N163US

Part: PLATE — LOOSE (ZONE 800) · airframe 77,779 hrs · 30,360 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTREPORTS DISARMING LEVER AT DOOR 2R IS LOOSE. MAINTENANCE TIGHTENED GRIP PLATE HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-22.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 77,134 hrs · 30,095 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 14WL DURING EMERGENCY LIGHTING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 14WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: MECHANISM — OUT OF ADJUST (ZONE 800 ARMING) · airframe 76,894 hrs · 30,005 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR IS DIFFICULT TO ARM. MAINTENANCE LUBRICATED AND ADJUSTED THE ARMING MECHANISM ON THE DOOR PER AMM 52-10-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: RELAY — FAULTED (ZONE 100) · airframe 76,514 hrs · 29,837 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR NOT SHOWING ARMED ON DOOR/OXY PAGE WHEN FLIGHT ATTENDANT REPORTS IT IS ARMED. MAINTENANCE ACCOMPLISHED TSM 52-11-00-810-804-A AND WAS UNABLE TO DUPLICATE THE ISSUE AND REPLACED THE POWER SUPPLY SWITCH OVER RELAY (12WN) PER ASM 52-73-01 DUE TO REPEAT WRITEUPS.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800) · airframe 76,473 hrs · 29,822 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR CLOSED AND DOOR/OXY PAGE SHOWING OPEN. MAINTENANCE ADJUSTED THE PROXIMITY SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-00-820-002-A01.

Part: DOOR — NOISY (ZONE 800) · airframe 76,305 hrs · 29,749 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4L CREAKS LOUDLY WHEN OPENED. MAINTENANCE LUBRICATED THE L4 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-00-00.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800) · airframe 75,668 hrs · 29,475 cycles

AIRCRAFT IN BASE MAINTENANCE: 1R DOOR SLIDE ARM RIGGING CHECK ARMING INTERMITTENT. MAINTENANCE ACCOMPLISHED PERFORMED RIGGING CHECK OF THE SLIDE ARMING PROXIMITY SWITCH 4WN2 PER AMM 52-70-00-040-007-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER OF THE EMERGENCY ESCAPE SLIDE RELEASE-SYSTEM OF THE PASSENGER CREW DOOR PER AMM 52-71-00-820-002-A01 WITH NO ISSUES NOTED.

Part: SPEAKER — INOPERATIVE (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: NO EVACUATION ALARM AT DOOR 3. MAINTENANCE ACCOMPLISHED AN OPERATIONAL TEST OF THE LOUD SPEAKER SYSTEM PER AMM 23-73-51 AND THE SPEAKER AT DOOR 3L FAILED THE TEST. MAINTENANCE REPLACED THE SPEAKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER AMM 23-73-00-710-026-A WITH NO ISSUES NOTED.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 11. REPAIRED SKIN PANEL PER EA 361177.

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 361177

Part: COVER PLATE — CORRODED (ZONE 100) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATG ANTENNA/COVER PLATE BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPLACED COVER PLATE PER SRM 51-72-11.

Part: FITTING — WORN (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD AVIONIC COMPARTMENT RACK 80VU RIGHT HAND SUPPORT STRUT / FITTING WORN BETWEEN FR 23 AND FR 24 AT S38R. REPLACED SUPPORT / FITTING PER EA 361415.

Part: FITTING — WORN (ZONE 100) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD AVIONIC COMPARTMENT RACK 80VU LEFT HAND SUPPORT STRUT / FITTING WORN BETWEEN FR 23 AND FR 24 AT S38L. REPLACED SUPPORT / FITTING PER EA 361415.

Part: FITTING — NONE (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 360681. REPLACED RIGHT HAND CONTINUITY FITTING PER EA 360681.

Part: FITTING — NONE (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 360681. REPLACED LEFT HAND CONTINUITY FITTING PER EA 360681.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND WINDSHIELD CENTER POST AREA AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 360681.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: WINDOW FRAME — NONE (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND WINDSHIELD FRAME CENTER POST AREA AT FR 2 AND Y0 NEEDS TO BE MODIFIED (MIRROR FITTING / POCKET MACHINING) PER EA 360681. MODIFIED THE RIGHT HAND WINDSHIELD FRAME CENTER POST AREA PER EA 60681.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: SPIGOT — CORRODED (ZONE 400) · corrosion level 2 · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING BETWEEN PYLON RIB 7 AND 8. REPLACED SPIGOT FITTING PER SRM 54-51-12.

Part: CONNECTOR — CRACKED (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR CROSS BEAM SECTION CONNECTION AT FR 66 BETWEEN S23R AND S24R. REPLACED BEAM CROSS BEAM SECTION CONNECTION PER SRM 51-42-11.

Part: CONTROL CABLE — DEFORMED (ZONE 800) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 FLEXIBLE CONTROL CABLE HOSE HAS DEFORMATION. REPLACED FLEXIBLE CONTROL CABLE PER AMM 52-11-22.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON HINGE ARM END FITTING BEARING # 4 ON LEFT-HAND HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #4 PER AMM 55-16-42-000-001-A.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED ON FRAME 68 IN THE PASSENGER CABIN. PERFORMED REPAIR ON LOWER SILL PER SRM 53-41-14-300-001.

Part: CROSSBEAM — CRACKED (ZONE 100) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK CROSS BEAM CONNECTION LOCATED AT FR 68 BETWEEN STR 22L TO STR 23L AT AFT GALLEY AREA, REPLACED CROSSBEAM SECTION CONNECTION PER SRM 51-72-11-911-001.

Part: CROSSBEAM — CRACKED (ZONE 100 - FUSE) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON CROSSBEAM SECTION CONNECTION LOCATED AT FR 66 BETWEEN STR 22L AND 23L IN AFT GALLEY AREA. REPLACED CROSSBEAM SECTION CONNECTION PER SRM 51-42-11-801.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #5 SLAT TRACK BOLT. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #6 SLAT TRACK BOLT. REPLACED BOLT PER TASK CARD 26C61057005.

Part: STRIKER — OUT OF ADJUST (ZONE 800 ASSIST) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER DIMENSION "A" BETWEEN THE FINGER AND STRIKER LEVER NEEDS TO BE ADJUSTED. MAINTENANCE ADJUSTED DIMENSION "A" BETWEEN THE FINGER AND STRIKER LEVER PER AMM 52-13-14-820-002-A.

Part: HANDLE — CRACKED (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER AMM 56-12-11 AND CMM 56-12-11.

Part: HANDLE — CRACKED (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER AMM 56-12-11 AND CMM 56-12-11.

Part: STOP FITTING — WORN (ZONE 800) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 833 HAS 3 WORN DOOR STOP SCREWS ON THE AFT SIDE. REPLACED DOOR STOPS SCREW PER AMM 52-32-31.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

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

Part: FITTING — CRACKED (ZONE 200) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 LEFT AND DOOR STOP FITTING #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING BEARING 1 ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING 1 ON LH HORIZONTAL STABILIZER.

Part: HINGE ARM — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON HINGE ARM END FITTING BEARING #5 ON LEFT-HAND HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING PER AMM 55-16-42-000-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING BEARING 2 ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING 2 ON LH HORIZONTAL STABILIZER.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING BEARING 3 ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING 3 ON LH HORIZONTAL STABILIZER.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING BEARING 6 ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING 6 ON LH HORIZONTAL STABILIZER.

Part: WINDOW — SCRATCHED (ZONE 800) · airframe 75,667 hrs · 29,474 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIR 833 WINDOW INNER AND OUTER PANES SCRATCHED. REPLACED WINDOW ASSEMBLY PER AMM 56-31-15.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 74,408 hrs · 28,939 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND ROWS 14 AND 15 EMERGENCY ISLE LIGHTS INOPERATIVE. FOUND WIRE TO EMERGENCY LIGHTS AT ROWS 14 AND 15 WITH A WIRE BROKEN. PERFORMED WIRE REPAIR OF EMERGENCY LIGHTS PER ESPM 20-43-11.

Part: HANDLE — OBSTRUCTED (L3 ARMING LEVER) · airframe 73,867 hrs · 28,703 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR SLIDE WILL NOT ARM. REMOVED INSULATION FROM SLIDE ARM HANDLE LUBED L3 DOOR HANDLE OPERATES NORMAL PER AMM 52-22-00-720.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 73,832 hrs · 28,690 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND FLOOR PANEL 151GF IN AFT CARGO TO BE DELAMINATED AND SQUISHY. REMOVED AND REPLACED AFT CARGO PANEL 151GF REF AMM 53-42-14.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 72,899 hrs · 28,273 cycles

AIRCRAFT WAS GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN IN FLIGHT OR CLOSE IN FLIGHT. LUBED DOOR AS REQUIRED.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 72,753 hrs · 28,209 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED LAVATORY DOOR LATCH.

Part: FITTING — BINDING (ZONE 800 - DOORS) · airframe 72,658 hrs · 28,162 cycles

AIRCRAFT WAS GROUNED: GATE AGENT WAS UNABLE TO OPEN FORWARD ENTRY DOOR FROM THE OUTSIDE DUE TO BINDING OF THE DOOR FRAME. ADJUSTED LOWER FORWARD ROLLER BEARING FITTING PER AMM 52-11-00.

