESSURE NORMAL SERVICED L4 DOOR DAMPER PER AMM 52-10-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,599 hrs · 24,683 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L/1R EMERGENCY EXIT LIGHTED BLINKING OFF/ON. REMOVED AND REPLACED THE 1L EMERGENCY BATTERY POWER SUPPLY PER THE AMM 33-51-38.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,355 hrs · 24,589 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY EXIT LAMPS INOPERATIVE. REPLACED FORWARD GALLEY EMERGENCY LAMP BATTERY PER AMM 33-51-38/0401-00.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 65,296 hrs · 24,566 cycles

AIRCRAFT WAS GROUNDED: CIDS PANEL CAUTION LIGHT ILLUMINATED. FOUND L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L3 ASSIST BOTTLE PER AMM 52-22-00-614-002A.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 65,237 hrs · 24,538 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN INTERCOMMUNICATION DATA SYSTEM LIGHT ON. FOUND L3 DOOR DAMPER IN THE YELLOW BAND. SERVICE L3 DOOR DAMPER PER AMM 52-10-00.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 65,223 hrs · 24,532 cycles

AIRCRAFT WAS NOT GROUNDED: AT LEVEL OFF FORWARD LAVATORY SMOKE WARNING. FLIGHT ATTENDANT REPORTED NO ODOR OCCUPANT REPORTED NOT SMOKING OR VAPE. NO CURRENT WARNINGS OR FAULTS. ACCOMPLISHED TEST PER AMM 26-17-00. TEST OK.

Part: APU — LEAKING (ZONE 100 FUSE) · airframe 65,030 hrs · 24,444 cycles

AIRCRAFT WAS GROUNDED. MUSTY, FOUL ODOR DURING DESCENT AROUND 5,000' TO AFTER LANDING.IN COCKPIT THE ODOR CAME FROM 4 EYEBALL AIR VENTS. REPLACED APU AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ODORS NOTED, PER TASK CARDS 26L31049003 AND 26C31046016.

Part: BATTERY — INOPERATIVE (L2 FLASHLIGHT) · airframe 65,028 hrs · 24,443 cycles

AIRCRAFT WAS NOT GROUNDED. FLASHLIGHT AT 2L DOOR INOPERATIVE. REPLACED BATTERY.

Part: DAMPER — LOW PRESSURE (DOOR ASSIST) · airframe 64,764 hrs · 24,326 cycles

AIRCRAFT WAS NOT GROUNDED. CIDS CAUTION LIGHT ILLUMINATED ON FORWARD FLIGHT ATTENDANT PANEL. ACCOMPLISHED DOOR DAMPNER AND EMERGENCY OPERATION CYLINDER RECHARGE, AS PER AMM 52-22-00-614-002-A ON LEFT AFT EMERGENCY EXIT DOOR.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 64,683 hrs · 24,295 cycles

AIRCRAFT WAS GROUNDED. CABIN CABIN INTERCOMMUNICATION DATA SYSTEM PANEL RED CAUTION LIGHT ON, LIGHT EXTINGUISHED WHEN PUSHED. SERVICED PASSENGER DOOR L3 ASSIST BOTTLE, PER AMM 52-22-00-301.

Part: SEAL — LEAKING (CARGO DOOR) · airframe 64,635 hrs · 24,275 cycles

AIRCRAFT WAS GROUNDED. DURING CLIMB THROUGH 20,000 FEET, CABIN PRESSURE PUSHING 9400 AND CLIMBING. PERFORMED EMERGENCY DESCENT. FOUND FORWARD CARGO DOOR SEAL LEAKING. REMOVED AND REPLACED FORWARD CARGO DOOR SEAL, IAW AMM 52-31-18.

Part: PUMP — DEFECTIVE (HYD SYSTEM) · airframe 64,591 hrs · 24,251 cycles

AIRCRAFT WAS GROUNDED. APRROXIMATLEY 25 MINUTES OUT FROM THE SCHEDULED ARRIVAL STATION (FLL) THE BLUE ELECTRIC HYDRAULIC PUMP FAILED IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED BLUE HYDRAULIC SYSTEM ELECTRIC PUMP AND ACCOMPLISHED A SATISFACTORY LEAK AND OPERATIONAL CHECK, PER AMM 29-12-51.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 64,355 hrs · 24,161 cycles

AIRCRAFT WAS GROUNDED, L4 DOOR ASSIST BOTTLE PRESSURE LOW. NEEDS SERVICED. SERVICED BOTTLE TO SERVICEABLE PRESSURE PER AMM 12-14-00.

Part: POWER UNIT — FAILED (CABIN) · airframe 64,276 hrs · 24,125 cycles

AIRCRAFT IN BASE MAINTENANCE - EMERGENCY LIGHT SYSTEM TEST FAILED, AMM 33-51-38, EPSU BATTERY, FORWARD LEFT. REMOVED AND REPLACED POWER UNIT, OPERATION CHECKS GOOD PER AMM 33-51-38.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 63,819 hrs · 23,939 cycles

AIRCRAFT NOT GROUNDED: FLIGHT DECK SIDE WINDOW R3 HEAT ARCING INTERMITTENT WITH ELECTRICAL ODOR SMELL.***SUPPLEMENTAL ACTION SECT 4 AND 5: REMOVED AND REPLACED FO AFT FIXED WINDOW IAW AMM 56-11-12-400-002.***(CLOSED)

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 63,627 hrs · 23,868 cycles

AIRCRAFT WAS NOT GROUNDED: DURING OPERATIONS CHECK, BITE OF EMERGENCY POWER SUPPLY UNIT, EMERGENCY EXIT RIGHT FAULT DISPLAYED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER MM 33-51-38.

Part: SLIDE — OUT OF ALIGNMENT (R3 DOOR) · airframe 63,734 hrs · 23,909 cycles

AIRCRAFT WAS GROUNDED: R3 DOOR SLIDE DOOR SEPERATED FROM SLIDE ASSY AT AFT CORNER OF SLIDE DOOR BLOWN OUT. REMOVED AND REPLACED R3 DOOR SLIDE IAW W/C 25-94-02.

Part: ARMING LEVER — UNSECURE (R3 DOOR) · airframe 63,627 hrs · 23,868 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R SLIDE ARMING LEVER COMING OFF. MAINTENANCE SECURED ARMING LEVEL AT DOOR 3R PER AMM 52-20-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,571 hrs · 23,847 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT #1 JUMPSEAT WAS INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD PRACTICES.

Part: ACCUMULATOR — LOW PRESSURE (L4 DOOR) · airframe 63,348 hrs · 23,748 cycles

AIRCRAFT WAS GROUNDED: CABIN EMERGENCY DOOR ACCUMULATOR LOW AT L4 DOOR. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00-614-001-A.

