N538UW

Part: WIRE — BROKEN (ZONE 200) · airframe 49,897 hrs · 20,241 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SIDE OF SEAT 36C DOES NOT OPERATE DURING EMERGENCY LIGHTING TEST. MAINTENANCE FOUND A BROKEN WIRE AND REPAIRED IT PER ESPM 20-43-11. A SATISFACTORY OPERATIONAL CHECK WAS AQCCOMPLISHED WITH NO ISSUES NOTED.

Part: LIGHT — NO TEST (ZONE 200) · airframe 49,897 hrs · 20,241 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SIDE OF SEAT 36C DOES NOT OPERATE DURING EMERGENCY LIGHTING TEST. (OPEN)

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR 843 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR 844 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: 1R 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 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: 4L 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 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR 834 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 49,157 hrs · 19,919 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: DIAPHRAGM — RUPTURED (ZONE 800) · airframe 49,092 hrs · 19,886 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE FOUND DISCHARGED. REPLACED L1 DOOR DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-610-001-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 48,698 hrs · 19,730 cycles

AIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY 15WL DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 48,696 hrs · 19,729 cycles

AIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE DISPLAYS FOR EMERGENCY POWER SUPPLY UNIT 10WL DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL TEST PER AMM 33-51-38 WITH NO FAULTS NOTED.

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 48,133 hrs · 19,504 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT UNABLE TO ARM L1 DOOR SLIDE, HANDLE DOES NOT MOVE TO ARMED POSITION. MAINTENANCE CLEARED LANYARD,UNDERSIDE OF THE DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER .AMM 52-10-00.

Part: BATTERY — NO TEST (ZONE 200) · airframe 47,788 hrs · 19,347 cycles

AIRCRAFT WAS NOT GROUNDED: MEGAPHONE INOPERATIVE. MAINTENANCE REPLACED MEGAPHONE BATTERIES.

Part: BATTERY — NO TEST (ZONE 200) · airframe 46,601 hrs · 18,811 cycles

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

Part: BATTERY — NO TEST (ZONE 200) · airframe 46,601 hrs · 18,811 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 15WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202411262158) AND BATTERY (AALA202411266431) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 46,601 hrs · 18,811 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 15WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202411262158) AND BATTERY (AALA202411266431) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: LEVER — LOOSE (R3 DOOR) · airframe 46,069 hrs · 18,575 cycles

AIRCRAFT WAS NOT GROUNDED: FA REPORTS DOOR ARMING LEVER ON 3R IS LOOSE. TIGHTENED ARMING FLAG ON 3R DOOR.

Part: LEVER — LOOSE (ZONE 800) · airframe 45,915 hrs · 18,502 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARM/DISARM LEVER LOOSE. TIGHTENED BOLT.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 45,308 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: DOOR 2L CHECK SLIDE PRESSURE MESSAGE. REPLACED 2L SLIDE BOTTLE PER AMM 25-62-49.

Part: DOOR — STUCK (L2 LAVATORY) · airframe 44,874 hrs · 18,050 cycles

AIRCRAFT WAS NOT GROUNDED: L2 LAVATORY DOOR DIFFICULT TO OPEN / WILL NOT OPEN. MAINTENANCE ADJUSTED THE LAVATORY DOOR AND ACCOMPLISHED A SATISFAXCTORY OPERATIONAL CHECK.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 44,623 hrs · 17,942 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY POWER SUPPLY UNIT SYSTEM CHECK FAULT MESSAGE FOR BATTERY / EMERGENCY POWER SUPPLY UNIT 12WL. MAINTENANCE ACCOMPLISHED TSM 33-51-00 AND CLEANED EMERGENCY POWER SUPPLY UNIT 12WL CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 43,904 hrs · 17,604 cycles

AIRCRAFT WAS NOT GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 151MK HAS DELAMINATION. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 42,959 hrs · 17,151 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT STATES 2R FLASHLIGHT IS NOT FLASHING. MAINTENANCE REPLACED FLASHLIGHT ( AALA202310166787) AND FLASHLIGHT HOLDER / BRACKET (AALA202310163289).

Part: BRACKET — INOPERATIVE (ZONE 200 - FUSE) · airframe 42,959 hrs · 17,151 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT STATES 2R FLASHLIGHT IS NOT FLASHING. MAINTENANCE REPLACED FLASHLIGHT ( AALA202310166787) AND FLASHLIGHT HOLDER / BRACKET (AALA202310163289).