Part: DOOR — INOPERATIVE (ZONE 900 - LAV/G) · airframe 72,652 hrs · 28,159 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR WILL NOT OPEN OR CLOSE CORRECTLY. **SUPPLEMENTAL REPORT FOR AALA202401029776: MAINTENANCE REPLACED THE MID LAVATORY DOOR PER AARD 25-40-00-16** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,652 hrs · 28,159 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR WILL NOT OPEN OR CLOSE CORRECTLY. (OPEN)

Part: BELLOWS — SEPARATED (ZONE 100 - FUSE) · airframe 71,545 hrs · 27,672 cycles

AIRCRAFT WAS GROUNDED: APPROXIMATELY 2 HOURS INTO FLIGHT A BURNING RUBBER / ELECTRICAL ODOR WAS SMELLED THROUGHOUT THE ENTIRE AIRCRAFT FOR APPROXIMATELY 5 MINUTES THEN THE ODOR DISSIPATED. MAINTENANCE FOUND THE LEFT PACK BELLOWS BETWEEN THE CONDENSOR (10HM2) AND CHECK VALVE (15MH) WAS SEPERATING FROM THE FLANGE. MAINTENANCE REPLACED THE BELLOWS AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: PROXIMITY SWITCH — DIRTY (ZONE 800 - DOORS) · airframe 71,506 hrs · 27,654 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN DOOR ECAM MESSAGE STILL SHOWN WITH DOOR CLOSED AND LOCKED. MAINTENANCE CLEANED DOOR LOCKING HOOK PROXIMITY SWITCH PER AMM 52-71-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900 - LAV/G) · airframe 71,114 hrs · 27,465 cycles

AIRCRAFT WAS NOT GROUNDED: L4 SMOKE ALARM ENROUTE. NO SMOKE DETECTED. FLIGHT CREW TURNED OFF WATER HEATER AND CLOSED AFT LAVATORY PER MOC INSTRUCTIONS. MAITENANCE ACCOMPLISHED TSM 26-17-00-810-801-A AND FOUND NO FAULTS WITH THE SMOKE DETECTION SYSTEM AND RESET THE LAVATORY WATER HEATER.

Part: CONTROLLER — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,854 hrs · 27,335 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT. WITH PACK 2 INOPERATIVE AND ON MEL ,#1 PACK TEMPERATURE DISPLAYED AMBER XX AND CREW WAS UNABLE TO MONITOR PACK. THE AIRCRAFT LANDED SAFELY AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE #1 PACK CONTROLLER PER AMM 21-61-34.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 70,699 hrs · 27,265 cycles

AIRCRAFT WAS NOT GROUNDED: 1ST CLASS LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE LAVATORY DOOR PER AMM 52-51-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HINGE — STICKING (ZONE 900 - LAV/G) · airframe 70,456 hrs · 27,144 cycles

AIRCRAFT WAS NOT GROUNDED: 1ST CLASS LAVATORY DOOR IS STICKY, HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED DOOR HINGE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 69,758 hrs · 26,833 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 12WL BATTERY FAULT. MAINTENANCE REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (LAVATORY) · airframe 69,469 hrs · 26,703 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. THE DOOR APPEARS TO BE STICKING AT THE BOTTOM LEFT-HAND SIDE OF THE DOOR. MAINTENANCE CLEANED BOTTOM OF DOOR AND DOOR SILL. ALSO ADJUSTED THE DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,384 hrs · 26,669 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS NOT WORKING AT SEAT NO. 14,15,17,18,21,22,28,29,32,33 AND 34. ALSO CENTER CEILING EMERGENCY LIGHTS INOPERATIVE NEAR SEAT NO.15 AND 25. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202211299513) AND BATTERY (AALA202211294342) PER AMM 33-51-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,384 hrs · 26,669 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS NOT WORKING AT SEAT NO. 14,15,17,18,21,22,28,29,32,33 AND 34. ALSO CENTER CEILING EMERGENCY LIGHTS INOPERATIVE NEAR SEAT NO.15 AND 25. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL (AALA202211299513) AND BATTERY (AALA202211294342) PER AMM 33-51-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR — STICKING (ZONE 900 - LAV/G) · airframe 69,187 hrs · 26,584 cycles

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

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 69,149 hrs · 26,571 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLIGHT FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. ADJUSTED LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-50-00.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 68,864 hrs · 26,432 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-21.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 68,461 hrs · 26,246 cycles

AIRCRAFT WAS NOT GROUNDED: AFT GALLEY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT PER AMM 25-65-00.

Part: BULB — OUT OF POSITION (ZONE 200 - FUSE) · airframe 68,229 hrs · 26,140 cycles

AIRCRAFT WAS NOT GROUNDED: INBOARD FLASHLIGHT NEXT TO DOOR 4R IS INOPERATIVE. RE-POSITIONED LIGHT BULB AS REQUIRED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DETACHED (ZONE 200 - FUSE) · airframe 67,936 hrs · 26,010 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK ESCAPE ROPE COVER ON CAPTAINS SIDE FELL OFF. RE-INSTALLED COVER PER AMM 25-61-00.

Part: HINGE — WORN (ZONE 300 - STABS) · airframe 67,820 hrs · 25,963 cycles

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

Part: HINGE — WORN (ZONE 300 - STABS) · airframe 67,820 hrs · 25,963 cycles

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

Part: HINGE — WORN (ZONE 300 - STABS) · airframe 67,820 hrs · 25,963 cycles

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

Part: SLIDE — DEFORMED (ZONE 800 - DOORS) · airframe 67,820 hrs · 25,963 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 SLIDE DEFORMED. REPLACED SLIDE PER TASK CARD 26C83152002.

Part: FRAME — CRACKED (ZONE 100 - FUSE) · airframe 67,820 hrs · 25,963 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FOOT COUPLING AT FR 43 BETWEEN S18L AND S24L. REPLACED FRAME SECTION PER EA 336307, EO 5320Y003-001 AND DRAWING R53370232 REV D.

Part: PRESSURE SWITCH — FAULTY (ZONE 300 - STABS) · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: APU AUTO SHUTDOWN 23 MINUTES AFTER TAKEOFF. APU SHUTDOWN AGAIN AFTER RESTART. RETURNED TO DFW, LANDING SAFELY. REPLACED APU LOW OIL PRESSURE SWITCH (AALA202205110105) PER AMM 49-94-14. OPERATIONAL AND LEAK CHECKS GOOD. REPLACED #2 EGT THERMOCOUPLE PROBE (AALA202205127356) PER AMM 49-72-15. OPERATIONAL CHECK GOOD.

Part: WIRE — FAULTY (ZONE 400 - NAC/P) · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: ENROUTE, ENGINE #2 BLEED LOW PRESSURE FOLLOWED BY ENGINE #2 IDG TEMPERATURE ECAM ADVISORY FLASHING. EMERGENCY DECLARED; FLIGHT LANDED SAFELY AT DFW. (SEE AALA202205119559 FOR #2 IDG REPLACEMENT). **SUPPLEMENTAL REPORT FOR AALA202205129588: REPLACED ENGINE #2 OVER PRESSURE VALVE WIRE 3611-0372 FROM CONNECTOR 5HA2-A PIN 1 TO CONNECTOR 451VC2-A PIN 1 ( AALA202205129588) PER ESPM 20-53-21 AND AWM 36-11-04. ACCOMPLISHED SATISFACTORY ENGINE AUTOMATIC START PER AMM 71-00-00-710-003-B. ECAM AIR ENG 2 BLEED ABNORMAL PRESSURE MESSAGE IS NO LONGER SHOWED. REPLACED ENGINE #2 OVER PRESSURE VALVE (AALA202205275305) PER AMM 36-11-53-400-001-A. ACCOMPLISHED SATISFACTORY BITE TEST BMC2 PER AMM 36-11-00-740-001-A. ACCOMPLISHED SATISFACTORY OVER PRESSURE VALVE LEAK CHECK.** (CLOSED).

Part: NONE — NONE · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: ENROUTE, ENGINE #2 BLEED LOW PRESSURE FOLLOWED BY ENGINE #2 IDG TEMPERATURE ECAM ADVISORY FLASHING. EMERGENCY DECLARED; FLIGHT LANDED SAFELY AT DFW. (SEE AALA202205119559 FOR #2 IDG REPLACEMENT). **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: THERMOCOUPLE — FAULTY (ZONE 300 - STABS) · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: APU AUTO SHUTDOWN 23 MINUTES AFTER TAKEOFF. APU SHUTDOWN AGAIN AFTER RESTART. RETURNED TO DFW, LANDING SAFELY. REPLACED APU LOW OIL PRESSURE SWITCH (AALA202205110105) PER AMM 49-94-14. OPERATIONAL AND LEAK CHECKS GOOD. REPLACED #2 EGT THERMOCOUPLE PROBE (AALA202205127356) PER AMM 49-72-15. OPERATIONAL CHECK GOOD.

Part: IDG — FAULT MESSAGE (ZONE 400 - NAC/P) · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: ENROUTE, ENGINE #2 BLEED LOW PRESSURE FOLLOWED BY ENGINE #2 IDG TEMPERATURE ECAM ADVISORY FLASHING. EMERGENCY DECLARED; FLIGHT LANDED SAFELY AT DFW. #2 IDG REPLACED PER AMM 24-21-51. OPERATIONAL AND LEAK CHECKS GOOD PER AMM 24-21-51. (SEE AALA202205129588 FOR ENGINE #2 BLEED LOW PRESSURE)

Part: NONE — NONE (ZONE 400 - NAC/P) · airframe 67,817 hrs · 25,962 cycles

AIRCRAFT WAS GROUNDED: ENROUTE, ENGINE #2 BLEED LOW PRESSURE FOLLOWED BY ENGINE #2 IDG TEMPERATURE ECAM ADVISORY FLASHING. EMERGENCY DECLARED; FLIGHT LANDED SAFELY AT DFW. (SEE AALA202205119559 FOR #2 IDG REPLACEMENT). **SUPPLEMENTAL REPORT FOR AALA202205129588: REPLACED ENGINE #2 OVER PRESSURE VALVE WIRE 3611-0372 FROM CONNECTOR 5HA2-A PIN 1 TO CONNECTOR 451VC2-A PIN 1 (AALA202205129588) PER ESPM 20-53-21 AND AWM 36-11-04. ACCOMPLISHED SATISFACTORY ENGINE AUTOMATIC START PER AMM 71-00-00-710-003-B. ECAM AIR ENG 2 BLEED ABNORMAL PRESSURE MESSAGE IS NO LONGER SHOWED. REPLACED ENGINE #2 OVER PRESSURE VALVE (AALA202205275305) PER AMM 36-11-53-400-001-A. ACCOMPLISHED SATISFACTORY BITE TEST BMC2 PER AMM 36-11-00-740-001-A. ACCOMPLISHED SATISFACTORY OVER PRESSURE VALVE LEAK CHECK.** (CLOSED).