Part: ACCUMULATOR — LOW PRESSURE (L3 DOOR) · airframe 63,348 hrs · 23,748 cycles

AIRCRAFT WAS GROUNDED: CABIN EMERGENCY DOOR ACCUMULATOR LOW AT L3 DOOR. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 63,259 hrs · 23,708 cycles

AIRCRAFT WAS GROUNDED: R3 DOOR ASSIST BOTTLE LOW PRESSURE.REMOVED AND REPLACED DOOR DAMPER AMD EMERGENCY OPERATION CYLINDER IAW AMM 52-22-14.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 63,249 hrs · 23,704 cycles

AIRCRAFT WAS GROUNDED: CIDS PANEL WARNING LIGHT ON. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 63,103 hrs · 23,646 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT WAS ON STEADY. MAINTENANCE SERVICED R3 DOOR ASSIST BOTTLE TO PROPER PRESSURE PER STANDARD PRACTICES.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 63,024 hrs · 23,615 cycles

AIRCRAFT WAS GROUNDED: CIDS PANEL WARNING INDICATION DISPLAYED AND RESET. MAINTENANCE SERVICED R3 EMERGENCY DOOR TO PROPER PRESSURE PER AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 62,982 hrs · 23,597 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT PANEL, CIDS CAUTION LIGHT RESET WAS NO HELP. MAINTENANCE SERVICED RIGHT EMERGENCY EXIT DOOR ASSIST BOTTLE TO PROPER PRESSURE PER MM 12-52-00.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 62,814 hrs · 23,536 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY TEST FAILED. MAINTENANCE ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 62,792 hrs · 23,528 cycles

AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT DISPLAYED DOOR PRESSURE WARNING. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-22-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,483 hrs · 23,391 cycles

AIRCRAFT NOT GROUNDED: FLASHLIGHT AT DOOR 3L NEED REPLACEMENT. REMOVED AND REPLACED BATTERY FOR FLASHLIGHT AT 3L DOOR. CKS OK. REF AMM 25-60-00.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 62,305 hrs · 23,313 cycles

AIRCRAFT NOT GROUNDED: CIDS CAUTION LIGHT ON. SERVICED R3 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERSPEED) · airframe 62,213 hrs · 23,276 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS OVER SPEED WARNING ON CONTINOUSLY AT ALTITUDE AND DECENT. ALL AIRSPEED INDICATIONS NORMAL 300 KNTS, CLEAN CONFIGURATION. MAINTENANCE ACCOMPLISHED ADIRS START PROCEDURE IAW AMM 34-10-00-860-002-A. RESET OF FWC 1(2) IAW TSM 24-00-00.

Part: ACCUMULATOR — LOW PRESSURE (EMERGENCY EXIT) · airframe 62,013 hrs · 23,196 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND EMERGENCY EXIT DOOR LOW PRESSURE. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER STANDARD PRACTICES.

Part: BATTERY — NO TEST (FWD FLASHLIGHT) · airframe 61,609 hrs · 23,042 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT 2R WAS NOT WORKING. MAINTENANCE REPLACED FLASHLIGHT BATTERY AT 2R AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-60-00.

Part: SENSOR — FAULTY (ZONE 200 - FUSE) · airframe 61,010 hrs · 22,808 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS FLIGHT RETURNED TO PHX ON ACCOUNT OF FALSE OVERSPEED WARNING. EMERGENCY DECLARED AND THE FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE CONFIRMS THE AIRCRAFT WAS IN CLEAN/FLAP UP CONFIGURATION DURING THE OVERSPEED WARNING EVENTS. MAINTENANCE SUSPECTS THE FLAP HANDLE COMMAND SENSOR AT FAULT. REMOVED AND REPLACED THE FLAP CONTROL COMMAND SENSOR UNIT IAW AMM 27-51-17. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 60,962 hrs · 22,792 cycles

AIRCRAFT WAS GROUNDED: CIDS CAUTION LIGHT ON DISPLAYED. MAINTENANCE SERVICED R3 DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-22-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R3 DOOR ASSIST) · airframe 60,837 hrs · 22,743 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR EMERGENCY ASSIST CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER 52-22-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,837 hrs · 22,743 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT LIGHT ON RIGHTHAND SEAT ROW 22 INOPERABLE. MAINTENANCE RESECURED LOOSE CONNECTOR AND REPLACED LIGHT LENS PER AMM 33-51-18 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 60,837 hrs · 22,743 cycles

AIRCRAFT IN BASE MAINTENANCE: L4 DOOR EMERGENCY ASSIST CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 60,837 hrs · 22,743 cycles

CIDS CAUTION LIGHT DISPLAYED ON FLIGHT ATTENDANT PANEL, FOR THE DOOR BOTTLE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 60,837 hrs · 22,743 cycles

DURING PREFLIGHT, THE FORWARD CIDS CAUTION LIGHT DISPLAYED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-22-00.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 1 RUDDER HINGE POINT HAD EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 7 RUDDER HINGE HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 2 RUDDER HINGE HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 5 RUDDER HINGE POINT HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 3 RUDDER HINGE POINT HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,752 hrs · 22,708 cycles

NR 4 RUDDER HINGE POINT HAD EXCESSIVE PLAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-36-41-400-001-A.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

RIGHT ELEVATOR NR 5 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

RIGHT ELEVATOR NR 4 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

RIGHT ELEVATOR NR 1 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

RIGHT ELEVATOR NR 6 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

THE RIGHT ELEVATOR NR 3 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

RIGHT ELEVATOR NR 2 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LEFT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 3 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 1 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 6 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 4 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN, THE AIRCRAFT WAS GROUNDED. REPLACED HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 5 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,752 hrs · 22,708 cycles

LEFT ELEVATOR NR 2 HINGE FITTING HAD EXCESSIVE PLAY AND WAS WORN. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 60,731 hrs · 22,696 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED R3 DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 60,624 hrs · 22,666 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR 3R DOOR ASSIST BOTTLE PRESSURE WAS LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE ON EMERGENCY DOOR 3R PER AMM 52-10-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,344 hrs · 22,562 cycles

CABIN EPSU BATTERIES FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERIES IAW AMM 33-51-11 OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 59,940 hrs · 22,395 cycles

POWER SUPPLY FAILED TO TEST ON THE CIDS PANEL. THE AIRCRAFT WAS GROUNDED. REPLACED THE POWER SUPPLY IAW AMM 33-51-38.

Part: BUSHING — WORN (LT MLG) · airframe 59,821 hrs · 22,349 cycles

FOUND SEVERAL AREAS OF WEAR AND 1 GOUGE ON THE LEFT FORWARD PINTLE PIN BEARING. ACCOMPLISHED A PERMANENT REPAIR ON THE BUSHING IAW EA 286478.

Part: SWITCH — FAULTED · airframe 59,776 hrs · 22,330 cycles

AFTER PASSING 10,000 FEET AND ACCELERATING THROUGH 250 KTS AIRCRAFT GENERATED RED OVERSPEED WARNING AND RED ECAM MAX VFE 235 KTS. AIRCRAFT WAS CLEAN WITH NO SECONDARY ISSUES. AS AIRCRAFT SLOWED BELOW 250 WARNING/ECAM SELF CLEARED. ACCELERATING ABOVE 250 WARNING RETURNED. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED 22FP SELECTION SWITCH AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: TRANSFER VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 59,682 hrs · 22,286 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM FUEL ACTIVE TRANSFER FAULT AT FLIGHT LEVEL 320, FORWARD ACTIVE QUANTITY 5280, AFT ACTIVE QUANTITY 160 PER PROCEDURE DESCENDED TO FLIGHT LEVEL 270 AND WAS ABLE TO BURN ALL ACTIVE FUEL. REPLACED ACTUATOR TRANSFER VALVE PER AMM 28-28-53-401, DUE TO NO TRANSFER SYMBOL (GREEN TRIANGLE) SHOWING DURING AUTO OR MANUAL TRANSFER. ACCOMPLISHED OPERATIONS TEST OF ACTUATOR AUTO AND MANUAL TRANSFER R SYSTEM PER AMM 28-28-00-501. OPERATIONS OK.

Part: RESERVOIR — LOW PRESSURE (EMERGENCY EXIT) · airframe 59,650 hrs · 22,273 cycles

LOW PRESSURE ON THE EMERGENCY EXIT DOOR SLIDE RESERVOIR. REPLACED THE RESERVOIR IAW AMM 25-62-49-400-001-A.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 59,650 hrs · 22,273 cycles

CRACKED FLOOR PANEL 251DG IN THE PASSENGER CABIN . REPAIRED THE FLOOR PANEL IAW EA 284760.