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 42,893 hrs · 17,116 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-60-00.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 42,766 hrs · 17,055 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 42,263 hrs · 16,829 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 24 AND 25 EMERGENCY LIGHT INOPERATIVE. DETERMINATED WIRE BROKE AT 7261VC7-A CONNECTER. RETERMINATED THE WIRE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ARMING LEVER — LOOSE (ZONE 800 - DOORS) · airframe 40,600 hrs · 16,075 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR SLIDE ARMING LEVER LOOSE. MAINTENANCE TIGHTENED 3R DOOR SLIDE ARMING LEVER PER AMM 52-22-22.

Part: PLATE — LOOSE (R3 DOOR) · airframe 40,408 hrs · 15,985 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR DISARMING LEVER LOOSE. MAINTENANCE RESECURED 3R DOOR EMERGENCY ARM/DISARM HANDLE PUSH PLATE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-00.

Part: APU — ODOR (ZONE 100) · airframe 40,302 hrs · 15,931 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AND DURING INITIAL CLIMB FUMES WERE SMELLED IN FLIGHT DECK AND ALSO REPORTED IN CABIN BY FLIGHT ATTENDANT. SMELLED LIKE EXHAUST OR OIL. FLIGHT ATTENDANT SAID IT SMELLED LIKE BURNT CRAYONS / MUSTY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU DUE TO FINDING EVIDENCE OF OIL LEAKING FROM THE LOAD COMPRESSOR DRAIN. (OPEN)

Part: APU — CONTAMINATED (ZONE 100 - FUSE) · airframe 40,302 hrs · 15,931 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AND DURING INITIAL CLIMB FUMES WERE SMELLED IN FLIGHT DECK AND ALSO REPORTED IN CABIN BY FLIGHT ATTENDANT. SMELLED LIKE EXHAUST OR OIL. FLIGHT ATTENDANT SAID IT SMELLED LIKE BURNT CRAYONS / MUSTY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU DUE TO FINDING EVIDENCE OF OIL LEAKING FROM THE LOAD COMPRESSOR DRAIN. **SUPPLEMENTAL REPORT FOR AALA202212161331: MAINTENANCE CLEANED THE APU COMPARTMENT PER AMM 49-00-00-100-003-A AND THE APU INTAKE PER TASK CARD 26T31049006. A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM WAS ACCOMPLISHED PER TASK CARD 26L00021004. A FOLLOW UP GENERAL VISUAL INSPECTION OF THE APU COMPARTMENT FOR LEAKS AND ODORS WAS ACCOMPLISHED WITH NO LEAKS OR ODOR NOTED. ** (CLOSED)

Part: RESERVOIR — NONE (ZONE 800 - DOORS) · airframe 39,313 hrs · 15,467 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLIGHT FLIGHT ATTENDANT REPORTED 2L CHECK SLIDE PRESSURE ON FLIGHT ATTENDANT PANEL. REPLACED 2L DOOR SLIDE BOTTLE RESERVOIR PER AMM 25-62-49.

Part: PRESSURE SWITCH — DEFECTIVE (ZONE 500 - LH WI) · airframe 38,906 hrs · 15,293 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT TANK #1 LOW PRESSURE ECAM DURING DESCENT. REPLACED FUEL PRESSURE SWITCH 23QA PER AMM 28-21-15-400. A SATISFACTORY LEAK/ OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — DEFECTIVE (ZONE 200 - FUSE) · airframe 38,766 hrs · 15,223 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAILED BITE TEST PER TASK CARD 26L00005005. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY BITE TEST PER AMM 33-51-38.

Part: RELAY — DEFECTIVE (ZONE 100 - FUSE) · airframe 36,870 hrs · 14,414 cycles

AIRCRAFT WAS NOT GROUNDED: DURING FINAL APPROACH, SPOILER 1 / SEC 1 FAULT OCCURRED, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RELAY 41CE1 FOR SEC1 COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK

Part: WIRE HARNESS — MISINSTALLED (R1 DOOR) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL CHECK OF THE MANUAL MASK RELEASE NOT DEPLOYED CONTAINER OXYGEN ON DOOR R1. FOUND ELECTRICAL WIRING OF CONTAINER OXYGEN BOX 40RW INCORRECTLY INSTALLED, WIRING CORRECTLY INSTALLED AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 35-23-07 AND 35-23-00-710-001.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF THE EMERGENCY LIGHTS, POWER SUPPLY UNIT 11WL SHOWS FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT AILERON) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: MIGRATED BEARING HINGE ARM 3 AILERON ON LEFFT WING (1EA). REPLACED HINGE ARM 3 AILERON ON LEFT WING PER CMM 57-51-54-820-804-A01.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA CABIN FLOOR PANEL 261PF DELAMINATED. REPLACED PANEL PER SRM 53-02-00-300-011 AND IRM 9701.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 13WL IN PASSENGER CABIN FAILED. REPLACED POWER SUPPLY PER AMM 33-51-38-000-001.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 221PF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 221PF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,487 hrs · 14,248 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,487 hrs · 14,248 cycles

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

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT WAS GROUNDED: DELAMINATED FLOOR PANEL 251LF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 251LF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 222CF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 222CF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 231FF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 231FF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 221DF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 221DF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 221EF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 221EF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL A321 SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 251FF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 251FF FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011.