Part: FITTING — STICKING (ZONE 800 - DOORS) · airframe 67,299 hrs · 25,728 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS 4L DOOR DIFFICULT TO ARM. CLEANED AND LUBRICATED GIRT BAR FLOOR FITTINGS PER AMM 52-13-12.

Part: MEGAPHONE — INOPERATIVE (ZONE 200 - FUSE) · airframe 66,805 hrs · 25,506 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD CABIN MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-51.

Part: LATCH — DIRTY (ZONE 900 - LAV/G) · airframe 66,587 hrs · 25,406 cycles

AIRCRAFT WAS NOT GROUNDED: 3L LAVATORY DOOR HARD TO OPEN. CLEANED LATCH MECHANISM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — OUT OF POSITION (ZONE 200 - FUSE) · airframe 66,519 hrs · 25,380 cycles

AIRCRAFT WAS NOT GROUNDED: ON CABIN WALK THROUGH FOUND 19C EMERGENCY LIGHT ON THE FLOOR. RE-ATTACHED SEAT 19C EMERGENCY LIGHT PER ESO 25-21-61.

Part: WIRE HARNESS — DAMAGED (ZONE 600 - RH WI) · airframe 66,411 hrs · 25,332 cycles

AIRCRAFT WAS GROUNDED: FUEL CENTER RIGHT HAND TRANSFER FAULT ANNUNCIATED ON ECAM. COMPLIED WITH ECAM PROCEDURE AND SUCCESSFULLY TRANSFERRED CENTER FUEL. FLIGHT DIVERTED TO DFW LANDING SAFELY. MAINTENANCE REPLACED FUEL COMPENSATOR-ULTRA 52QT (AALA202111176375) PER AMM 28-42-48-401. ACCOMPLISHED REPAIR OF TERMINAL LUG ON WIRE HARNESS TO COMPENSATOR 52QT PER EA.NO 332031 (AALA202111174012).

Part: COMPENSATOR — FAULTY (ZONE 600 - RH WI) · airframe 66,411 hrs · 25,332 cycles

AIRCRAFT WAS GROUNDED: FUEL CENTER RIGHT HAND TRANSFER FAULT ANNUNCIATED ON ECAM. COMPLIED WITH ECAM PROCEDURE AND SUCCESSFULLY TRANSFERRED CENTER FUEL. FLIGHT DIVERTED TO DFW LANDING SAFELY. MAINTENANCE REPLACED FUEL COMPENSATOR-ULTRA 52QT (AALA202111176375) PER AMM 28-42-48-401. ACCOMPLISHED REPAIR OF TERMINAL LUG ON WIRE HARNESS TO COMPENSATOR 52QT PER EA.NO 332031 (AALA202111174012).

Part: TRACK — LACK OF LUBE (ZONE 800 - DOORS) · airframe 66,265 hrs · 25,269 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR HARD TO OPEN. CLEANED AND LUBRICATED L1 DOOR TRACK PER AMM 52-11-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: ACTUATOR — DEFECTIVE (ZONE 100 - FUSE) · airframe 66,261 hrs · 25,266 cycles

AIRCRAFT WAS GROUNDED: AROUND 10,000 ' ECAM FUEL: LEFT WING TANK OVERFLOW SHUT OFF LEFT CENTER TANK TRANSFER PER ECAM FUEL CONTINUED TO FLOW FROM CENTER TO LEFT TANK EVEN WITH VALVE CLOSED KEEPING LEFT TANK IN OVERFLOW CONDITION.. REPLACED FUEL VALVE ACTUATOR AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK

Part: VALVE — DEFECTIVE (ZONE 500 - LH WI) · airframe 66,249 hrs · 25,260 cycles

AIRCRAFT WAS GROUNDED: LEFT WING FUEL TANK OVERFLOW ECAM MESSAGE, AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CLACK VALVE 214QM (AND) CLACK VALVE 216QM (AALA202110219658) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: VALVE — DEFECTIVE (ZONE 500 - LH WI) · airframe 66,249 hrs · 25,260 cycles

AIRCRAFT WAS GROUNDED: LEFT WING FUEL TANK OVERFLOW ECAM MESSAGE, AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CLACK VALVE 214QM (AND) CLACK VALVE 216QM (AALA202110219658) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 66,233 hrs · 25,253 cycles

AIRCRAFT WAS NOT GROUNDED: L3 ESCAPE SLIDE LIGHTING INOPERATIVE. ** SUPPLEMENTAL REPORT FOR AALA202110194646: ACCOMPLISHED TSM 33-51-00 AND FOUND EMERGENCY POWER SUPPLY UNIT 11WL AT FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38. WILL BE SUBMITTED** (CLOSED)

Part: NONE — NONE · airframe 66,233 hrs · 25,253 cycles

AIRCRAFT WAS NOT GROUNDED: L3 ESCAPE SLIDE LIGHTING INOPERATIVE. ** SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LIGHT — DAMAGED (ZONE 200 - FUSE) · airframe 66,021 hrs · 25,171 cycles

AIRCRAFT WAS NOT GROUNDED: ASILE EMERGENCY LIGHT AT SEAT 15C DAMAGED. RESECURED LIGHT PER AMM 33-51-00.

Part: UNKNOWN — ODOR (A/C PACK SYSTEM) · airframe 66,022 hrs · 25,171 cycles

AIRCRAFT WAS GROUNDED: AIR CONDITIONING SYSTEM HAS A FOUL AND PUNGENT ODOR AT LOWER ALTITUDES WITH MODERATE TEMPERATURE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: ECS — ODOR · airframe 66,022 hrs · 25,171 cycles

AIRCRAFT WAS GROUNDED: AIR CONDITIONING SYSTEM HAS A FOUL AND PUNGENT ODOR AT LOWER ALTITUDES WITH MODERATE TEMPERATURE. ACCOMPLISHED WORKCARDS 26L00021002 AND 26L00021004, NO ODOR PRESENT.

Part: IDG — FAILED (NR 1) · airframe 65,889 hrs · 25,122 cycles

AIRCRAFT WAS GROUNDED: WITH #1 ENGINE IDG ON MEL THE #2 ENGINE FAILED IN FLIGHT, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PHX ON APU ELECTRICAL POWER WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #2 ENGINE IDG AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 24-21-51.

Part: LIGHT — BROKEN (SEAT ROW9 ABC) · airframe 65,855 hrs · 25,109 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AT SEAT 9,12 ABC ARE BROKEN. REPLACED EMERGENCY LIGHTS AT SEAT 9,12 ABC PER 33-502-00.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 63,211 hrs · 23,962 cycles

AIRCRAFT WAS NOT GROUNDED: OVERHEAD WHITE EMERGENCY LIGHT AT ROW 9 INOPERATIVE.. CONNECTED WIRE THAT WAS DISCONNECTED FROM OVERHEAD EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECKED GOOD PER AMM 33-51-00-710.

Part: STRUT — MISINSTALLED (TE FLAPS) · airframe 62,903 hrs · 23,843 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CONTROL FLAPS LOCKED - ALIGNMENT FAULT OCCURRED ON TAKEOFF AT APPROXIMATELY 30 KNOTS AND THE CREW ABORTED THE TAKEOFF. FOUND THE LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT INCORRECTLY INSTALLED AND INSTALLED IT CORRECTLY PER AMM 27-51-44. (AALA202007109013) IN ADDITION REPLACED THE INSTRUMENTATION POSITION PICK-OFF UNIT (IPPU 3CN) PER AMM 2755-11.(AALA202007109015) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POSITION UNIT — FAULTED (TE FLAPS) · airframe 62,903 hrs · 23,843 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CONTROL FLAPS LOCKED - ALIGNMENT FAULT OCCURRED ON TAKEOFF AT APPROXIMATELY 30 KNOTS AND THE CREW ABORTED THE TAKEOFF. FOUND THE LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT INCORRECTLY INSTALLED AND INSTALLED IT CORRECTLY PER AMM 27-51-44. (AALA202007109013) IN ADDITION REPLACED THE INSTRUMENTATION POSITION PICK-OFF UNIT (IPPU 3CN) PER AMM 2755-11.(AALA202007109015) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SPLICE PLATE — CRACKED (FRAMES 62-63) · airframe 62,901 hrs · 23,842 cycles

AIRCRAFT IN BASE VISIT: L/H OUTBOARD SEAT TRACK FWD O/B LOWER SPLICE FOUND TO HAVE AN EXISTING CRACK. REPLACED SPLICE IAW EO 2518E208-017 AND DRAWING D53492806016.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,900 hrs · 23,842 cycles

AIRCRAFT IN BASE VISIT: CABIN FLOOR PANEL 222EF HAS SURFACE DELAMINATION. REMOVED AND REPLACED FLOOR PANEL 222EF, IAW AMM 53-00-00-400-801-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 61,912 hrs · 23,460 cycles

AIRCRAFT WAS NOT GROUNDED: AFT CABIN EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,904 hrs · 23,457 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT DOOR 2R WAS NOT CHARGING. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD PRACTICES.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR ASSIST) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY ACCUMULATOR REQUIRED SERVICE. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS EMERGENCY POWER SUPPLY (13WL) FAILED TEST. REMOVED & REPLACED EPSU (13WL) IAW AMM 33-51-38. OPS/ BITE TEST NORMAL.