Part: STRUCTURE — CORRODED (FRAMES 56-57) · airframe 59,650 hrs · 22,273 cycles

CORROSION ON INTERTERNAL BASE OF ANTENNA AT FRAMES 56 TO 57, BETWEEN STRINGERS 42L TO 43L IN THE AFT CARGO BAY. REPLACED INTERNAL STRUCTURE (BASE OF ANTENNA).

Part: CONNECTOR — BROKEN (DOOR SLIDE) · airframe 59,650 hrs · 22,273 cycles

BROKEN CONNECTOR BACKSHELL FOR THE EMERGENCY EXIT DOOR SLIDE INTERNAL STRUCTURE BETWEEN FRAMES 35.1 TO 35.2A, STRINGERS 24L TO 27L. REPLACED THE CONNECTOR BACKSHELL IAW ESPM 20-30-45 PB0101, CONFIG 01, AND AWM 33-51-04.

Part: STRUT — CORRODED (RT WING TE FLAP) · airframe 59,650 hrs · 22,273 cycles

CORROSION WAS FOUND ON THE RIGHT WING INBOARD FLAP INTERCONNECTING STRUT. REPLACED IAW TC 26C67057001.

Part: STRUT — CORRODED (LT WING TE FLAP) · airframe 59,650 hrs · 22,273 cycles

CORROSION WAS FOUND ON THE LEFT WING INBOARD FLAP INTERCONNECTING STRUT. REPLACED IAW TC 26C57057001.

Part: GUSSET — CRACKED (FRAME 68) · airframe 59,650 hrs · 22,273 cycles

CRACK INDICATION ON THE GUSSET AT FRAME 68, STRINGER14L. REPLACED THE GUSSET IAW SRM 51-42-11, AND DRAWING D53480020.

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 59,650 hrs · 22,273 cycles

CRACK INDICATION ON THE FRAME 36 PRESSURE DECK PANEL Y1469.8 ON THE LOWER FUSELAGE. REPAIRED THE PRESSURE DECK PANEL IAW EA 284466.

Part: FLOOR PANEL — DELAMINATED · airframe 59,650 hrs · 22,273 cycles

DELAMINATION ON FLOOR PANEL 261DF. REPLACED IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 221DF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM, REVISION H.

Part: FITTING — EXCESS PLAY (FRAME 66) · airframe 59,650 hrs · 22,273 cycles

EXCESSIVE PLAY IN THE FITTING AT FRAME 66, STRINGER 15R. REPLACED THE FITTING IAW AMM 52-13-31-400-002-A A321

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION ON THE ACCESS PANEL 640BB, RIGHT WING BETWEEN RIBS 5 TO 6. REPLACED THE ACCESS PANEL IAW AMM 57-27-11-400-002-A.

Part: FLOOR SUPPORT — CORRODED (FRAME 47) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE FLOOR SUPPORT AT FRAME 47.1, IN THE PASSENGER CABIN. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 59,650 hrs · 22,273 cycles

DELAMINTION ON FLOOR PANEL 211JF. REPLACED THE FLOOR PANEL IAW AMM 53-12-11-400-001-A.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE SHAPE SILL IN THE AFT GALLEY AREA, FRAMES 66 TO 68, STRINGER 23L. REPLACED THE SILL IAW SRM 51-72-11 AND DRAWING D53480505.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 232FF IN THE FORWARD GALLEY, FRAMES 20 - 24. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION ON FLOOR PANEL 222CF. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE SEAT TRACK, -Y765 BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-1,1 DRAWINGS D53110920, AND D53112814.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION ON FLOOR PANEL 221EF AT FRAMES 16 TO 20, Y254 TO Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 222EF IN THE FORWARD GALLEY AREA. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, FRAMES 64 TO 66, -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472190.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 12 TO 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53110920.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,650 hrs · 22,273 cycles

FLOOR PANEL 231BF DELAMINATED BETWEEN FRAMES 20 TO 24, Y254 TOY-254 IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H .

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION WAS FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 64 AND 66, Y765. REPAIRED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DWG D53472815.

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE LOWER SUPPOERT EXISTING REPAIR, AT FRAME 66 AND STRINGER 23L IN THE AFT GALLEY. REPAIRED THE SUPPORT IAW SRM 53-41-14-300-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DRAWING 53472780.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 221PF IN THE FWD GALLEY AREA LOCATED BETWEEN FRAMES 12 - 16, Y765 AND Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIG 20106, AND IRM 9701, REV H.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND THE ON SHEAR PLATE AT STRINGER 23R, BETWEEN FRAMES 69 - 70. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DRAWING D53477180.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, +Y1292, BETWEEN FRAMES 64 AND 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DWG D53472815.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON LOWER SUPPORT BETWEEN FRAMES 66 - 68, STRINGER 23R. REPLACED THE SUPPORT IAW SRM 51-72-11, DRAWING D53480505, AND 53-41-14, REP 1.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION ON FLOOR PANEL 251WF, FRAMES 62 TO 64, Y765 TO -Y765. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 261AG IN THE AFT GALLEY BETWEEN FRAMES 64 - 66, Y254 THRU -Y254. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 59,650 hrs · 22,273 cycles

CRACK INDICATIONS FOUND ON THE INTERCOSTAL FOR DOOR STOP NR 7, FRAME 16. REPLACED THE INTERCOSTAL IAW SRM 51-72-11M, AND DRAWING D53112300.

Part: FRAME — CRACKED (FRM 20) · airframe 59,650 hrs · 22,273 cycles

FRAME 20 CRACKED, STRINGER 22R. REPAIRED THE FRAME IAW EA 283955.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 59,650 hrs · 22,273 cycles

CRACK INDICATIONS ON THE INTERCOSTAL FOR DOOR STOP 7 AT FASTENER HOLES 1 & 3, LOCATED AT FRAME 16 RIGHT. REPLACED THE INTERCOSTAL IAW SRM 51-72-11 AND DRAWING D53112300.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION ON FLOOR PANEL 262BG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW EA 284341.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 261PF IN THE AFT GALLEY AREA BETWEEN FRAMES 68 - 70, Y1292 THRU -Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIG 20106, AND IRM 9701, REV H.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,650 hrs · 22,273 cycles

DELAMINATION FOUND ON FLOOR PANEL 261BG, IN THE AFT GALLEY AREA BETWEEN FRAMES 64 - 66, Y765 TO Y1732. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION FOUND ON THE UPPER SURFACE SKIN BETWEEN RIBS 5 TO 6, STRINGER 17R ON THE RIGHT WING. REPAIRED THE SKIN IAW SRM 51-21-11-283-014.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 59,650 hrs · 22,273 cycles

CORROSION TO UPPER SURFACE EXTERNAL SKIN BETWEEN RIBS 4 TO 5, ON THE LT WING BETWEEN WING STA 2440 TO 2300. REPAIRED THE SKIN IAW EA 284511.

Part: WARNING LIGHT — ILLUMINATED (NR 2 BLEED SYS) · airframe 59,650 hrs · 22,273 cycles

NR 2 ENGINE BLEED FAULT, HOT ACRID ODOR WITH NOTABLE HEAT INCREASE IN COCKPIT TEMPERATURE NOTICED BEFORE THE NR 2 BLEED FAULT. NR 1 & 2 ENGINE BLEED SYSTEM OPS CHECKED GOOD IAW AMM 36-11-00-710-003A. ACCOMPLISHED J/C 26L00021001 WITH NO FINDINGS OF ODOR IAW TSI 00776904 MOC & MOD CONCURS AIRCRAFT OK FOR SERVICE.