Part: PIN — STUCK (LT ENG MOUNT) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ENGINE AFT ENGINE MOUNT CENTER LOWER SOLID PIN STUCK. REPLACED PIN PER AMM 71-22-11-000-010-A AND AMM 71-22-11-200-804-A.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 251TF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 251TF IN FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 51-02-00-300-011 AND IRM 9701 REVISION L.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 251RF FORWARD GALLEY AREA. REPLACED FLOOR PANEL 251RF IN FORWARD GALLEY AREA WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011 AND IRM 9701 REVISION L.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 252QF PASSENGER CABIN. REPLACED FLOOR PANEL 252QF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011 AND IRM 9701 REVISION L.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 252TF PASSENGER CABIN. REPLACED FLOOR PANEL 252TF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011 AND IRM 9701 REVISION L.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 251YF PASSENGER CABIN. REPLACED FLOOR PANEL 251YF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL PER A321 SRM 53-02-00-300-011 AND IRM 9701 REVISION L.

Part: WEB — CRACKED (FRMS 11-12) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON FLOOR STRUCTURE SUPPORT WEB. L= 0.690 INCHES. REPLACED FLOOR STRUCTURE SUPPORT WEB BETWEEN FR11 TO FR12, AND Y765 LEFT SIDE IN PASSENGER CABIN PER SRM 51-42-11-801.

Part: SKIN — CORRODED (FRM 21-22) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND LOWER FUSELAGE INTERNAL SKIN AIR INLET DUCT FLANGE BETWEEN FR 21 AND FR 22. REPLACED FLANGE PER SRM 51-72-11.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR LOWER SURFACE DELAMINATED AT RIB 6 AND 16 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR LOWER SURFACE PER SRM 55-21-11-300-032.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: FLOOR PANEL — CORRODED (AFT GALLEY) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR PANEL 261LG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 36,487 hrs · 14,248 cycles

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

Part: SHEAR PLATE — CRACKED (FRM 69 S23L) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-42-00-801.

Part: SEAT TRACK — CORRODED (FRM 16) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK BEAM AT FR 16 AND +Y1292. REPLACED SEAT TRACK BEAM PER SRM 51-725-11.

Part: CYLINDER — NO TEST (PAX DOOR) · airframe 36,487 hrs · 14,248 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNCTIONAL TEST. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14-400-001.

Part: TRANSFER SYS — FAULT MESSAGE (FUEL SYSEM) · airframe 35,741 hrs · 13,938 cycles

AIRCRAFT WAS NOT GROUNDED: CLIMBING THRU 33,000, GOT FUEL ACT TRANSFER FAULT.1160 IN ACT AT TIME( STARTED W/2520 IN LT. ACT ON GRND).PRESSED ACT TO FWD, FED NORMALLY TO 0. RESELECTED ACT "AUTO". ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE ACT AUTO TRANSFER SYSTEM PER AMMM 28-28-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 35,427 hrs · 13,800 cycles

AIRCRAFT WAS NOT GROUNDED: 2R DOOR SLIDE BOTTLE INDICATION AT TOP OF RED ARK. REPLACED 2R DOOR SLIDE BOTTLE ASSEMBLY PER AMM 25-62-49.

Part: SLIDE — NOT REPORTED (L4 DOOR) · airframe 35,107 hrs · 13,659 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR SLIDE DUE FOR REPLACEMENT. REMOVED SLIDE FROM L4 DOOR. RE-INSTALLED SAME SERVICEABLE L4 DOOR SLIDE, PER JOB CARD 26L00025010. SLIDE FOUND TO BE BAD FROM STOCK.

Part: HINGE FITTING — GOUGED (RT MLG DOOR) · airframe 34,909 hrs · 13,575 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON FORWARD SIDE HAS DEEP GOUGE FROM HEAD OF HINGE BOLT ROTATING. INSTALLED A NON-REINFORCING REPAIR. ACCOMPLISHED FORWARD FACE REPAIR, IAW AIRBUS REPAIR INSTRUCTION R533-70507 ISSUE B.