Part: ACCUMULATOR — LOW PRESSURE (L4 DOOR ASSIST) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR EMERGENCY ACCUMULATOR REQUIRED SERVICE. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (R4 DOOR ASSIST) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY ACCUMULATOR REQUIRED SERVICE. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR ASSIST) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY ACCUMULATOR REQUIRED SERVICE. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 61,622 hrs · 23,355 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR EMERGENCY EXIT DAMPER REQUIRED SERVICE. MAINTENANCE SERVICED DOOR DAMPER TO PROPER PRESSURE PER AMM 52-22-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 61,532 hrs · 23,322 cycles

AIRCRAFT WAS NOT GROUNDED: DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS PER JOB CARD 26L00005005, R4 AND L4 LOWER INTERIOR EMERGENCY LIGHTS WOULD NOT COME ON. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,525 hrs · 23,319 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS DURING COMPLIANCE OF OPS CHECK EPSU, FOUND L3 UNIT FAULT. REMOVED AND REPLACED L3 EPSU UNIT AND EMERGENCY BATTERY IAW AMM 33-51-38. OPS CHECK OK.

Part: PULLEY — OUT OF TOLERANCE (RUDDER SYS) · airframe 60,953 hrs · 23,077 cycles

AIRCRAFT IN BASE VISIT: PILOT REPORTS CLIMBING THROUGH 11, 000 FT BETWEEN 250-280 KNTS. BOTH SET OF RUDDER PEDALS HAD A HARD FAST VIBRATION (FELT LIKE A RVIET GUN) THERE WAS NO AIRFRAME VIBRATION ASSOCIATED WITH IT. LASTED APPROX 2 MIN. MAINTENANCE REPORTS ACCOMPLISHED ALL STEPS OF EA 297571. (SEE SDR # AALA201908129020)

Part: UNKNOWN — VIBRATION · airframe 60,916 hrs · 23,063 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS APPROX. 1500 FT AGL, A/C FULLY CONFIGURED FLAPS FULL 143 KNOTS, MEDIUM TO SEVERE VIBRATION IN RUDDER PEDALS. ON LDG FELT LIKE RUDDER MADE UNCOMMANDED MOVEMENT. NO FAULTS NOTED. PERFORMED RUDDER CONTROL ADJUSTMENTS AND TESTS IAW AMM 27-21-00, NO FAULTS FOUND. TESTED ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING-ACTIVATION IAW AMM 27-23-00, NO HISTORY. ALL CHECKS OK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 60,818 hrs · 23,028 cycles

AIRCRAFT WAS NOT GROUNDED: DURING COMPLIANCE OF JOBCARD 26C00033004, FOUND EMERGENCY POWER SUPPLY UNIT AT L3 DOOR FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,746 hrs · 22,996 cycles

AIRCRAFT WAS NOT GROUNDED: 3L FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT PER MM 33-50-00.

Part: REGULATOR — OUT OF TOLERANCE (RUDDER) · airframe 60,634 hrs · 22,949 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT 40 FEET DURING LANDING, RUDDER PEDALS HAD FLUTTER UNTIL MAIN GEAR TOUCH DOWN. FLAPS 3, AP OFF, GW 105,000, NO AIRFRAME VIBRATIONS NOTED. MAINTENANCE REMOVED AND REPLACED THE RUDDER TRIM ACTUATOR IAW AMM. MAINTENANCE ALSO REMOVED AND REPLACED THE CABLE TENSION REGULATOR ASSEMBLY AND RUDDER CONTROL CENTERING ROD. RIG CHECKED GOOD IAW AMM 27-21-15. (SEE SDR # AALA201906209001)

Part: ACTUATOR — OUT OF TOLERANCE (TE FLAPS) · airframe 60,634 hrs · 22,949 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AT 40 FEET DURING LANDING, RUDDER PEDALS HAD FLUTTER UNTIL MAIN GEAR TOUCH DOWN. FLAPS 3, AP OFF, GW 105,000, NO AIRFRAME VIBRATIONS NOTED. MAINTENANCE REMOVED AND REPLACED THE RUDDER TRIM ACTUATOR IAW AMM. MAINTENANCE ALSO REMOVED AND REPLACED THE CABLE TENSION REGULATOR ASSEMBLY AND RUDDER CONTROL CENTERING ROD. RIG CHECKED GOOD IAW AMM 27-21-15

Part: FEEL UNIT — FAULTED (RUDDER SYSTEM) · airframe 60,617 hrs · 22,943 cycles

AIRCRAFT WAS GROUNDED: STRONG VIBRATION IN RUDDER PEDALS 2000' AGL BEFORE GEAR EXTENSION TO 500' AGL GEAR DOWN VIBRATION CONTINUED 20 SECONDS AFTER AUTOPILOT OFF. PEDALS LEFT AND RIGHT BOTH SIDES CAPT & FO MOVING 3/8" DISPLACEMENT. PUSHING ON BOTH PEDALS WOULD NOT STOP PEDALS FROM JUMPING AROUND, WENT AWAY AT 500' AGL. MAINTENANCE REPLACED THE ARTIFICIAL FEEL AND TRIM UNIT IAW AMM 27-23-41-4 00-001-A AND PERFORMED OPERATIONAL TEST OF THE ARTIFICAL FEEL AND TRIM UNIT IAW AMM 27-23-00-710-001-A AND 27-23-00-710-001-A-01 AND PERFORMED OPERATIONAL TEST OF THE RUDDER TRIM ACTUATION IAW AMM 27-22-00-710-002-A AND TESTS ARE OK.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RUDDER HINGE FITTING NR 3 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RUDDER HINGE FITTING NR 7 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RUDDER HINGE FITTING NR 5 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RUDDER HINGE FITTING NR 4 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING NR 2 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING NR 3 WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #1 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #4 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND ELEVATOR #5 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND ELEVATOR #4 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #5 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #3 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND ELEVATOR #6 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #6 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 60,486 hrs · 22,885 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #2 HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 60,243 hrs · 22,784 cycles

MAINTENANCE FOUND THE L1 DOOR EMERGENCY ASSIST ACTUATOR BOTTLE WITH PRESSURE LOW. SERVICED THE CYLINDER IAW AMM 52-10-00. NO LEAKS NOTED.

Part: ATTACH FITTING — WORN (THRUST REVERSER) · airframe 60,149 hrs · 22,744 cycles

RIGHT INBD THRUST REVERSER AFT ATTACH FITTING ON PYLON IS WORN ALLOWING THE BEARING TO MIGRATE. REPLACED THE ATTACH FITTING IAW AMM 54-57-17-400-003.

Part: ATTACH FITTING — WORN (THRUST REVERSER) · airframe 60,149 hrs · 22,744 cycles

RIGHT INBD THRUST REVERSER CENTER ATTACH FITTING ON PYLON IS WORN ALLOWING THE BEARING TO MIGRATE. REPLACED THE ATTACH FITTING IAW AMM 54-57-17-400-003.

Part: BEARING — MIGRATED (THRUST REVERSER) · airframe 60,149 hrs · 22,744 cycles

RIGH PYLON OTBD THRUST REVERSER AFT HINGE FITTING AT RIB 2 FOUND WORN DUE TO BEARING MIGRATION. REPLACED THE HINGE FITTING IAW AMM 54-57-17-400-003-A.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 60,149 hrs · 22,744 cycles

AFT GALLEY FLOOR PANEL 261AG DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-001, AND IRM 9701, REV I.

Part: FITTING — CRACKED (LT FLAP TRACK) · airframe 60,149 hrs · 22,744 cycles

LEFT WING FLAP TRACK AFT FITTING WAS CRACKED. REPLACED THE FLAP TRACK FITTING IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 60,149 hrs · 22,744 cycles

FORWARD GALLEY FLOOR PANEL 231FF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701, REV I.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 60,149 hrs · 22,744 cycles

FORWARD GALLEY FLOOR PANEL 221DF WAS DELAMINATED. REPLACED THE FLOOR PANEL PER SRM 53-12-00-300-006, AND IRM 9701, REV I.

Part: HINGE ARM — WORN (LT ELEVATOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 60,149 hrs · 22,744 cycles

FORWARD GALLEY FLOOR PANEL 232DF WAS DELAMINATED. REPAIRED THE FLOOR PANEL IAW SRM 53-02-00-300-013, PARA 2B.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK NR 2 MID, AFT BOLT. REPLACED THE BOLT IAW AMM 27-84-63-400-002-A.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION ON THE RIGHT WING LEADING EDGE SLAT TRACK NR 6 UPPER AFT BOLT. REPLACED THE BOLT IAW AMM 27-84-63-400-002-A.

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION FOUND ON THE LOWER SILL, FRAME 66, STRINGER 23L. REPAIRED THE SILL IAW SRM 53-41-14-300-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION FOUND ON AFT GALLEY FLOOR SUPPORT BETWEEN FRAMES 64 AND 66 AT +Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION FOUND ON THE AFT GALLEY SHEAR PLATE, BETWEEEN FRAMES 69 AND 70, STRINGER 23L. REPLACED THE SHEAR PLATE IAW SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 60,149 hrs · 22,744 cycles

CRACKED AFT GALLEY SHEAR PLATE BETWEEN FRAMES 69 AND 70 AT STRINGER 23R. REPLACED SHEAR PLATE IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 60,149 hrs · 22,744 cycles

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

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 12 AND 24, +Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 60,149 hrs · 22,744 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAME 12 AND 24, -Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 60,149 hrs · 22,744 cycles

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

Part: COUPLING — DAMAGED (SEAT TRACK) · airframe 60,149 hrs · 22,744 cycles

SEAT TRACK COUPLING AT FRAME 24, +Y1292, HAD AN ELONGATED HOLE. REPLACED THE COUPLING IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 60,149 hrs · 22,744 cycles

FORWARD GALLEY FLOOR PANEL 222EF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FITTING — CRACKED (FRAME 16) · airframe 60,149 hrs · 22,744 cycles

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

Part: FITTING — CRACKED (FRAME 16) · airframe 60,149 hrs · 22,744 cycles

CRACKED DOOR CUTOUT INTERCOSTAL FITTING AT FRAME 16, RIGHT AT THE NR 7 DOOR STOP. REPLACED INTERCOSTAL FITTING IAW SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 60,149 hrs · 22,744 cycles

CRACKED INTERCOSTAL AT FRAME 16, AT THE NR 1 DOOR STOP. REPLACED THE INTERCOSTAL IAW EA 289695, AND SRM 51-72-11.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 60,149 hrs · 22,744 cycles

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

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 60,149 hrs · 22,744 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY AND IS WORN. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-A.