Part: RESERVOIR — LOW PRESSURE (R3 DOOR SLIDE) · airframe 59,408 hrs · 22,188 cycles

R3 DOOR SLIDE PRESSURE WAS LOW. REPLACED R3 DOOR SLIDE INFLATION RESERVOIR IAW AMM 25-62-49. OPERATIONS CHECK GOOD.

Part: COVER — DETACHED (R4 DOOR SLIDE) · airframe 59,386 hrs · 22,181 cycles

R4 DOOR SLIDE COVER WOULD NOT STAY ATTACHED. MAINTENANCE ATTACHED THE DOOR SLIDE COVER IAW AMM 25-62-50, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 58,893 hrs · 22,006 cycles

THE AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO CUTOUT SILL BEAM CORRODED IN 3 AREAS. REPLACED FORWARD CARGO SILL PER SRM 41-42-11 AND DRAWING C2E53231145 AND VERIFIED RIGGING OF CARGO DOOR SWITCH PER AMM 52-71-12.

Part: STUD — MISSING (R3 DOOR SLIDE) · airframe 58,893 hrs · 22,006 cycles

THE R3 DOOR SLIDE COVER TWO STUDS WERE MISSING. REPLACED THE STUDS IAW AMM 25-24-00.

Part: STUD — MISSING (L3 DOOR SLIDE) · airframe 58,893 hrs · 22,006 cycles

THE L3 DOOR SLIDE COVER, FOUR STUDS WERE MISSING. REPLACED THE STUDS IAW AMM 25-24-00.

Part: STUD — MISSING (R2 DOOR SLIDE) · airframe 58,893 hrs · 22,006 cycles

THE R2 DOOR SLIDE COVER WAS MISSING STUDS. REPLACED THE STUDS IAW AMM 25-24-00.

Part: APU — ODOR (APU BAY) · airframe 58,811 hrs · 21,977 cycles

ROTTEN EGG, DIRTY SOCK ODOR REPORTED IN CABIN, AIR CONDITIONER R2 DOOR, LESSER EXTENT IN 1ST CLASS AND COCKPIT AREAS. THEN AFTER LANDING A FUEL/OIL ODOR WAS DETECTED. FOUND SOURCE OF CABIN ODOR TO BE APU. ACCOMPLISHED 10 MIN HIGH POWER ENGINE RUN WITH PACKS FULL HOT, NO ODORS NOTED. AIRCRAFT WAS GROUNDED. REPLACED THE APU IAW JC 26L31049003, COMPLETED TESTING.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 58,558 hrs · 21,881 cycles

EMERGENCY LIGHT LENS AT THE R2 DOOR WAS FOUND DETACHED. SECURED LENS IAW GPM 05-01.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 58,177 hrs · 21,733 cycles

CIDS CAUTION INDICATES THE L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L3 DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,983 hrs · 21,665 cycles

REPORT OF CABIN ODOR PRIOR TO FLIGHT. TROUBLESHOT CABIN AIR QUALITY IAW TASK CARD 26L00021001. PERFORMED TROUBLESHOOT AND FOUND NO ODORS DURING ENGINES AND AUXILIARY POWER UNIT RUN. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — BROKEN (SEAT 10C) · airframe 57,778 hrs · 21,588 cycles

SEAT 10C EMERGENCY LIGHT BROKEN. REPLACED THE LIGHT ASSY. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,415 hrs · 21,451 cycles

EMERGENCY LIGHT LENS AT SEAT 32C IS BROKEN. REPLACED THE LENS CHECKED OK.

Part: COVER — LOOSE (R4 DOOR SLIDE) · airframe 57,025 hrs · 21,295 cycles

SLIDE PACK COVER AT THE R4 DOOR LOOSE. SECURED SLIDE COVER AT R4 DOOR IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,625 hrs · 21,142 cycles

ISLE EMERGENCY LIGHT FIRST ROW SEAT BROKEN. REPAIRED ISLE EMERGENCY LIGHT FIRST ROW IAW AMM.

Part: SWITCH — ERRATIC (FUEL SYSTEM) · airframe 56,458 hrs · 21,066 cycles

CENTER TANK LEFT TRANSFER VALVE SHOWS CROSS LINE AMBER, POSITION DISAGREES,CLOSES IN AUTOMATIC MODE. RESET PUMP SWITCH PERFORMED OPS TEST IAW AMM. CHECKS OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,216 hrs · 20,981 cycles

L4 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED IAW AMM 33-51-13.

Part: DOUBLER — DEBONDED (RT WING TE FLAP) · airframe 55,907 hrs · 20,863 cycles

DISBONDED DOUBLER ON TRAILING EDGE FLAP TAB 137 INCHES FROM INBOARD END. REPAIRED RIGHT HAND TRAILING EDGE FLAP TAB ASSEMBLY PER AIRBUS SRM 57-53-00-300-015. AIRCRAFT WAS GROUNDED.

Part: TAB — DEBONDED (TE FLAP) · airframe 55,898 hrs · 20,861 cycles

AIRCRAFT WAS GROUNDED. DURING CREW WALK AROUND, THE CREW FOUND RIGHT OUTBOARD FLAP REPAIR DEBONDED. REPAIRED FLAP TAB PER 27-54-62.

Part: COMPUTER — FAULTY (ZONE 100) · airframe 55,862 hrs · 20,849 cycles

AIRCRAFT WAS NOT GROUNDED. AFTER THROTTLES WERE ADVANCED FOR TAKE OFF A F/CTL ELAC2 FAULT DISPLAYED ON ECAM. TAKE OFF WAS ABORTED AT APPROXIMATELY 10 KNOTS. REMOVED AND REPLACED THE ELAC2 COMPUTER IAW AMM 27-93-34. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LEVER — LOOSE (L3 DOOR ARMING) · airframe 55,738 hrs · 20,799 cycles

L3 DOOR ARMING LEVER LOOSE. SECURED ARMING LEVER.

Part: UPLOCK — FAULTY (NLG) · airframe 55,697 hrs · 20,784 cycles

AFTER TAKEOFF AND 30 MINUTES INTO FLIGHT IN THE MID FL250, IAS WAS 310 KIAS, A NOSE GEAR INDICATION SHOWED TWO RED TRIANGLE NOT UP AND LOCKED. DESCENDED ALTITUDE THAT ALLOWED SLOWING TO LESS THAN VLE. ACCOMPLISHED ECAM PROCEDURE. EXTENDED GEAR ON DOWNWIND, WITH GOOD, SAFE, DOWN & LOCKED INDICATION. UNEVENTFUL LANDING. ACCOMPLISHED TSM 32-31-00-810-827-A, WITH NO FAULTS, REMOVED AND REPLACED NLG UPLOCK 2530GM IAW AMM 32-31-21 LEAK & OPS CHECKED OK. AIRCRAFT WAS GROUNDED.

Part: BRAKE — OVERTEMP (MLG) · airframe 55,566 hrs · 20,735 cycles

DURING TAKE OFF SPEED BELOW 80KTS, HAD A HOT BRAKE ECAM MESSAGE CAME UP, ABORTED THE TAKE OFF AND CAME BACK TO THE GATE NR 4 BRAKE WAS 340 DEGREES C. MAINTENANCE INSPECTED THE BRAKES, REMOVED AND REPLACED THE NR 4 MAIN LANDING GEAR TIRE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 55,391 hrs · 20,663 cycles

EMERGENCY LIGHT LENS 9D BROKEN. REPLACED THE LENS.

Part: TERMINAL — MISSING (EMERGENCY LIGHT) · airframe 55,156 hrs · 20,565 cycles

EMERGENCY LIGHT ROW 9D FIXTURE BROKEN. FOUND MISSING TERMINAL END AND INSTALLED SEAT 9 D EMERGENCY LIGHT WIRE TERMINAL END.