Part: HINGE FITTING — WORN (LT MLG DOOR) · airframe 34,909 hrs · 13,575 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND LEFT MAIN LANDING GEAR DOOR FORWARD DOOR HINGE BOLT SHOWS EVIDENCE OF ROTATION WITH SLIGHT WEAR ON FORWARD FACE OF FITTING. NON-REINFORCING REPAIR INSTALLED AND ACCOMPLISHED FORWARD FACE REPAIR, IAW AIRBUS REPAIR INSTRUCTION R533-70507 ISSUE B.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 34,449 hrs · 13,375 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT ENTRY WAY FLOOR PANEL 151GF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: TRANSFORMER — FAILED (ZONE 100 - FUSE) · airframe 33,764 hrs · 13,106 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS DURING EMER GEN TEST ESS/TR FAILED AMBER XX 'S AMPS. MAINTENANCE REMOVED AND REPLACED ESS/TR IAW AMM 24-34-51. OPS CHECK NORMAL.

Part: RESERVOIR — LEAKING (R3 DOOR SLIDE) · airframe 32,889 hrs · 12,772 cycles

AIRCRAFT WAS GROUNDED: FA REPORTED MESSAGE; CHECK DOOR 3R SLIDE PRESSURE. R & R R3 DOOR SLIDE INFLATION RESERVOIR IAW AMM 25-62-49. OPS GOOD.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,078 hrs · 12,498 cycles

AIRCRAFT WAS NOT GROUNDED: PASSENGER SEAT ROW 12ABC EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED 12ABC EMERGENCY LIGHT WIRE HARNESS PER AMM 33-51-19 P.B.0401.

Part: LIGHT — UNKNOWN (COCKPIT) · airframe 31,129 hrs · 12,148 cycles

AFTER LANDING, CABIN EMERGENCY LIGHTS CAME ON ARMED POSITION IN COCKPIT. MAINTENANCE ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: KNOB — SHEARED (SELECTOR) · airframe 30,887 hrs · 12,044 cycles

ALTIMETER ISSUE, EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. ON ARRIVAL, FOUND THE SELECTOR KNOB HAD SHEARED AND HAD COME LOOSE. THE AIRCRAFT WAS GROUNDED. REPLACED FCU IAW AMM 22-81-12. PERFORMED SATISFACTORY AFS TEST & LAND CAT 3 CAPABILITY TEST IAW AMM 22-96-00 & AMM 22-97-00.

Part: ACCUMULATOR — FAULTY (BRAKE SYSTEM) · airframe 30,590 hrs · 11,928 cycles

LOSS OF BRAKE PRESSURE WITH APPLICATION OF BRAKES. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED BRAKE ACCUMULATOR IAW AMM 32-44-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM IAW AMM 32-42-00-710-001-A.

Part: LENS — MISSING (L1 DOOR) · airframe 30,307 hrs · 11,816 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR ASSIST BOTTLE VIEWING WINDOW MISSING LENS. RE-ATTACHED DOOR ASSIST VIEWING WINDOW WITH ADHESIVE. OK FOR CONTINUED SERVICE.

Part: DIRECTOR — ERRATIC (CIDS) · airframe 28,969 hrs · 11,323 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD FLIGHT ATTENDANT PANEL FAULTING 2L EMERGENCY EXIT DOOR SLIDE BOTTLE PRESSURE. ACCOMPLISHED RESET OF CIDS NO HISTORY LAST 30 DAYS REMOVED PLACARD REMOVE FROM MIC PER AMM 23-33-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 28,962 hrs · 11,321 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT CAME ON INTERMITTENTLY. MAINTENANCE CLEARED SWITCH AND CHECKED EMERGENCY LIGHT WITH BITE TEST AND PERFORMED OPERATIONAL CHECK PER AMM 33-51-00-710-001.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,597 hrs · 11,187 cycles

THE AIRCRAFT WAS IN BASE MAINTENANCE. INTERGRANULAR CORROSION FOUND ON FUSELAGE SKIN AROUND WASTE TANK VENT TUBE CUTOUT. REPAIRED FUSELAGE SKIN PER SRM 53-41-11-300-004 FIGURE 20108.

Part: DECODER — MALFUNCTIONED (L2 DOOR BOTTLE) · airframe 28,492 hrs · 11,147 cycles

L2 DOOR SLIDE INDICATED LOW PRESSURE. REPLACED THE DECODER 300 RH4 IAW AMM 23-73-47 .

Part: FLOOR PANEL — DAMAGED (ROW 10) · airframe 27,862 hrs · 10,903 cycles

SOFT SPOT IN THE FLOOR PANEL 231AG BY ROW 10. REPLACED THE FLOOR PANEL 231AG IAW AMM 53-32-12.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,874 hrs · 10,515 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT FLASHLIGHT AT DOOR 3 INOPERABLE. MAINTENANCE REPLACED BATTERY AS REQUIRED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,874 hrs · 10,515 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT DOOR 3 INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT AS REQUIRED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: INTAKE DUCT — CONTAMINATED (APU) · airframe 26,472 hrs · 10,361 cycles

EVIDENCE OF OIL IN APU AIR INTAKE AFTER INSPECTION, CAUSING ODOR IN CABIN. CLEANED OIL FROM INTAKE AND PERFORMED INSPECTION IAW AMM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 26,392 hrs · 10,333 cycles

EMERGENCY LIGHTS AT SEATS 22 INOPERATIVE. SECURED THE CONNECTOR AT THE SIDEWALL PANEL. OPS TESTED SERVICEABLE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 26,278 hrs · 10,283 cycles

L1 DOOR DAMPER BOTTLE NEEDS SERVICED. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM.