Part: WINDOW FRAME — CRACKED (FRAME 4) · airframe 60,149 hrs · 22,744 cycles

A CRACK INDICATION FOUND ON THE LEFT WINDSHIELD FRAME, FRAME 4, +Y1292. REPAIRED THE WINDSHIELD FRAME IAW EA 289742.

Part: FITTING — CRACKED (WINDOW POST) · airframe 60,149 hrs · 22,744 cycles

WINDSHIELD CENTER POST, LEFT CONTINUITY FITTING FOUND CRACKED BETWEEN FRAMES 1 AND 2. REPLACED THE CONTINUITY FITTING IAW EA 289470.

Part: DRIVE SHAFT — FAILED (BRAKE TACH) · airframe 59,588 hrs · 22,514 cycles

AFTER TAKE OFF, RECEIVED A BRAKE AUTO BRAKE FAULT. DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 4 MAIN WHEEL TACHOMETER DRIVE SHAFT IAW AMM 32-42-68-400 AND AMM 32-42-00-810-815A. OPS TESTED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,575 hrs · 22,507 cycles

NR 2 FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT IAW AMM 25-65-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 59,536 hrs · 22,491 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD ENTRANCE (1L) EMERGENCY FLASHLIGHT IS DEAD. REPLACED FORWARD EMERGENCY FLASHLIGHT PER AMM 25-65-00.

Part: BUSTLE — DETACHED (L4 DOOR SLIDE) · airframe 59,449 hrs · 22,456 cycles

L4 DOOR ESCAPE SLIDE BUSTLE DETACHED. MAINTENANCE SECURED THE SLIDE COVER AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 59,323 hrs · 22,415 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD EMERGENCY LIGHT POWER SUPPLY HAS "EXT LOADS" FAULT MESSAGE. REPLACED EMERGENCY LIGHT POWER SUPPLY (10WL) PER AMM 33-51-38-401. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTO BRAKES) · airframe 59,217 hrs · 22,376 cycles

AUTO BRAKE FAULT, BRAKES RELEASED. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TSM 32-42-00-810-815. NO FAULTS NOTED. NO HISTORY IN 30 DAYS. CHANGED THE NR 4 WHEEL TACHOMETER AS PRECAUTION IAW AMM 32-42-57. SYSTEMS CHECK OK.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 58,343 hrs · 22,040 cycles

R3 EMERGENCY EXIT DAMPER BOTTLE PRESSURE LOW. SERVICED THE BOTTLE IAW AMM 52-10-00-614-001-A.

Part: PIN — CORRODED (LT MLG) · airframe 58,343 hrs · 22,040 cycles

LEFT MAIN LANDING GEAR REAR PINTLE PIN CORRODED. THE AIRCRAFT WAS GROUNDED.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 58,119 hrs · 21,961 cycles

ROW 8A EMERGENCY LIGHT, BULB AND COVER MISSING. REPLACED THE LIGHT ASSEMBLY.

Part: TAB — BINDING (GIRT BAR) · airframe 57,678 hrs · 21,796 cycles

CABIN PRESSURE LIGHT ON THE L4 DOOR FLASHES IN FLIGHT WITH INDICATION OF THE L4 SLIDE NOT ARMED ON ECAM DOOR PAGE. WHEN HANDLE PRESSED ON NORMALLY, DOOR ARMING HANDLE INDICATIONS RETURN TO NORMAL. SECURITY TAB FOUND JAMMED AT GIRT BAR RETAINING HOOKS. OPS CHECKED THE L4 DOOR ARMING AND DISARMING GOOD. AIRCRAFT OK FOR SERVICE

Part: BUSTLE — LOOSE (L4 DOOR) · airframe 57,505 hrs · 21,720 cycles

AIRCRAFT WAS NOT GROUNDED. SLIDE PACK COVER AT DOOR 4L IS LOOSE. REPOSITIONED AND RESECURED 4L DOOR BUSTLE.

Part: CLAMP — BROKEN (BLEED DUCT) · airframe 57,239 hrs · 21,626 cycles

AFTER TAKEOFF, CLIMBING THRU 3500FT, RECEIVED A NR 1 ENGINE FIRE ECAM. FOLLOWED BY AN NACELLE OVERHEAT INDICATION. A BLEED LEAK IN THE THE NR 1 NACELLE. FOUND THE LOWER OVERPRESSURE VALVE BAND CLAMP BROKEN. REPLACED LOWER BAND CLAMP IAW AMM 36-11-53. THE AIRCRAFT WAS GROUNDED.

Part: CLAMP — BROKEN (LT ENG BLEE DUCT) · airframe 57,239 hrs · 21,626 cycles

AFTER TAKEOFF, LEFT ENGINE FIRE AND OVERHEAT WARNING ILLUMINATED ON THE ECAM, INSPECTED AND FOUND A BROKEN CLAMP ON THE ENGINE BLEED DUCT, CLOSE TO OVER PRESSURE VALVE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ENTRY DOOR) · airframe 57,163 hrs · 21,597 cycles

THE AIRCRAFT WAS NOT GROUNDED. LEFT FORWARD ENTRY DOOR NOT CLOSED. INDICATION AFTER PUSHBACK. PERFORMED CIDS RESET AND TEST. SYSTEM OPERATIONS CHECK OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,339 hrs · 21,285 cycles

ENROUTE, F/AS REPORTED A STRONG BURNING RUBBER ODOR APPROXIMATELY ROWS 19 - 21,4 D.H. ODOR DISSIPATED. ACCOMPLISHED TROUBLESHOOTING CABIN AIR QUAILTY IAW J.C.26L00021001. RAN APU WITH BOTH PACKS ON FOR 20 MINS. NO ODOR FOUND. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,196 hrs · 21,222 cycles

EMERGENCY LENS MISSING AT SEAT 9E. REPLACED THE LENS IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,462 hrs · 20,931 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,424 hrs · 20,917 cycles

MISSING EXIT SIGN LENS COVER AT R4 DOOR. REPLACED THE LENS.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 55,353 hrs · 20,891 cycles

AFT FLASHLIGHT INOPERATIVE. INSTALLED NEW SERVICEABLE FLASHLIGHT.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 55,268 hrs · 20,861 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO FLOOR PANEL 151MK. REPLACED AFT CARGO FLOOR PANEL 151MK PER AMM 53-42-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 55,268 hrs · 20,861 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO FLOOR PANEL 151LF. REPLACED AFT CARGO FLOOR PANEL 151LF PER AMM 53-42-14.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 54,886 hrs · 20,710 cycles

R1 DOOR EXIT LIGHT LENS DETACHED. REPLACED THE LIGHT COVER.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 54,735 hrs · 20,657 cycles

LENS BROKEN. REPLACED THE BROKEN EMERGENCY LIGHT LENS AT ROW 22L.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,294 hrs · 20,488 cycles

EMERGENCY LIGHT COVER AT SEAT 8C MISSING. REPLACED MISSING LENS.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 54,146 hrs · 20,427 cycles

SEAT 21DEF EXIT SIGN MISSING. REPLACED THE SIGN.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 53,949 hrs · 20,350 cycles

DURING AN A-8 CHECK, FOUND WALL MOUNTED EXIT EMERGENCY LIGHTS AT RT & LT AFT PAX SERVICE DOORS IN AFT GALLEY NOT WORKING. FOUND BOTH AFT GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLIES DISCONNECTED, CONNECTED THE LIGHTS, OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 53,949 hrs · 20,350 cycles

DURING A-8 CHECK FOUND WALL MOUNTED EXIT EMERGENCY LIGHTS AT RT AFT PAX SERVICE DOORS IN AFT GALLEY NOT WORKING. FOUND BOTH AFT GALLEY WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLIES DISCONNECTED, CONNECTED THE LIGHTS.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 53,736 hrs · 20,266 cycles

DURING ABORTED TAKEOFF, FULL TAKEOFF THRUST WAS NEVER APPLIED DUE TO NR 1 ENGINE LAGGING. SPEED AT TAKEOFF REJECTION LESS THAN 10 KNOTS. AIRCRAFT WAS GROUNDED. PERFORMED TSM 71-00-00-810-807-A. CHECK PERFORMED & FOUND WITHIN LIMITS IAW AMM 71-00-00-710-02 5-A.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,282 hrs · 20,085 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 14 MISSING IT`S LENS. INSTALLED THE LENS IAW AMM 33-51-19. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS.

Part: LENS — MISSING (CABIN) · airframe 52,980 hrs · 19,969 cycles

EMERGENCY FLOOR LIGHT RED LIGHT MISSING AT 9D. REPLACED RED FLOOR LIGHT LENS COVER AT 9D IAW AMM 33-50-00. OK FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED,

Part: FAN — FAULTY (ZONE 200) · airframe 52,857 hrs · 19,916 cycles

AIRCRAFT WAS NOT GROUNDED. BLOWER VENT FAULT STARTED WITH LOUD NOISE, ELECTRICAL BURNING SMELL, THEN THE FAULT. MAINTENANCE INSTALLED NEW BLOWER FAN PER AMM 21-26-51.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 52,725 hrs · 19,862 cycles

CRACK INDICATION ON AFT RIGHT BOX BEAM UPPER FLANGE 2 HOLES AT FRAME 43 AND -Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 52,725 hrs · 19,862 cycles

CRACK INDICATIONS ON LEFT SIDE BOX BEAM UPPER FLANGE AFT 2 HOLES AT FR 43 AND Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Part: LENS — MISSING (CABIN) · airframe 51,910 hrs · 19,534 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 27 ABC EMERGENCY LIGHT IS MISSING LENS. INSTALLED LENS IAW AMM 33-51-11 AND 33-50-00.

Part: ATTACH FITTING — WORN (LT AILERON) · airframe 51,526 hrs · 19,390 cycles

AIRCRAFT IN BASE MX. LEFT WING AILERON SERVO CONTROL ACTUATOR ATTACH FITTING LOCATED ON THE INBD SIDE OF THE AILERON WAS WORN. REPLACED THE LT WING AILERON IAW AMM 27-14-41-400-001-A.