Part: LIGHT — UNSECURE (CABIN) · airframe 55,137 hrs · 20,556 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT AT SEAT 9D FELL OFF. RE-INSTALLED EMERGENCY EXIT LIGHT AT SEAT 9D.

Part: LENS — LOOSE (CABIN) · airframe 55,128 hrs · 20,552 cycles

AIRCRAFT NOT GROUNDED. 10D EMERGENCY LIGHT COVER NOT SECURED. REPLACED EMERGENCY LIGHT AT SEAT 10D.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 54,970 hrs · 20,494 cycles

DAMAGE IN AFT CARGO BAY FLOOR TO DOOR SILL AT FLOOR PANEL 151GF. REPAIRED THE FLOOR PANEL IAW AMM 53-42-14.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 54,574 hrs · 20,347 cycles

L4 DOOR, SMALL EMERGENCY EXIT LIGHT COVER MISSING. REPLACED THE COVER.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 54,466 hrs · 20,308 cycles

R4 DOOR ASSIST PRESSURE LOW. SERVICED THE R4 DOOR BOTTLE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 54,466 hrs · 20,308 cycles

L4 DOOR ASSIST PRESSURE LOW. SERVICED THE R4 DOOR.

Part: LENS — MISSING (CABIN) · airframe 54,388 hrs · 20,281 cycles

AIRCRAFT NOT GROUNDED. DOOR 4R EMERGENCY EXIT LIGHT COVER MISSING. REPLACED 4R EMERGENCY EXIT LIGHT COVER AND ACCOMPLISHED SATISFACTORY OPERATION.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 54,121 hrs · 20,180 cycles

EMERGENCY EXIT SIGN BY SEAT 9D STICKING OUT. REINSTALLED EXIT SIGN BY SEAT 9D AND ACCOMPLISHED SATISFACTORY CHECK.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 53,986 hrs · 20,133 cycles

AIRCRAFT WAS NOT GROUNDED. CIDS PANEL RED LIGHT. SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHT) · airframe 53,653 hrs · 19,997 cycles

DURING NORMAL OPERATION THE EMERGENCY EXIT LIGHTS WITH THE SWITCH IN THE ARM POSITION. LIGHT DISAGREES WITH ARM SWITCH POSITION. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (14WK) IAW AMM 33-51-38. OPERATIONAL CHECKED SATISFACTORY. AIRCRAFT WAS GROUNDED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 53,513 hrs · 19,933 cycles

PLASTIC COVER OF EXIT ROW LIGHT AT 1C HAS BEEN BROKEN OFF. SECURED THE LENS.

Part: COVER — UNSECURE (CABIN) · airframe 53,484 hrs · 19,920 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT LIGHT COVER BY 2L CAME OFF. MAINTENANCE REPLACED LIGHT COVER.

Part: ENGINE — DAMAGED (NR 2) · airframe 52,886 hrs · 19,679 cycles

AIRCRAFT WAS GROUNDED, ECAM-ENGINE 2 OIL FILTER CLOGGED. REPLACED NR 2 ENGINE IAW TASK CARD 26L40071001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,716 hrs · 19,611 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT ON SEAT ROW 9DF INOPERATIVE. REPLACED EMERGENCY LIGHT LENS AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-18-400-001-A.

Part: LIGHT — DETACHED (CABIN) · airframe 52,553 hrs · 19,544 cycles

AIRCRAFT WAS GROUNDED, EMERGENCY ESCAPE LIGHT AT SEAT 9D DAMAGED. REATTACHED EMERGENCY ESCAPE LIGHT AT SEAT 9D AND ACCOMPLISHED A SATSIFACTORY OPS CHECK IAW AMM 33-51-13.

Part: ARMING LEVER — LOOSE (L3 DOOR) · airframe 51,826 hrs · 19,289 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR ARMING LEVER IS LOOSE. SECURED 3L DOOR ARMING LEVER.

Part: HYDRAULIC LINE — LEAKING (RT PYLON) · airframe 51,746 hrs · 19,254 cycles

RETURNED, ACFT WAS GNDED. FLIGHT CREW REPORTED A HYD GREEN SYS LOW LEVEL WARNING, DECLARED AN EMER & RETURNED WHERE THE ACFT LANDED SAFELY & WAS TOWED TO THE TERMINAL. FOUND A LEAKING HYD LINE IN THE RT AFT SPAR AREA PYLON. THE LINE HAD A PIN HOLE. REPAIRED THE HYD LINE & ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: FAN — FAILED (ZONE 100) · airframe 51,467 hrs · 19,150 cycles

DIVERTED, ACFT WAS GNDED. DURING CLIMB OUT CREW NOTED A LOUD FAN SOUND WHICH WENT SILENT & A BURNING ELECTRICAL SMELL. THEY ALSO NOTED THAT THE EXTRACT FAN CB HAD POPPED. THE CREW DECLARED AN EMER & LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACED THE EXTRACT FAQN & ACCOMPLISHED A SATISFACTORY OPERATIONAL. CHECK IAW AMM 21-26-51.

Part: BOLT — WORN (LE SLAT) · airframe 50,898 hrs · 18,910 cycles

AIRCRAFT IN BASE MX. RT WING SLAT NR 4, SLAT TRACK 9 HAS WEAR ON THE STOP BOLT. REPAIRED STOP BOLT IAW SRM 57-40-00-201-22.

Part: COVER — UNSECURE (CABIN) · airframe 50,841 hrs · 18,892 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT COVER AT 9E WILL NOT STAY IN PLACE. INSTALLED LIGHT COVER AT 9E.

Part: SUPPORT BRACKET — BROKEN (CABIN) · airframe 50,553 hrs · 18,792 cycles

EMERGENCY LIGHT BROKEN SEAT 9D. REPLACED 9D LIGHT SUPPORT BRACKET ASSEMBLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW CMM 25-28-72.

Part: LENS — BROKEN (CABIN) · airframe 50,452 hrs · 18,752 cycles

EMERGENCY ESCAPE PATH LIGHTING AT DOOR R2 IS BROKEN. REPLACED EMER ESCAPE PATH LIGHT LENS IAW CMM 33-50-08.

Part: LIGHT — BROKEN (CABIN) · airframe 50,437 hrs · 18,746 cycles

EMERGENCY EXIT LIGHT ON SEAT AT 9D BROKEN. SECURED EMER EXIT LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,309 hrs · 18,691 cycles

RIGHT SIDE BOX BEAM UPPER FLANGE, BOTH AFT HOLES CRACKED AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,309 hrs · 18,691 cycles

LEFT SIDE BOX BEAM UPPER FLANGE, BOTH AFT HOLES CRACKED AT FRAME 43 & +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,850 hrs · 18,497 cycles

CIDS FAULT, LT MID EMER LIGHT PSU BATTERY. REPLACED BATTERY IAW AMM 33-51-38-400-002A.

Part: LENS — MISSING (CABIN) · airframe 48,995 hrs · 18,160 cycles

ROW 1C EMER EXIT LIGHT COVER MISSING. REPLACED ROW 1C EMER EXIT LIGHT LENS.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 48,277 hrs · 17,855 cycles

EMERGENCY EXIT LIGHT ON SIDE OF SEAT 9D BENT OUTWARD INTO AISLE. LIGHT NEEDS TO BE REPOSITIONED. REPOSITIONED LIGHT AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 48,053 hrs · 17,755 cycles

EXIT LIGHT AT SEAT 9D MISSING BULB & COVER. INSTALLED LIGHT COVER. OPERATIONS CHECKED OK IAW MM 33-51-18-400-00A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,903 hrs · 17,696 cycles

ECAM MSG FOR SMOKE LAVATORY SMOKE FOR APPROX 5 SECONDS THEN EXTINGUISHED. RESET CIDS, GND SCAN OK IAW AMM 31-50-00-710-001A. SDCU CHECKED OK IAW AMM A321 26-17-00-710-001A. OK FOR SERVICE.