Part: OIL CAP — LEAKING (APU) · airframe 25,778 hrs · 10,098 cycles

WET SOCK ODOR THROUGH OUT THE AIRCRAFT. HEAVY RAIN ON TAXI OUT FROM DEPARTURE AIRPORT. ODOR STARTED GOING AWAY AT CRUISE. FOUND APU OIL CAP LEAKING, REPLACED OIL CAP IAW CMM 49-27-31.

Part: INLET — CONTAMINATED (APU) · airframe 25,171 hrs · 9,868 cycles

ALL FLIGHT ATTENDANTS REPORTED A STRONG ODOR IN THE CABIN. MAINTENANCE COMPLETED CABIN ODOR JOB CARD 26L00021001. FOUND OIL ON APU INLET AND CLEANED APU BAY AS REQUIRED. ACCOMPLISHED DECONTAMINATION TASK CARD 26L00021004.

Part: WARNING MESSAGE — FALSE ACTIVATION (L1 DOOR) · airframe 25,030 hrs · 9,818 cycles

L1 DOOR SHOWS IT IS OPEN ON ECAM, WHEN IT'S CLOSED. OPENED & CLOSED DOOR TWICE, NO OPEN INDICATIONS. OPS CHECKED GOOD.

Part: AIR DATA MODULE — FAULTY (COCKPIT) · airframe 25,013 hrs · 9,812 cycles

DIVERTED DUE TO A LOSS OF CAPTAIN'S INSTRUMENTS AND WEATHER RADAR. AN EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED AIR DATA UNIT. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,784 hrs · 9,718 cycles

AFT LT DOOR MISSING EXIT SIGN. REPLACED AFT LT DOOR EXIT SIGN COVER.

Part: COOLING FAN — FAILED · airframe 24,773 hrs · 9,714 cycles

AFTER ARRIVING, FLIGHT ATTENDANTS REPORTED FUMES AND AN ODOR IN REAR OF CABIN. APU WAS IMMEDIATELY TURNED OFF AND APU SHUT DOWN. AFTER ALL PASSEMGERS DEPLANED APU WAS RESTARTED AND AIR WAS TURNED ON. MAINTENANCE SUSPECT APU AIR COOLING FAN BAD. MAINTENANCE REPLACED APU AIR COOLING FAN PER AMM 49-52-51. ACCOMPLISHED JOB CARDS 26L00021001 CABIN AIR QUALITY, 26L00021002 APU SMELL IN CABIN, 26L31049009 CLEAN APU LOAD COMPRESSOR, AND 26L00021004 DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 24,706 hrs · 9,685 cycles

SOFT SPOT IN FLOOR PANEL BETWEEN SEATS 2C & 2D. REPLACED CENTER AISLE FLOOR PANEL BETWEEN FRAMES 24 AND 28 IAW AMM 53-22-12. AIRCRAFT WAS GROUNDED.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 24,530 hrs · 9,621 cycles

IN FLIGHT, AT FL 320, MASTER CAUTION RED FOLLOWED BY A LAVATORY SMOKE ECAM MESSAGE, FAS CHECKED ALL LAVATORIES, NO SMOKE OR FIRE FOUND. REPLACED LAVATORY D SMOKE DETECTOR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,407 hrs · 9,578 cycles

SEAT 22D EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 23,793 hrs · 9,345 cycles

EMERGENCY FLASHLIGHT AT THE L4 DOOR, NOT FLASHING. REPLACED BATTERY PACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 23,045 hrs · 9,052 cycles

AFTER ARMING L2 DOOR, CHECK PSI WARNING APPEARED. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW 52-22-00-614-002-A.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 22,098 hrs · 8,716 cycles

FLIGHT CREW RECEIVED AN ECAM MESSAGE: FLIGHT CONTROL PITCH TRIM/MCDU/CG DISAGREE ON TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS. THE FLIGHT CREW ABORTED THE ACFT AND RETURNED TO THE GATE, INFORMED MAINTENACE OF THE ISSUE WHICH WAS NOTED BY MAINTENANCE.