Part: ATTACH FITTING — DAMAGED (FRAME 42) · airframe 51,526 hrs · 19,390 cycles

LT MLG DOOR ACTUATOR ATTACH POINT ON KEEL BEAM FWD LUG BUSHING BORE HOLE OVERSIZED & BUSHING LOOSE. ACCOMPLISHED FINAL RESTORATION INSTRUCTIONS ON EA 253285D BY REPLACING THE LT MLG DOOR FWD ACTUATOR FITTING LUG IAW SRM 51-42-11, DWG D53372720 & EA 253285D.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 51,526 hrs · 51,526 cycles

LT AFT NOSE GEAR DOOR LOOSE. REPLACED FWD HINGE FITTING ON THE LT AFT NOSE GEAR DOOR IAW CMM 52-82-32-405-805-A0.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 51,526 hrs · 19,390 cycles

RT AFT NOSE GEAR DOOR LOOSE. REPLACED FWD HINGE FITTING ON THE RT AFT NOSE GEAR DOOR IAW CMM 52-82-32-405-805-A01.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 51,526 hrs · 19,390 cycles

AIRCRAFT WAS IN BASE MX. LT WING ACCESS PANEL 540JB HAS CORROSION ON COUNTERSINKS. R & R ACCESS PANEL IAW SRM A321 51-72-11 & JC 26T54057001.

Part: FITTING — CRACKED (ZONE 800) · airframe 51,526 hrs · 19,390 cycles

AIRCRAFT IN BASE MX. RT MLG DOOR FWD DOOR ATTACHMENT FITTING ON THE KEEL BEAM HAS CRACK INDICATION. REPLACED FITTING IAW SRM 51-72-11 & DWG D53372720 & EA 260782.

Part: CABLE — DEFECTIVE (CABIN) · airframe 50,329 hrs · 18,925 cycles

AIRCRAFT WAS NOT GNDED. AFT LT ROW, SEAT'S EMER LIGHT INOPERATIVE. REPLACED CABLE FROM WALL PLUG TO SEAT. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-11.

Part: COVER — BROKEN (CABIN) · airframe 50,200 hrs · 18,875 cycles

AIRCRAFT WAS NOT GNDED. ROW 9D EMERGENCY EXIT LIGHT PLASTIC COVER BROKEN. REPLACED EMER EXIT LIGHT COVER.

Part: FAN — DEFECTIVE (E&E BAY) · airframe 50,150 hrs · 18,855 cycles

AIRCRAFT WAS GNDED. RECEIVED VENT EXTRACT FAULT & NOTICED A BURNT SMELL. REPLACED AVIONICS EXTRACT FAN 18HQ, & AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-26-51.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,443 hrs · 18,576 cycles

REJECTED TAKEOFF DUE TO THRUST LEVER ECAM FAULT AT APPROX 50 KNOTS. MAX BRAKE TEMP OBSERVED 210 DEGREES C. NO ECAM POST FLIGHT REPORT. PERFORMED POWER ASSURANCE CHECK IAW AMM 71-00-00-710-008-B. UNABLE TO DUPLICATE & OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 48,011 hrs · 17,996 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 34L. REPLACED THE EMER AISLE LIGHT LENS AT ROW 34L.

Part: UNKNOWN — MALFUNCTIONED · airframe 47,408 hrs · 17,752 cycles

ANTI-SKID, ALTERNATE BRAKE & NO NOSE WHEEL STEERING UPON GATE ARRIVAL. ACCOMPLISHED TSM 32-42-00-810-823-A & TSM 32-42-00810-807-A. SYS CHECKED GOOD. NO FAULTS DISPLAYED ON ECAM.

Part: LENS — MISSING (CABIN) · airframe 47,373 hrs · 17,737 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT ROW 9ED. REPLACED EMER LIGHT ASSEMBLY AT SEAT 9ED IAW AMM 33-50-00. OPERATIONAL CHECKED GOOD.

Part: MANIFOLD — LEAKING (HYDRAULIC SYS)

AIRCRAFT RETURNED TO FIELD. HYD RESERVOIR YELLOW SYS INOPERATIVE. FOLLOWED ECAM PROMPTLY WHICH CALLED FOR YELLOW ENG PUMP & PTU OFF. REPLACED GND SERVICE MANIFOLD & LEAK CHECK SYS IAW AMM 29-19-41, NO LEAK FOUND. OK FOR SERVICE.

Part: CHILLER — ODOR (AFT GALLEY) · airframe 46,363 hrs · 17,330 cycles

FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR IN AFT GALLEY. ODOR STOPPED AFTER TURNING CHILLER OFF. R & R AFT GALLEY CHILLER IAW AMM 25-34-51.

Part: SENSOR — FAULTY (NR 3 BRAKE) · airframe 45,710 hrs · 17,068 cycles

AFTER TAKEOFF CREW RECEIVED ECAM WARNING BRAKES HOT, INDICATED 995 DEG C ON BRAKE NR 3. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. R & R NR 3 BRAKE TEMP SENSOR IAW AMM 32-47-15-000-001A. OPERATIONS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 44,784 hrs · 16,710 cycles

THE SEAT MOUNTED EMERGENCY EXIT LIGHT MISSING AT ROW 1 A - C. R & R SEAT ASSEMBLY IAW AMM 25-21-41-000-001-A, CHECKED GOOD.

Part: LENS — BROKEN (EXIT SIGN) · airframe 44,383 hrs · 16,535 cycles

CREW REPORTED THE 4R DOOR EXIT SIGN COVER BROKEN. REPLACED LENS, OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 44,310 hrs · 16,502 cycles

CREW REPORTED PROBLEMS WITH CABIN EMERGENCY LIGHTS TURNING ON & OFF ON THEIR OWN. MX RESET POWER & ACCOMPLISHED SATISFACTORY OPERATIONS TEST OF EMERGENCY LIGHT SYS. CHECKED OK IAW AMM 33-51-00.

Part: BOTTLE — INOPERATIVE (DOOR ASSIST) · airframe 42,832 hrs · 15,834 cycles

CIDS CAUTION PANEL LIGHT ON. R & R INFLATION RESERVOIR BOTTLE IAW AMM 25-62-49-401.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,500 hrs · 15,691 cycles

ROW 5C MISSING EMERGENCY LIGHT LENS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42,157 hrs · 15,540 cycles

FLIGHT DEPARTED, ENROUTE, ON A MX FERRY FLIGHT DUE TO A CRACKED CAPTAINS LT FIXED WINDOW. AT FL230, CREW REPORTED A LOUD BANG AND WINDSHIELD STARTED TO CRACK AND THERE WAS A DIFFERENTIAL IN THE PRESSURIZATION. CREW DETERMINED TO RETURN TO FIELD. A NORMAL LANDING WAS MADE AND ACFT WAS NOT OVERWEIGHT. MX R & R CAPTAIN'S AFT FIXED WINDOW IAW AMM 56-11-12-400-002-A.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 41,970 hrs · 15,463 cycles

ROW 30 EMERGENCY LIGHT INOPERATIVE. FOUND BAD CABLE CONNECTOR UNDER SEAT, WIRING WILL NOT SECURE TO CONNECTOR. REPLACED UNDER SEAT CABLE HOUSING AT ROW 30.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 41,283 hrs · 15,184 cycles

THE 4L DOOR DIFFICULT TO ARM AND DISARM. REMOVED DEBRIS FROM UNDER GIRT BAR.

Part: HINGE FITTING — EXCESS PLAY (NR 4 ELEVATOR) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - EXCESSIVE PLAY AT RIGHT NR 4 ELEVATOR HINGE FITTING ASSEMBLY BETWEEN HORIZONTAL STABILIZER STA 2707 TO STA 3416 ALSO BETWEEN RIB 7 TO RIB 9. REPLACED RIGHT NR 4 ELEVATOR HINGE FITTING ASSEMBLY IAW A321 AMM 55-16-42.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - OUT OF ADJUST STRIKER LEVER MEASURE DIMENSION "J2" ON DOOR DAMPER MECHAMISM AT 831 DOOR. ACCOMPLISHED ADJUSTMENT OF STRIKER LEVER MEASUREMENT DIMENSION "J2" AT DOOR 831 IAW A321 AMM 52-11-14-820-002-A, PROCEDURE 3, ITEM D & 4, ITEM A, STEP 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR59+6 INCHES TO FR63, -Y765. REPAIRED SEAT TRACK BETWEEN FR59+6 INCHES TO FR63, -Y765 IAW A321 SRM 53-41-15, PAR 5B, PG 209-216 & AIRBUS DRAWING 53472079.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR24 TO FR26+10 INCHES, Y254. REPAIRED SUPPORT FLOOR BETWEEN FR24 TO FR26+10 INCHES, Y254 IAW EA 503923.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER SHAPE SILL FITTING BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23R. REPLACED CENTER SHAPE SILL FITTING BETWEEN FR66+5 INCHES TO FR67+16 INCHES, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT RIGHT AFT PASSENGER DOORWAY AT FR68, S23R. REPLACED CORNER FITTING AT RIGHT AFT PASSENGER DOORWAY AT FR68, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CRACK ON CONNECTING SECTION SPLICE AT FR68, -Y1162. REPLACED CONNECTING SECTION SPLICE AT FR68, -Y1162 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53480505.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL DOOR 540HB BETWEEN WS 7316 TO WS 7792 BETWEEN RIB 13 TO RIB 14. REPLACED LEFT WING LOWER FUEL DOOR 540HB IAW A321 SRM 51-72-11.

Part: ACCESS DOOR — DAMAGED (LT WING) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - ELONGATED HOLE ON LEFT WING FUEL DOOR 540LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 16 TO RIB 17. REPLACED LEFT WING FUEL DOOR 540LB IAW A321 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT L1 DOORWAY BETWEEN FR16 TO FR20, S23L. REPLACED FITTING AT L1 DOORWAY BETWEEN FR16 TO FR20, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112225.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING OF R1 DOORWAY BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING OF R1 DOORWAY BETWEEN FR16 TO FR20, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112225.