Part: COVER — UNSECURE (CABIN) · airframe 47,553 hrs · 17,547 cycles

EMERGENCY LIGHT AT SEAT 9D REPORTED BROKEN. SECURED LIGHT COVER IAW AMM 35-50-00.

Part: LIGHT — DETACHED (CABIN) · airframe 47,485 hrs · 17,519 cycles

EMERGENCY LIGHT AT SEAT 9D NEEDS REATTACHED. SECURED EMER LIGHT AT SEAT 9D.

Part: CONNECTOR — UNSECURE (ZONE 100) · airframe 46,767 hrs · 17,227 cycles

DURING FLIGHT CREW REPORTED RUNAWAY HEAT. MAXIMUM FWD TRIM TEMP GOT TO 152 & COCKPIT TEMP REACHED 102. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. FOUND LOOSE CONNECTOR ON LT INLET ACTUATOR. SECURED CONNECTOR. ACFT OK FOR SERVICE.

Part: APU — ODOR (APU BAY) · airframe 46,749 hrs · 17,220 cycles

A STRONG MOLD ODOR STARTING AT ROWS 26 & AFT. TROUBLE SHOT IAW JOB CARD 26L00021001 & 26L00021002. VERIFIED APU IS AT FAULT. ACFT PLACED ON MEL 49-10-01A. RAN APU, LT & RT PACKS FOR ONE HOUR. INSPECTED FOR LEAKS, NONE FOUND & NO ODOR DETECTED. THIS CLEARS MEL 49-10-01A.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 46,733 hrs · 17,216 cycles

EMERGENCY LIGHT TEST DOES NOT PASS. R & R MID CABIN EPSU, LT SIDE 15WL IAW AMM 33-51-38-000-001-A & 33-51-38-400-001-A. R & R BATTERY IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPERATIONS OK. ACFT OK FOR SERVICE.

Part: MECHANISM — DIRTY (R4 DOOR) · airframe 46,622 hrs · 17,170 cycles

DOOR 4R TOUGH TO DISARM BY CABIN CREW. INSPECTED DOOR 4R ARMING MECHANISM. CLEANED AREA AS NEEDED. DOOR 4R ARMING MECHANISM, OPERATIONS NORMAL AT THIS TIME.

Part: CIRCUIT BREAKER — POPPED (ZONE 200 - FUSE) · airframe 45,762 hrs · 16,843 cycles

DURING COCKPIT SETUP, THEY RECEIVED AN ECAM MESSAGE CB J R. FOUND CB P10 SLIDES ARM GND POPPED. RESET CB P10 & PERFORMED OPERATIONS CHECK ON ALL CABIN DOOR ARM SYS LIGHTS. NO FAULTS AT THIS TIME.

Part: LENS — MISSING (EXIT SIGN) · airframe 45,589 hrs · 16,777 cycles

THE LENS IS MISSING FROM THE EMER EXIT SIGN AT THE BOTTOM OF DOOR 4L.. INSTALLED LENS FOR EMER LIGHT AT DOOR 4L.

Part: SLIDE — SHORTED (L2 DOOR) · airframe 44,519 hrs · 16,330 cycles

EMERGENCY POWER SUPPLY UNIT FAULT. THE L2 DOOR SLIDE BAD & SHORTED. R & R L2 DOOR SLIDE ASSEMBLY IAW 26L00025012.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 44,519 hrs · 16,330 cycles

EMERGENCY LIGHT FAILED TEST, EMERGENCY POWER SUPPLY UNIT FAIL INT LOAD MID LT, EPSU EXT LOAD MID LT. REPLACED EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-35, OPERATIONS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 44,039 hrs · 16,127 cycles

CREW REPORTED THE EMERGENCY EXIT LIGHT COVER MISSING AT SEAT 21C. REPLACED LENS AT SEAT 21C.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 43,472 hrs · 15,885 cycles

EXIT LENS COVER MISSING AT 4R DOOR. REPLACED EXIT LENS COVER AT 4R DOOR.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 43,333 hrs · 15,815 cycles

L2 DOOR ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE IAW AMM 52-22-00-614.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 43,333 hrs · 15,816 cycles

R3 DOOR ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE IAW AMM 52-22-00-614.

Part: LIGHT — UNKNOWN (CABIN) · airframe 43,099 hrs · 15,721 cycles

L2 DOOR EXIT LIGHT ABOVE DOOR INOPERATIVE. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-00-710-008-A, NO FAULTS FOUND.

Part: LIGHT — UNKNOWN (CABIN) · airframe 43,099 hrs · 15,721 cycles

L2 DOOR EXIT LIGHT INOPERATIVE. ACCOMPLISHED OPS CHECK IAW AMM 33-51-00-710-008-A. NO FAULTS FOUND.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 43,043 hrs · 15,697 cycles

ON PREFLIGHT, AFT CABIN MEGAPHONE INOPERATIVE. REPLACED AFT MEGAPHONE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 42,078 hrs · 15,310 cycles

DIVERTED TO MSY DUE TO STRONG ODOR IN COCKPIT AND CABIN. CREW FOLLOWED QRH FUMES PROCEDURE. ODOR DISSIPATED SLIGHTLY BUT FLIGHT ATTENDANT SAID PASSENGERS CONTINUED TO COMPLAIN OF HEALTH CONCERNS. TROUBLESHOOT CABIN AIR QUALITY JOB CARD PERFORMED WITH NO POSITIVE FINDINGS. AIRCRAFT WAS FERRIED TO CLT, CREW REPORTED NO ODOR IN COCKPIT OR CABIN THROUGHOUT FLIGHT.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 42,069 hrs · 15,308 cycles

FLIGHT DIVERTED TO MSY DUE TO STRONG ODOR IN COCKPIT AND CABIN. CREW FOUND ODOR TO BE UNBEARABLE AND ALL FOUR DEVELOPED HEADACHES AND SCRATCHY THROATS. PERFORMED TROUBLESHOOT CABIN AIR QUALITY JOB CARD WITH NO POSITIVE FINDINGS. DURING FERRY TO CLT, NO ODOR IN COCKPIT OR CABIN NOTED.

Part: PROXIMITY SWITCH — FAULTY (R4 DOOR) · airframe 41,380 hrs · 14,980 cycles

CREW REPORTED THE 4R DOOR SLIDE SHOWS DISARMED ON ECAM. ARMING HANDLE RECYCLED - STILL SHOWS DISARMED AND CABIN PRESSURE LIGHT ON DOOR FLASHING. SOMETIME DURING DESCENT DOOR SHOWED REARMED. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH (7WN2) ON 4R DOOR IAW AMM 52-73-11-400-002-A. OPS CHECK NORMAL. ALSO, REMOVED AND REPLACED RELAYS 18WN1 AND 18WN2 IAW SWPM 20-46-50. NO FURTHER FAULTS NOTED. OK FOR SERVICE.

Part: FIRE BOTTLE — LOW (LAVATORY) · airframe 40,647 hrs · 14,652 cycles

FOUND MID LAV FIRE BOTTLE WEIGHT LOW. REMOVED AND REPLACED MID LAV FIRE BOTTLE IAW AIRBUS MAINTENANCE MANUAL 26-25-41-400-001A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,264 hrs · 14,481 cycles

2S CHECK - EMERGENCY LIGHT TEST FAILS ON PROGRAMMING TEST PANEL. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW A321 AMM 33-51-38. PERFORMED EMERGENCY LIGHT TEST IAW A321 AMM 33-51-00-710-001-A CHECKED GOOD.