Part: DOOR — DIRTY (L1) · airframe 22,059 hrs · 8,701 cycles

AFTER CLOSING THE L1 DOOR, THE DOOR INDICATED OPEN AND SLIDE ARMED ON DOOR PAGE. CLEANED DEBRIS FROM AROUND DOOR. CYCLED DOOR ARMED AND DISARMED WITH NO DEFECTS NOTED.

Part: CHILLER — FAILED (GALLEY) · airframe 21,878 hrs · 8,643 cycles

ODOR IN AFT GALLEY.MAINTENANCE FOUND AFT CHILLER FAIL LIGHT ILLUMINATED, AND IDENTIFIED ODOR TO FAILED CHILLER MOTOR. REPLACED AFT GALLEY AIR CHILLER PER AMM 25-34-51-000-002-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 21,822 hrs · 8,622 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT LENS COVER MISSING AT SEAT ROW 8L. REPLACED EMERGENCY LIGHT AT SEAT ROW 8L IAW AMM 33-51-19.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 21,717 hrs · 8,586 cycles

AIRCRAFT IN BASE MX. RECEPTACLE MISSING FOR EMER LIGHT PINS THAT CONNECT AT SEAT ROW 22AB. REPLACED CONNECTOR IAW ASM 33-51-04 & FOUND EMER POWER SUPPLY UNIT 12WL FAULTY DURING THE OPERATIONAL CHECK. REPLACED EMER POWER SUPPLY UNIT 12WL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400. SEE AALA201606089005 FOR ADDITIONAL PART.

Part: CONNECTOR — MISSING (CABIN) · airframe 21,717 hrs · 8,586 cycles

AIRCRAFT IN BASE MX. RECEPTACLE MISSING FOR EMER LIGHT PINS THAT CONNECT AT SEAT ROW 22AB. REPLACED CONNECTOR IAW ASM 33-51-04 & FOUND EMER POWER SUPPLY UNIT 12WL FAULTY DURING THE OPERATIONAL CHECK. REPLACED EMER POWER SUPPLY UNIT 12WL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400. SEE AALA201606089012 FOR ADDITIONAL PART.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 19,858 hrs · 7,854 cycles

SY6 CHECK, CABIN FLOOR SHEAR PLATE AT RBL 46 INCHES & FRAME 69 IS CRACKED. R & R SHEAR PLATE IAW 21 51-42-11 & DWG 18D53474180.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

SYS6 CHECK, CORROSION ON L4 DOOR CUT OUT LOWER SILL BEAM AT FRAME 68 & LBL 49. REPAIRED BEAM IAW SRM 53-41-14-201 REPAIR PRINCIPLE 5.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

SY6 CHECK, CABIN FLOOR SHEAR PLATE AT LBL 46 INCHES & FRAME 69 IS CRACKED. R & R SHEAR PLATE IAW SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

SYS6 CHECK, CORROSION ON THE R4 DOOR CUT OUT LOWER SILL BEAM AT FRAME 68, STRINGER 23 & RBL 49.25. REPAIRED BEAM IAW SRM 53-41-14-201 REPAIR PRINCIPLE 5.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

SY3 CHECK, CABIN DOOR SILL AT RBL 49.25 INCHES IS CORRODED, 4.75 INCHES FWD OF FRAME 68. REPAIRED DOOR SILL IAW SRM 53-41-14-201 PRINCIPLE 5.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

CORROSION ON FITTING AT FRAME 68 - 6", STRINGER 23R & RBL 56. REPLACED IAW SRM 51-42-11 & DWG 18D53480019.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,858 hrs · 7,854 cycles

SYS6 CHECK, CORROSION ON BEAM BETWEEN FRAME 66 & 68 AT LBL 29. REPLACED BEAM IAW SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (CABIN)

CENTER OF AISLE ROW 16, FLOOR HAS A SOFT SPOT. REPLACED CTR FLOOR PANEL 241HF IAW AMM 53-32-12.

Part: LENS — CRACKED (CABIN) · airframe 19,646 hrs · 7,773 cycles

MID CABIN CEILING MOUNTED EMER EXIT LIGHT LENS CRACKED. REPLACED LENS IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,848 hrs · 7,467 cycles

EMERGENCY SEAT LIGHT 10 ABC BAD. REPLACED THE SEAT 10 ABC EMER LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 18,848 hrs · 7,467 cycles

EMERGENCY LIGHTS AT SEATS 6 ABC & 12 ABC ARE INOPERATIVE. RECONNECTED THE EMER LIGHTS AT SEATS 6 ABC & 12 ABC.

Part: LENS — MISSING (CABIN) · airframe 17,084 hrs · 6,734 cycles

WHITE AISLE EMER LIGHT AT SEAT 12C LENS MISSING. REPLACED EMER LIGHT AT SEAT 12C. OPERATIONS CHECKED GOOD.