Part: STRUT — CORRODED (RT WING) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 407 TO WS 486 & BETWEEN RIB 8 & RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT IAW JOB CARD 26C67057001.

Part: STRUT — CORRODED (LT WING) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 & RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW A321 AMM 27-51-44.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR45+3 INCHES, -Y1292. REPLACED SEAT TRACK AT SEAT TRACK AT FR45+3 INCHES, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53372500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 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 51-72-11, AIRBUS DRAWING D53372500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CABIN SEAT TRACK CORRODED BETWEEN FR 36 AND FR 41 AT Y 1292. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM A321 51-72-11 AND AIRBUS DRAWING D57130147.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46+16 INCHES, -Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR46+16 INCHES, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53372500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CABIN SEAT TRACK IS CORRODED BETWEEN FR 41 AND FR 47 AT Y 1292. REMOVED AND REPLACED SEAT TRACK IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53372500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

DISCOVERED CORROSION ON SEAT TRACK Y765 LOCATED BETWEEN FR 41 TO FR 46 + 16" IN THE CENTER PAX CABIN FLOOR STRUCTURE (5 POINTS). THE SEAT TRACK AND FASTENERS WERE REPLACED IAW SRM A321 51-72-11 AND DRAWING D53372500.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - EXCESSIVE PLAY ON NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2632, RIB 6. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 2632, RIB 6 IAW A321 SRM 51-72-11 & AMM 55-36-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47.5 TO FR62+15 INCHES, Y765. REPLACED SEAT RAIL BETWEEN FR47.5 TO FR62+15 INCHES, Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472650 & D53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR35 TO FR35.8, -Y765. REPLACED SEAT TRACK BETWEEN FR35 TO FR35.8, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53235007.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, AT -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, AT -Y1292 IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53112812.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE ARM FITTING NR 2 AT RUDDER STA 120/BR2, RIB 4. REPLACED RUDDER HINGE ARM FITTING NR 2 AT RUDDER STA 120/BR2, RIB 4 IAW A321 SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - EXCESSIVE PLAY ON NR 1 RUDDER HINGE AT VERTICAL STABILIZER STA 780, RIB 2. REPLACED NR 1 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 780, RIB 2 IAW A321 SRM 51-72-11 & 51-42-11.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - ELONGATED HOLE ON SPLICE COUPLING AT FR64, -Y1292. REPLACED SPLICE COUPLING AT FR64, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47.5 TO FR63, -Y1292. REPLACED SEAT TRACK BETWEEN FR47.5 TO FR63, -Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472817.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT WEB BETWEEN FR20 TO FR24, S23R, -Y1732. REPLACED SUPPORT WEB BETWEEN FR20 TO FR24, S23R, -Y1732 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53112379 & D53112261.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR14 TO FR16, AT Y503.2. REPLACED RAIL DUMMY BETWEEN FR14 TO FR16, AT Y503.2 IAW SRM A321 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112816.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, Y765. REPLACED SEAT TRACK AT FR20, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112812 & D53115054.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR20-FR24, AT -Y189. REPLACED FLOORBEAM BETWEEN FR20-FR24, AT -Y189 IAW A321 SRM 51-42-11 AND AIRBUS DRAWING D53111406.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR62+15 INCHES TO FR64, -Y1292. REPLACED SEAT TRACK BETWEEN FR62+15 INCHES TO FR64, -Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53472817.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, AT Y1732. REPLACED WEB BETWEEN FR20 TO FR24, AT Y1732 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112812.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47.5 TO FR63, Y1292. REPLACED SEAT RAIL BETWEEN FR47.5 TO FR63, Y1292 IAW A321 SRM 51-72-11, AIRBUS DRAWING 53472817.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR63 TO FR64, -Y765. REPLACED SEAT TRACK BETWEEN FR63 TO FR64, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR14 TO FR16, AT -Y81. REPLACED DUMMY RAIL BETWEEN FR14 TO FR16, AT -Y81 IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53112828.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y765. REPLACED SEAT TRACK BETWEEN FR59+6 INCHES TO FR63, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234930.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

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

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR64 TO FR67+10 INCHES, Y512. REPLACED BEAM ASSEMBLY BETWEEN FR64 TO FR67+10 INCHES, Y512 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR65 TO FR66, AT Y1732. REPLACED BEAM ASSEMBLY BETWEEN FR65 TO FR66, AT Y1732 IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53474250.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - CORROSION ON AFT PAX CABIN FLOORBEAM. REPLACED FLOORBEAM AND FASTENERS IAW A321 SRM 51-72-11 AND DRAWING D534 72816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, S23R, -Y1732. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, S23R, -Y1732 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT AFT LEFT PASSENGER DOOR WAY BETWEEN FR66 TO FR68, S23L. REPLACED LOWER SILL AT AFT LEFT PASSENGER DOOR WAY IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503875.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON AUXILIARY BEAM ASSEMBLY BETWEEN FR64 TO FR66, Y512. REPLACED AUXILIARY BEAM ASSEMBLY BETWEEN FR64 TO FR66, Y512 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON CLEAT AT FR30, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR30, BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53234411.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FISH PLATE AT FR30+15 INCH, S42L. REPLACED FISH PLATE AT FR30+15 INCH, S42L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT AFT RIGHT PASSENGER DOOR WAY BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SILL AT AFT RIGHT PASSENGER DOOR WAY IAW A321 SRM 51-72-11, AIRBUS DRAWING D53480505 & EA 503888.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FISH PLATE AT FR30+15 INCHES, S43L. REPLACED FISH PLATE AT FR30+15 INCHES, S43L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

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

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151LF BETWEEN FR56 TO FR58, -Y765 TO Y765. REPLACED FLOOR PANEL 151LF IAW SRM 53-02-00 PARAGRAPH 8H, FIGURE 209 AND IRM 9701 REV G.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON CLEAT AT FR33, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR33, BETWEEN S40R TO S41R IAW A321 51-72-11 AND AIRBUS DRAWING D53234411.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON FISH PLATE AT FR30+15 INCHES, S41L. REPLACED FISH PLATE AT FR30+15 INCHES, S41L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, AT -Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, AT -Y1292 IAW A321 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON BEAM ASSEMBLY AT FR66, -Y465. REPLACED BEAM ASSEMBLY AT FR66, -Y465 IAW A321 SRM 51-72-11 & AIRBUS DRAWING 53472816.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.1 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR35.1 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53235027.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR34 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR34 BETWEEN S41R TO S42R IAW A321 SRM 51-72-11 & AIRBUS DRAWING 53234411.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151GF LOCATED BETWEEN FR 52 TO FR 56 AND BL Y-765 TO Y765. REPLACED FLOOR PANEL 151GF IN AFT CARGO COMPARTMENT IAW A321-211 SRM 53-02-00 PAR 8H FIGURE 209 AND IRM 9701 REV G.

Part: LEVER — DAMAGED (COCKPIT) · airframe 41,079 hrs · 15,084 cycles

2S CHECK - ELONGATED HOLE ON LEFT INBOARD FLAP LEVER ASSEMBLY. REPLACED LEFT INBOARD FLAP LEVER ASSEMBLY IAW A321 CMM 57-52-23.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · corrosion level 2 · airframe 41,079 hrs · 15,084 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151DF BETWEEN FR50 TO FR53 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 151DF IAW A321 SRM 53-02-00, PAR 8H, FIG. 209 & IRM 9701 REV G.

Part: TARGET — OUT OF ADJUST (L4 DOOR) · airframe 40,612 hrs · 14,876 cycles

L4 DOOR DISARMED ITSELF DURING CLIMBOUT. AIRCRAFT PRESSURIZED NORMALLY BUT ECAM SHOWED DOOR DISARMED AND RED LIGHTS WERE FLASHING ON FLIGHT ATTENDANT PANEL. ADJUSTED TARGET FOR SLIDE ARM SWITCH IAW AIRBUS MAINTENANCE MANUAL 52-13-22.

Part: BEAM — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

LP8009195-13 - CORROSION ON Z-BEAM BETWEEN FR66 TO FR69, Z-500, -Y1162.5. REPLACED Z-BEAM BETWEEN FR66 TO FR69, Z-500, -Y1162.5 IAW A312 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CRACK ALONG TOP CENTER OF SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480019.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON UPPER SURFACE OF SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23L IAW AIRBUS DRAWING D534711240200.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y765 IAW A321 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON FLOORBEAM AT FR66, Z-500, -Y1162.5. REPLACED FLOORBEAM AT FR66, Z-500, -Y1162.5 IAW A321 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, Z-500, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Z-500, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Z-500, -Y765 IAW AIRBUS DRAWING # D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y1192. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, Z-500, Y1192 IAW AIRBUS DRAWING D5347218820400.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 40,450 hrs · 14,801 cycles

FUSELAGE REPAIR - CORROSION ON UPPER SURFACE OF SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, S23R IAW TYPICAL REPAIR TR320-2528-10-0011E & AIRBUS DRAWING D533474180.

Part: PLATE — CRACKED (LT PYLON) · airframe 40,116 hrs · 14,665 cycles

RON VISIT - LEFT ENGINE PYLON AFT MOUNTING PLATE ASSEMBLY IS CRACKED/BROKEN. REPLACED LEFT ENGINE PYLON AFT MOUNTING PLATE ASSEMBLY IAW A321 SRM 51-42-11.

Part: PLATE — CRACKED (LT PYLON) · airframe 40,116 hrs · 14,665 cycles

RON VISIT - LEFT ENGINE PYLON AFT MOUNTING PLATE ASSEMBLY IS CRACKED/BROKEN. REPLACED LEFT ENGINE PYLON AFT MOUNTING PLATE ASSEMBLY IAW A321 SRM 51-42-11.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 39,998 hrs · 14,614 cycles

SLIDE PRESSURE AT 3R DOOR LOW. REMOVED AND REPLACED INFLATION RESERVOIR IAW AIRBUS MAINTENANCE MANUAL 25-62-49-400-001-A.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 39,772 hrs · 14,523 cycles

SEAT 31ABC EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE ON HARNESS UNDER SEAT 31ABC. REPLACED HARNESS.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,611 hrs · 14,465 cycles

SEVERAL AFT INTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AIRBUS MAINTENANCE 33-51-38.