Part: LENS — BROKEN (CABIN) · airframe 40,264 hrs · 14,481 cycles

2S CHECK - CABIN WALL MOUNTED L2 DOOR EMERGENCY EXIT SIGN LENS COVER BROKEN. REPLACED CABIN WALL MOUNTED L2 DOOR EMERGENCY EXIT SIGN LENS COVER IAW A321 AMM 33-51-13.

Part: LENS — BROKEN (CABIN) · airframe 40,264 hrs · 14,481 cycles

2S CHECK - CABIN WALL MOUNTED L4 DOOR EMERGENCY EXIT SIGN LENS COVER BROKEN. REPLACED CABIN WALL MOUNTED L4 DOOR EMERGENCY EXIT SIGN LENS COVER IAW A321 AMM 33-51-13.

Part: LENS — BROKEN (CABIN) · airframe 40,264 hrs · 14,481 cycles

2S CHECK - CABIN WALL MOUNTED R2 DOOR EMERGENCY EXIT SIGN LENS COVER BROKEN. REPLACED CABIN WALL MOUNTED R2 DOOR EMERGENCY EXIT SIGN LENS COVER IAW A321 AMM 33-21-13.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 40,264 hrs · 14,481 cycles

2S CHECK - L1 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RESEATED EMERGENCY LIGHT CONNECTOR AND PERFORMED OPS TEST IAW A321 AMM 33-51-00-710-008, TEST GOOD.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,264 hrs · 14,481 cycles

2S CHECK - GALVANIC CORROSION ON PROFILE CORNER BETWEEN FR56 TO FR58, S23R. REPLACED PROFILE CORNER BETWEEN FR56 TO FR58, S23R IAW A321 SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,264 hrs · 14,481 cycles

2S CHECK - GALVANIC CORROSION ON SCUFF PLATE SUPPORT BETWEEN FR16 TO FR20, S23R, -Y1732 PLUS 5 INCHES. REPLACED SCUFF PLATE SUPPORT BETWEEN FR16 TO FR20, S23R, -Y1732 IAW A321 SRM 51-73-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,264 hrs · 14,481 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR39 TO FR46, Y1292. REPLACED SEAT TRACK BETWEEN FR39 TO FR46, Y1292 IAW A321 SRM 51-74-00, 53-31-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,264 hrs · 14,481 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR47, -Y756. REPLACED SEAT TRACK AT FR47, -Y756 IAW A321 SRM 53-31-15 FIG 103, 51-54-11, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,264 hrs · 14,481 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A321 SRM 53-31-15 FIG 101 & 51-42-11.

Part: SLIDE — FAULTY (R4 DOOR) · airframe 39,554 hrs · 14,194 cycles

RED CAUTION LIGHT ON CIDS PANEL FOR R4 DOOR SLIDE. REMOVED AND REPLACED R4 DOOR ESCAPE SLIDE.

Part: MEGAPHONE — WEAK (CABIN) · airframe 37,962 hrs · 13,590 cycles

AFT EMERGENCY MEGAPHONE WEAK. MAINTENANCE REPLACED THE AFT MEGAPHONE.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 151GF BETWEEN FR53 TO FR56, -Z1500 & BETWEEN Y1000 TO -Y1000. REPLACED FLOOR PANEL 151GF IAW A321 AMM 53-42-14-400-001.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 261DF AT FR20, Y510. REPLACED FLOOR PANEL 261DF IAW MCGILL IRM 9701 REV G.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - CORROSION ON STRINGER BETWEEN FR35 TO FR35.8, S41R. SPLICED STRINGER BETWEEN FR35 TO FR35.8, S41R IAW EA 201213.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CORNER FITTING AT FR68, S23L, Y1589. REPLACED CORNER FITTING AT FR68, S23L, Y1589 IAW A321 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69, S23L. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, S23L IAW A321 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24, -Y1497. REPLACED FLOOR PANEL 232FF IAW MCGILL IRM 9701 REV G.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON CORNER FITTING AT FR68, S23R. REPLACED CORNER FITTING AT FR68, S23R IAW A321 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR68, -Y1732. REPLACED SHAPE SILL BETWEEN FR68, -Y1732 IAW A321 SRM 51-72-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 SURFACE CORROSION ON FUSELAGE FRAME AT FR68, S23R. REPAIRED FUSELAGE FRAME AT FR68, S23R IAW A321 SRM SRM 53-41-12.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON L4 DOOR SILL AT FR66, S23L, Y1589. REPAIRED L4 DOOR SILL ANGLE BRACKET AT FR66, S23L, Y1589 IAW EA 201206.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR47.2 TO FR47.5, Y1629. REPLACED FLOORBEAM BETWEEN FR47.2 TO FR47.5, Y1629 IAW A321 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - GALVANIC CORROSION ON SILL PLATE AT FR66, S23R. REPAIRED SILL PLATE AT FR66, S23R IAW EA 201205.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Y1162 IAW A321 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR68, S23R, -Y1162.5. REPLACED FLOORBEAM AT FR68, S23R, -Y1162.5 IAW A321 SRM 51-42-11, 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, S23R, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, S23R, -Y81 IAW A321 SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR65 TO FR68, S23L, Y765. REPLACED FLOOR BEAM BETWEEN FR65 TO FR68, S23L, Y765 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM BETWEEN FR66 TO FR68, S23R, -Y765. REPLACED FLOOR BEAM BETWEEN FR66 TO FR68, S23R, -Y765 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR23, S23L, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR23, S23L, Y254 IAW A321 SRM 51-72-11 & AIRBUS DRAWING B2D53112554.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A321 SRM 51-72-11, 53-11-15 FIGURE 107.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A321 SRM 51-72-11, AND TYPICAL REPAIR 320-2528-10-0011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1162.5. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162.5 IAW A321 SRM 51-75-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, S23R, -Y1292. REPLACED FLOORBEAM AT FR66, S23R, -Y1292 IAW A321 SRM 52-41-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A321 SRM 51-72-11, 53-00-15 FIGURE 104.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y464.8. REPLACED FLOORBEAM AT FR66, -Y464.8 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162.5. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162.5 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM FR20 TO FR20, 23R, -Y189. REPLACED FLOORBEAM FR20 TO FR20, 23R, -Y189 IAW A321 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE PLATE BETWEEN FR69 TO FR70, -Y1162.5. REPLACED SHEAR TIE PLATE BETWEEN FR69 TO FR70, -Y1162.5 IAW A321 SRM 51-72-11 AND TYPICAL REPAIR 320-258-10-0011.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR16, Y503.2. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR16, Y503.2 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM, BETWEEN FR66 TO FR68, S23R, -Y1162. REPLACED FLOOR BEAM, BETWEEN FR66 TO FR68, S23R, -Y1162 IAW A321 SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM BETWEEN FR16 TO FR20, S23R, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, S23R, -Y254 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,534 hrs · 13,441 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16, S23R, -Y1379.5. REPLACED FLOORBEAM AT FR16, S23R, -Y1379.5 IAW A321 SRM 51-42-11, 51-72-11.

Part: BOTTLE — DEFECTIVE (R3 DOOR) · airframe 36,360 hrs · 13,039 cycles

PHL - EES - R3 DOOR ASSIST BOTTLE ACTUATOR REQUIRES REPLACEMENT. MAINTENANCE REMOVED AND REPLACED R3 DOOR ASSIST BOTTLE ACTUATOR IAW AIRBUS MAINTENANCE MANUAL 52-22-14.