Part: DOOR SILL — DIRTY (FUSELAGE) · airframe 16,929 hrs · 6,664 cycles

R4 DOOR DIFFICULT TO ARM. REMOVED DEBRIS FROM R4 DOOR SILL PLATE. R4 DOOR ARMING OPERATIONS OK.

Part: HINGE BRACKET — EXCESS PLAY (LT ELEVATOR) · airframe 16,725 hrs · 6,581 cycles

RON VISIT LT ELEVATOR NR 2 HINGE BOLT & ASSEMBLY LOOSE AT HORIZONTAL STAB RIB 8. REPLACED IAW AMM 55-16-42-400-001.

Part: HINGE BRACKET — EXCESS PLAY (LT ELEVATOR) · airframe 16,725 hrs · 6,581 cycles

RON VISIT LT ELEVATOR NR 1 HINGE BOLT & ASSEMBLY LOOSE AT HORIZONTAL STAB RIB 5. REPLACED IAW AMM 55-16-42-400-001.

Part: HINGE BRACKET — EXCESS PLAY (LT ELEVATOR) · airframe 16,725 hrs · 6,581 cycles

RON VISIT LT ELEVATOR NR 3 HINGE BOLT & ASSEMBLY LOOSE AT HORIZONTAL STAB RIB 9. REPLACED HINGE BRACKET ASSEMBLY IAW AMM 55-16-42-400-001.

Part: PANEL — LOOSE (CABIN) · airframe 16,548 hrs · 6,517 cycles

EXIT LIGHT PANEL AT L1 DOES NOT STOW PROPERLY. REPOSITIONED EXIT LIGHT PANEL AT L1 DOOR.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 16,382 hrs · 6,445 cycles

L3 SLIDE RESERVOIR PRESS READS LOW. REPLACED L3 SLIDE RESERVOIR IAW AMM 25-62-49-000-001A & 25-62-49-400-001A.

Part: LENS — UNSECURE (CABIN) · airframe 16,366 hrs · 6,438 cycles

COVER FOR EMER EXIT LIGHT AT 4R FALLS OUT. SECURED LENS ON EMER EXIT SIGN AT 4R.

Part: FLOOR PANEL — DEBONDED (CARGO BAY) · airframe 16,342 hrs · 6,430 cycles

RON VISIT DISBOND & DELAMINATION ON FWD CARGO COMPARTMENT FLOOR PANEL AT FRAME 32 & BETWEEN Y200 T0 -Y200. REPLACED FWD CARGO COMPARTMENT FLOOR PANEL 131EF IAW AMM TASK 53-22-14-000-001-A.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 16,339 hrs · 6,429 cycles

RON VISIT DELAMINATION ON FLOOR PANEL 221EF AT FRAME 18, Y900. REPLACED IAW AMM 53-12-12-400-001.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 13,616 hrs · 5,255 cycles

SOFT SPOT ON FLOOR PANEL 221DF BETWEEN FRAMES 16 TO 21, Y=0. REPLACED FLOOR PANEL IAW AMM 53-12-12-400.

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY SMOKE) · airframe 13,357 hrs · 5,146 cycles

AFT LT LAVATORY HAS A BURNING ODOR. ECAM SMOKE ALARM WENT OFF, F/A REPORTED PASSENGER SPRAYED SOMETHING IN AFT LT LAVATORY SHE ALSO STATED THE AFT RT LAVATORY TRIGGERED A WARNING. MX FOUND NO PRESENCE OF ANY ODOR IN LT OR RT AFT LAVATORY. NO DEFECTS NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 13,245 hrs · 5,087 cycles

EXIT LIGHT COVER MISSING FROM R4 DOOR. INSTALLED EXIT LIGHT COVER.

Part: LENS — MISSING (CABIN) · airframe 11,575 hrs · 4,372 cycles

DOOR 4R EMERGENCY LIGHT COVER MISSING. REPLACED DOOR 4R EMERGENCY LIGHT COVER.

Part: CYLINDER — DISCHARGED (L4 DOOR) · airframe 11,079 hrs · 4,154 cycles

C11 CHECK - L-4 DOOR ASSIST CYLINDER LEAKS OUT DURING CHARGING. REPLACED L2 DOOR ASSIST CYLINDER AS PER A321 AMM 52-13-14.