Part: SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 38,846 hrs · 14,179 cycles

EMERGENCY LIGHTS REMAIN ON. REMOVED AND REPLACED EMERGENCY LIGHT TOGGLE SWITCH IAW AIRBUS MAINTENANCE MANUAL 20-45-21.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 38,581 hrs · 14,072 cycles

WHEN EMERGENCY EXIT LIGHT SWITCH IS TURNED OFF, THE LIGHTS TURN ON. RESET AIRCRAFT POWER - OPERATIONAL TEST NORMAL.

Part: LENS — MISSING (CABIN) · airframe 38,496 hrs · 14,042 cycles

LENS CAP MISSING FOR EMERGENCY FLOOR LIGHTING ROWS 8 & 9. INSTALLED LENSES.

Part: LENS — MISSING (CABIN) · airframe 38,254 hrs · 13,951 cycles

EMERGENCY EXIT LIGHT COVER ROW 9D SEAT MOUNTED MISSING. MAINTENANCE REPLACED MISSING LIGHT COVER AT 9D.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,670 hrs · 13,703 cycles

EMERGENCY EXIT LIGHT AT DOOR 3R INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-401-001.

Part: RESERVOIR — DEFECTIVE (R3 DOOR) · airframe 37,413 hrs · 13,597 cycles

GALLEY MAT CHECK - SAFETY PIN DID NOT ENGAGE R3 DOOR RESERVOIR OPERATION VALVE CAUSING SLIDE DEPLOYMENT WHEN DOOR OPENED. REPLACED R3 DOOR RESERVOIR ASSEMBLY IAW A312 AMM 25-62-49-000-001 & 33-51-00-710-001.

Part: SLIDE — DEPLOYED (R3 DOOR) · airframe 37,413 hrs · 13,597 cycles

GALLEY MAT CHECK - SAFETY PIN DID NOT ENGAGE R3 DOOR RESERVOIR OPERATION VALVE CAUSING SLIDE DEPLOYMENT WHEN DOOR OPENED. REPLACED R3 DOOR SLIDE ASSEMBLY IAW A312 AMM 25-62-47-400.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 36,983 hrs · 13,431 cycles

R3 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R3 DOOR ASSIST PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: LENS — MISSING (CABIN) · airframe 36,297 hrs · 13,192 cycles

RED LENS COVER EMERGENCY EXIT AT SEAT 8C MISSING. MAINTENANCE INSTALLED NEW LENS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 35,973 hrs · 13,092 cycles

EMERGENCY EXIT LIGHT DOOR 1R INOPERATIVE. MAINTENANCE TIGHTENED AND SECURED CONNECTOR IAW AIRBUS MAINTENANCE MANUAL 33-50-00.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 35,973 hrs · 13,092 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT AISLE 31. MAINTENANCE ADJUSTED EXIT LIGHT CONNECTOR AS REQUIRED IAW AIRBUS MAINTENANCE MANUAL 20-18-01.

Part: LENS — MISSING (CABIN) · airframe 34,801 hrs · 12,688 cycles

MX - LAX - EEL - FORWARD LAV EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED EMERGENCY LIGHT LENS.

Part: LENS — IMPROPER PART (CABIN) · airframe 32,901 hrs · 11,946 cycles

FLT 1243 - PHL - EEL - LENS COVER ON EMERGENCY EXIT ROW 8C IS THE WRONG COLOR. MAINTENANCE REPLACED EMERGENCY AISLE LENS COVER.

Part: A/C PACK — LOW PRESSURE (R3 DOOR) · airframe 32,592 hrs · 11,832 cycles

FLT 964 - SFO - EES - CIDS PANEL CAUTION LIGHT ILLUMINATED FOR R-3 DOOR. MAINTENANCE SERVICED R-3 DOOR ASSIST BOTTLE.

Part: ACTUATOR — LOW PRESSURE (EMERGENCY EXIT) · airframe 32,133 hrs · 11,648 cycles

LOG PAGE 8749849 - FLT 1970-CLT - EES - CHECK ALL SLIDE DOOR BOTTLE PRESSURE INDICATIONS FOR PROPER READINGS AND INTERFACE WITH CIDS CAUTION PANEL. MAINTENANCE SERVICED R3 DOOR ACTUATOR PER AIRBUS MAINTENANCE MANUAL 52-22-00. ALL FAULTS CLEARED.

Part: LENS — MISSING (CABIN) · airframe 31,719 hrs · 11,459 cycles

FLT 1515 - LAS - EEL - FLOOR PROXIMITY EXIT LIGHT LENS MISSING AT R4 DOOR. MAINTENANCE INSTALLED NEW LENS AT R4 DOOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,593 hrs · 11,389 cycles

FLT 1791 - TPA - EEL - 4L DOOR EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY. OPERATIONAL CHECK WAS NORMAL.

Part: STRUCTURE — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER INGRESSION ON RIGHT ELEVATOR AT SEVERAL AREAS FROM 29 TO 90 INCHES FROM INBOARD END & 28 TO 9 INCHES FROM ELEVATOR TRAILING EDGE. REPLACED RIGHT ELEVATOR IAW A321 AMM 27-34-41.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 173 INCHES FROM INBOARD END & 5.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 40 INCHES FROM INBOARD END & 6 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 165 TO 167 INCHES FROM INBOARD END & 6 TO 9.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 87 INCHES FROM INBOARD END & 21.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FRAME CLEATS AT FR 35.1 TO FR 35.5 & BETWEEN S40R TO S41R. REPLACED FRAME CLEATS AT FR 35.1 TO FR 35.5 & BETWEEN S40R TO S41R IAW A321 SRM 51-42-11, 51-72-11 & 53-21-12.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 105 INCHES FROM INBOARD END & 17 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,244 hrs · 11,222 cycles

PIT - C11 - MAJOR REPAIR - WATER DAMAGE ON LEFT ELEVATOR UPPER SURFACE COMPOSITE 21 INCHES FROM INBOARD END & 7.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE COMPOSITE IAW A321 SRM 55-21-11.

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR) · airframe 30,020 hrs · 10,814 cycles

FLT 1145 - PHL - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ON LEFT ENTRY DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 29,963 hrs · 10,799 cycles

FLT 1433 - CABIN ODOR - SHORTLY AFTER TAKEOFF ACRID ODOR IN COCKPIT AND CABIN. SELECTED COND PAGE AND HAD AMBER "FAN". TURNED CABIN FAN SWITCH (OVERHEAD) OFF AND ODOR WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN PER MM 21-21-51-04 AND REPLACED BOTH FILTERS PER AMM 21-21-41-04.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 28,098 hrs · 10,153 cycles

FLT 752 - SEA - PHL - EMERGENCY EQUIPMENT - L1 DOOR EMERGENCY CYLINDER ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED L1 DOOR EMERGENCY CYLINDER ACCUMULATOR TO PROPER PRESSURE PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

RIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1.5 SQ INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

RIGHT FLOORBEAM TOP FLANGE FROM FR 64-FR 69, -Y1160 TO -Y1192 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1.5 SQ INCH.

Part: GIRT BAR — OUT OF ADJUST (ZONE 200)

PHL - THE CABIN CREW STATED THAT THE EMERGENCY ESCAPE SLIDE ARMING LEVER AT DOOR 4L KEEPS POPPING OUT. MAINTENANCE ADJUSTED THE GIRT BAR FITTING. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,963 hrs · 7,719 cycles

RIGHT FLOORBEAM TO FLANGE FROM FR 64-68; -Y1160 TO -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 SQ INCH.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 20,963 hrs · 20,963 cycles

PANEL 251 AG FRAME 47-47.5 DAMAGED. MANUFACTURED NEW PANEL PER MCGILL IRM 9701 REV F, DEFECT SIZE: 2 X 1 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

Y254 AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 5 X 5 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

LEFT FLOORBEAM ON TOP FLANGE FROM FR 65-69 AT Y1160 - 1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER DWG D53472815, SRM 51-74-12; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 8 INCHES SQ.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

FLOORBEAM Y-254 FR 17-19 HAS CORROSION. REMOVED AND REPLACED BEAM PER SRM 53-00-14; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: .5 X 4 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,963 hrs · 20,963 cycles

RIGHT FLOORBEAM TOP FLANGE FROM FR 64-69, -Y1160-1292 HAS CORROSION. REMOVED AND REPLACED 3 FLOORBEAMS PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 4 SQ INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,963 hrs · 20,963 cycles

FLOORBEAM AT Y765 AT LAV D AFT MOUNT NEAR FRAME 66 HAS CORROSION. REMOVED & REPLACED WITH IDENTICAL PART PER SRM 53-00-14 FIG 102, DEFECT SIZE: 2 SQ INCHES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

THE FORWARD EMERGENCY POWER SUPPLY UNIT, FIN 10WL, WILL NOT TEST. MAINTENANCE REPLACED THE BATTERY PACK FOR THE FORWARD EMERGENCY POWER SUPPLY UNIT, FIN 10WL. OPERATIONALLY CHECKS OK.

Part: LANDING GEAR — MALFUNCTIONED

PIT - FLT 45 - EN ROUTE PIT-LAX, AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR, BUT THE CONDITION REMAINED THE SAME. FLIGHT RETURNED TO FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE EQUIPMENT WAS CALLED OUT BY ATC. (M)

Part: LIGHT — INOPERATIVE (PAX CABIN)

LGA - THE EMERGENCY LIGHT SYSTEM FAILED THE EMERGENCY LIGHT SYSTEM TEST. MAINTENANCE REPLACED THE RIGHT SIDE, FIRST POSITION, EMERGENCY ESCAPE SLIDE. SYSTEM TESTS OK. (M)