Part: ACTUATOR — LOW PRESSURE (R3 DOOR) · airframe 36,266 hrs · 13,008 cycles

LAX - EES - CIDS CAUTION DOOR PRESSURE LOW. MAINTENANCE SERVICED 3R DOOR ASSIST.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 36,251 hrs · 13,003 cycles

PHL - EES - CIDS WARNING ILLUMINATED FOR R3 DOOR. MAINTENANCE SERVICED R3 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,960 hrs · 12,917 cycles

FLT 1471 LAX-PHX - ODOR - DIRTY SOCK SMELL IN COCKPIT AND MID CABIN AT 31,000". CREW REPORTED OF HEADACHES AND DIZZINESS. SMELL WENT WAY ON DESCENT WHEN APU BLEED WAS SELECTED ON. COULD NOT DETECT ANY ODOR IN CABIN WHILE USING APU OR ENGINES AT VARIED POWER. APU AREA CLEAN AND SERVICE CORRECT. COMPLETED CARD 26L00021003 FOUND NO OIL IN SPINNER OR LPC SHAFT, BOROSCOPE OF IGV AREA, CLEAN NO EXTERNAL LEAKAGE IN INLET OR ENGINE AREAS. CHECKED DUCTING BOTH ENGINES AT PRV, FOUND DRY. ALSO COMPLETED CARD 26L00021001, 26L00021004, & 26L00021005.

Part: LENS — MISSING (CABIN) · airframe 35,727 hrs · 12,827 cycles

MX - LAX - EEL - EMERGENCY LIGHT LENS COVER MISSING AT SEAT 22R. MAINTENANCE INSTALLED EMERGENCY LIGHT LENS AT 22R.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 35,397 hrs · 12,710 cycles

FLT 1746 - MCO - EES - CABIN CONTROL PANEL BY THE 1L DOOR IS DISPLAYING RED CIDS CAUTION LIGHTS. MAINTENANCE SERVICED R-3 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-614-002.

Part: ACTUATOR — LOW PRESSURE (R3 DOOR) · airframe 34,821 hrs · 12,498 cycles

FLT 710 - LAX - EES - RED LIGHT ON CIDS CAUTION PANEL FOR R2 AND R3 DOOR PRESSURE LOW. MAINTENANCE SERVICED R3 DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 34,821 hrs · 12,498 cycles

FLT 710 - LAX - EES - RED LIGHT ON CIDS CAUTION PANEL FOR R2 AND R3 DOOR PRESSURE LOW. MAINTENANCE SERVICED R2 DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 33,145 hrs · 11,864 cycles

FLT 1630 - LGA - EMERGENCY EQUIPMENT - AFT MEGAPHONE FOUND INOPERATIVE. REMOVED AND REPLACED AFT MEGAPHONE IAW AIRBUS MAINTENANCE MANUAL 25-65-51.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 33,104 hrs · 11,842 cycles

FLT 1792 - CLT - EES - LOW DOOR PRESSURE ALERT ON CIDS. MAINTENANCE FOUND 3R DOOR OPENING ASSIST BOTTLE PRESSURE LOW. SERVICED BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 32,623 hrs · 11,647 cycles

FLT 1843 BOS - EES - CIDS WARNING MESSAGE R3 BOTTLE PRESSURE LOW. MAINTENANCE REPLACED INFLATION RESERVOIR PER AIRBUS MAINTENANCE MANUAL 25-62-00-810-810.

Part: BLADES — BROKEN (NR 1 ENGINE) · airframe 32,557 hrs · 11,610 cycles

FLT 1511, AIRCRAFT EXPERIENCED NR 1 ENGINE ROLLBACK WITH 9.9 N1 VIBRATION WHILE EN ROUTE. CREW DECLARED AN EMERGENCY AND THE FLIGHT WAS DIVERTED TO BNA. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. VENDOR REPORT IDENTIFIED 3RD STAGE LPT BLADE SET WITH SEVERAL BROKEN BLADES.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 32,418 hrs · 11,554 cycles

PIT - EES - ESCAPE SLIDE NR 3R INFLATION RESERVOIR PRESSURE LOW. MAINTENANCE REPLACED THE NR 3R ESCAPE SLIDE INFLATION RESERVOIR IAW AIRBUS MAINTENANCE MANUAL 25-62-49-04.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 31,714 hrs · 11,269 cycles

FLT 1843 - CLT - EES - CAUTION LIGHT ON CIDS PANEL FOR R-2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-0.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 30,943 hrs · 10,987 cycles

FLT 799 - SEA - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ILLUMINATED ON FLIGHT ATTENDANT PANEL FOR DOOR EXIT R PRESSURE LOW. MAINTENANCE SERVICED DOOR R-3 ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: LENS — MISSING (CABIN) · airframe 30,729 hrs · 10,906 cycles

FLT 1529 - DEN - EEL - 9D SEAT MOUNTED EMERGENCY LIGHT MISSING RED LENS COVER. MAINTENANCE INSTALLED NEW LENS COVER AT 9D PER AIRBUS MAINTENANCE MANUAL 33-51-19.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 30,432 hrs · 10,805 cycles

LOG PAGE 8608513 - WEEKLY CHECK/PHL - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST FAIL. REPLACED 10WL POWER SUPPLY DUE TO UNIT FAULT LAMP ON AND REPLACED R1 DOOR SLIDE DUE TO BAD LIGHTING. EMERGENCY LIGHT OPERATIONAL TEST GOOD.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 30,432 hrs · 10,805 cycles

LOG PAGE 8608513 - WEEKLY CHECK/PHL - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST FAIL. REPLACED 10WL POWER SUPPLY DUE TO UNIT FAULT LAMP ON AND REPLACED R1 DOOR SLIDE DUE TO BAD LIGHTING. EMERGENCY LIGHT OPERATIONAL TEST GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,763 hrs · 9,880 cycles

FLT 939 PHL-CLT EMERGENCY EQUIPMENT. AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MX R&R THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: SAFETY WIRE — BROKEN (EVAC SLIDE) · airframe 27,755 hrs · 9,875 cycles

PIT - C11, SAFETY WIRE BROKEN ON BOTTOM REAR OF PACK. THE SAFETY WIRE HOLDS THE PAWL IN PLACE, HOLDING THE RETAINING PINS OF THE SLIDE. REPLACED SLIDE WITH BROKEN PAWL SAFETY WIRE WITH A NEW SLIDE. INSTALLED BY ROUTINE JOB CARD RT AFT PAX /CREW DOOR LOBE AND OPERATIONAL CHECKS.

Part: ENGINE — MALFUNCTIONED (NR 1)

TPA FLT 1945 EN ROUTE CLT TO RSW. OVER THE VICINITY OF GNV, THE NUMBER ONE ENGINE N1 SPEED DROPPED TO 50 PERCENT. A PASSENGER REPORTED TO HAVE SEEN FIRE AND SMOKE COME FROM THE NUMBER ONE ENGINE. THE FLIGHT DIVERTED TO TPA, AND DURING DESCENT, REGAINED POWER IN THE NUMBER ONE ENGINE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.

Part: SEAL — LEAKING (LT ENGINE)

ABQ FLT 1596 EN ROUTE. WHILE IN CRUISE FLIGHT, THE NR 1 ENGINE BEGAN TO LOOSE OIL PRESSURE. THE CREW SHUTDOWN THE NR 1 ENGINE AND THE FLIGHT DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THERE WAS 20 MINUTES OF SINGLE ENGINE TIME. MAINTENANCE REPLACED THE TRANSFER GEARBOX ADAPTER SEAL. ENGINE OPERATIONALLY AND LEAK CHECKS OK. (K)