Part: DIAPHRAGM — LEAKING (L4 BOTTLE) · airframe 10,426 hrs · 3,866 cycles

MESSAGE ON CIDS PANEL TO CHECK DOOR 4L PRESSURE. SERVICED DOOR 4L ASSIST BOTTLE. DUE TO REPEATED SERVICINGS, COMPLETED ADDITIONAL TROUBLESHOOTING AND FOUND PERCUSSION DIAPHRAGM LEAKING. REMOVED AND REPLACED DIAPHRAGM-SEALING IAW 52-11-05.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 10,408 hrs · 3,858 cycles

L-4 DOOR ASSIST BOTTLE ON CIDS. CHECKED FOR LEAKS WITH NONE NOTED. SERVICED L-4 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 10,377 hrs · 3,848 cycles

CHECK DOOR PRESSURE AT L4. SERVICED L4 DOOR ASSIST BOTTLE PRESSURE PER AMM 52-00-040-001A.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 10,350 hrs · 3,836 cycles

CHECK PRESSURE LIGHT ON CIDS PANEL DOOR 4L. SERVICED 4L DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001A.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 10,302 hrs · 3,811 cycles

FLIGHT ATTENDANT REPORTED CIDS AMBER CAUTION LIGHT FLASHING FOR 4L DOOR. SERVICED 4L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 9,979 hrs · 3,669 cycles

L4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L4 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-03.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 9,319 hrs · 3,425 cycles

VARIOUS EMERGENCY AND OVERHEAD LIGHTS IN THE CABIN ARE RANDOMLY FLASHING ON INCLUDING 2L, 2R, 3L AND 3R EXIT LIGHTS. ATTEMPTED A CIDS COMPUTER RESET PER QRH - NO HELP. MAINTENANCE PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AIRBUS MAINTENANCE MANUAL 33-51-00-710-001A WITH NO FAULTS FOUND AND NO HISTORY.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 8,887 hrs · 3,269 cycles

DOOR 2R SLIDE PRESSURE SHOWN IN RED. REMOVED AND REPLACED R2 INFLATION RESERVOIR ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 25-62-49.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 8,583 hrs · 3,158 cycles

PLATE ON EMERGENCY EXIT SIGN ON 4L DOOR IS BROKEN. INSTALLED NEW COVER AS REQUIRED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 8,329 hrs · 3,056 cycles

DUAL FMGC FAILURE ON APPROACH INTO CLT. AIRCRAFT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING IAW AIRBUS MAINTENANCE MANUAL 22-96-00-710-001 WITH NO DEFECTS OR FAULTS NOTED AND NO SUBSEQUENT ISSUES TO DATE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 8,103 hrs · 2,964 cycles

THE 4R DOOR EXIT COVER MISSING. INSTALLED 4R DOOR EXIT LENS COVER.

Part: MASK — MISSING (ZONE 200) · airframe 7,434 hrs · 2,698 cycles

SMOKE MASK IS MISSING. MAINTENANCE INSTALLED SMOKED MASK.

Part: RESERVOIR — FAULTY (EVAC SLIDE) · airframe 6,898 hrs · 2,501 cycles

CIDS PANEL CAUTION 'CHECK 2R SLIDE PRESSURE'. GAUGE APPEARS TO BE IN GREEN. REMOVED AND REPLACED R2 SLIDE RESERVOIR ASSEMBLY.

Part: LENS — MISSING (CABIN) · airframe 6,615 hrs · 2,403 cycles

EXIT LIGHT COVER AT 4L DOOR FELL OFF. MAINTENANCE REPLACED EMERGENCY EXIT FLOOR LEVEL LIGHT LENS AT DOOR 4L.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 5,563 hrs · 2,047 cycles

MX - PHL - EES - R-3 SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED R-3 SLIDE BOTTLE IAW AIRBUS MAINTENANCE MANAUL 25-62-49-000-001-01/400-001-0.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 3,585 hrs · 1,374 cycles

FLT 1439 - CLT - EES - CIDS PANEL SHOWS R-1 SLIDE PRESSURE INDICATION - SLIDE PRESSURE CHECKS NORMAL. MAINTENANCE REMOVED AND REPLACED R-1 SLIDE PACK.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 3,177 hrs · 1,223 cycles

FLT 1490 - SEA - EEL - CIDS PANEL SHOWS EXIT SLIDE DOOR 4-L PRESSURE LOW. MAINTENANCE SERVICED 4-L DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW (DOOR ASSIST) · airframe 3,079 hrs · 1,182 cycles

FLT 1630 - LGA - EES - AFT LEFT DOOR ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED AFT LEFT DOOR ACCUMULATOR IAW MAINTENANCE MANUAL 52-10-00.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 3,018 hrs · 1,152 cycles

FLT 938 - CLT - EES - CIDS PANEL SHOWS LOW PRESSURE ON SLIDE/CABIN DOOR 4L. MAINTENANCE SERVICED 4L DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-03.

Part: BOTTLE — LOW PRESSURE (L4 DOOR)

FLT 1546 - PHX - EES- 4L DOOR CHECK DOOR PRESSURE RED FLASHING LIGHT ON CIDS PANEL. MX SERVICED 4L DOOR ASSIST BOTTLE IAW MM 52-10-00.