N835AW

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 58,596 hrs · 29,381 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE PROFORMING J/C 26C00025003 NOTICE MEGAPHONE INOP. MAINTENANCE REPLACED MEGAPHONE IAW AMM 25-65-51.

Part: FAN — ODOR (ZONE 100) · airframe 58,200 hrs · 29,131 cycles

AIRCRAFT WAS GROUNDED: AT GATE WHEN SHUT DOWN NUMBER ONE ENGINE, STRONG FUME SMELL IN FORWARD CABIN HAD BEEN RUNNING #2 PACK FOR 25 MIN. MAINTENANCE REPLACED RECIERCULATION FAN.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 59,657 hrs · 28,786 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU 13WL FAILED BATTERY TEST. REPLACED EPSU 13WL IAW A319 AMM 33-51-38-000-002-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 59,657 hrs · 28,786 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU 11WL FAILED BATTERY TEST. REPLACED EPSU 11WL IAW A319 AMM 33-51-38-000-002-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 57,657 hrs · 28,786 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING EMERGENCY TEST EPSU 13WL BATTERY FAILED. MAINTENANCE REPLACED 13WL EPSU BATTERY IAW A319 AMM 33-51-38-000-002-A, OPS TEST IAW A319 AMM 33-51-00-710-001-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 57,657 hrs · 28,786 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING EMERGENCY TEST EPSU 11WL BATTERY FAILED. MAINTENANCE REPLACED 11WL EPSU BATTERY IAW A319 AMM 33-51-38-000-002-A.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 56,721 hrs · 28,201 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY EMER LIGHT FAILED OPERATIONAL TEST OF EMERGENCY LIGHTING. MAINTENANCE REPLACED EPSU EMER LIGHT BATTERY IN REF TO AMM 33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 56,721 hrs · 28,201 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU UNIT EMERGENCY LIGHT FAILED OPERATIONAL TEST OF EMERGENCY LIGHTING. MAINTENANCE REPLACED EPSU EMER BATTERY IN REF TO AMM 33-51-38.

Part: BRAKE — INTERMITTENT (MLG) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WHEEL — DEFECTIVE (MLG) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TRANSDUCER — DEFECTIVE (MLG BRAKES) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TIRE — FAILED (NR 4) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **SUPPLEMENTLA REPORT WILL BE SUBMITTED** (OPEN)

Part: TACHOMETER — DEFECTIVE (MLG WHEEL) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WHEEL — DEFECTIVE (MLG) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TRANSDUCER — DEFECTIVE (MLG BRAKES) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **ORIGINAL REPORT WAS AALA202403088306** MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SERVO VALVE — DEFECTIVE (MLG BRAKES) · airframe 55,118 hrs · 27,160 cycles

AIRCRAFT WAS GROUNDED: #4 TIRE WAS BLOWN ON LANDING. FLIGHT CREW REPORTED AUTO BRAKES ON LOW, AS WE DECELERATED FELT BRAKE GRAB ON RIGHT SIDE. ECAM MESSAGES BRAKES AUTO BRAKE FAULT BRAKE RELEASES BRAKE SYSTEM 1 FAULT. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT CAME TO A STOP NORMALLY AND WAS TOWED TO THE GATE. **SUPPLEMENTAL REPORT FOR AALA202403088306: MAINTENANCE REPLACED THE FOLLOWING ITEMS: THE RIGHT-HAND MAIN LANDING GEAR BRAKE SERVO VALVE 16GG, THE #3 WHEEL TACHOMETER 20GG (AALA202405017718), BRAKE PRESSURE TRANDUCER 12GG (AALA202405013339), BRAKE PRESSURE TRANSDUCER 13GG (AALA202405016334) THE #3 BRAKE ASSEMBLY (AALA202405016027), THE #3 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405013624) AND THE #4 MAIN LAND GEAR WHEEL / TIRE ASSEMBLY (AALA202405019939). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: FRAME — WORN (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND FALSE FRAME HAS ELONGATED / WORN FASTENER HOLES AT FR 1, BETWEEN Z0 0 AND Z -339. REPAIRED FALSE FRAME PER EA 348650.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMING PER EA 348297 THE RIGHT HAND CONTINUITY FITTING NEEDS TO BE REPLACED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 348297.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

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

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 7.

Part: WINDOW FRAME — NONE (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMING THE LEFT HAND WINDSHIELD FRAME CENTER POST NEEDS TO BE MODIFIED / REPAIRED PER THE MIRROR REPAIR PROCEDURES OUTLINED IN EA 348297 AT FR 2 AND Y0. MAINTENANCE MODIFIED / REPAIRED WINDSHIELD FRAME PER EA 348297.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 348297.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST LOWER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 348297.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER FITTING AT AFT GALLEY AREA LOCATED BETWEEN FR 66 AND FR 68, STR 23R. REPLACED CENTER FITTING PER SRM 51-42-11-801.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

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

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 LEFT AND DOOR STOP 7 INBOARD LOWER FASTENER HOLE H3. REPLACED INTERCOSTAL FITTING SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEAR PLATE IN AFT GALLEY AREA LOCATED BETWEEN FR 69 TO FR 70 AND AT STR 23R. REPLACED SHEAR PLATE PER SRM 51-72-11-911-001.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 54,391 hrs · 26,724 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: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP 7 INBOARD LOWER FASTENER HOLE H3. REPLACED INTERCOSTAL FITTING SRM 51-42-11.

Part: HINGE PIN — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #4 HINGE PIN. REPLACED HINGE PIN PER AMM 27-14-41.

Part: HINGE PIN — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 54,391 hrs · 26,724 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #3 HINGE PIN. REPLACED HINGE PIN PER AMM 27-14-41.

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 53,803 hrs · 26,333 cycles

AIRCRAFT WAS GROUNDED: CAPTAINS SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. MAINTENANCE FOUND THE SLIDING WINDOW WAS HITTING THE WINDOW FRAME WHEN OPENING AND CLOSING WHICH RESULTED IN GROOVE MARKS ON THE WINDOW. MAINTENANCE REPLACED THE SLIDING WINDOW PER AMM 56-12-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — LOOSE (MLG) · airframe 52,494 hrs · 25,573 cycles

AIRCRAFT WAS GOUNDED: DURING GEAR RETRACTION ON TAKEOFF, LANDING GEAR UNLOCK ECAM ILLUMINATED FOR ONE MINUTE. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SENSORS 18GA, 19GA, 24GA, AND 25GA LOOSE. SECURED PROXIMITY SENSORS IAW AMM 32-31-73 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — LOOSE (MLG) · airframe 52,494 hrs · 25,573 cycles

AIRCRAFT WAS GOUNDED: DURING GEAR RETRACTION ON TAKEOFF, LANDING GEAR UNLOCK ECAM ILLUMINATED FOR ONE MINUTE. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SENSORS 18GA , 19GA, 24GA, AND 25GA LOOSE. SECURED PROXIMITY SENSORS IAW AMM 32-31-73 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — LOOSE (MLG) · airframe 52,494 hrs · 25,573 cycles

AIRCRAFT WAS GOUNDED: DURING GEAR RETRACTION ON TAKEOFF, LANDING GEAR UNLOCK ECAM ILLUMINATED FOR ONE MINUTE. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SENSORS 18GA , 19GA, 24GA, AND 25GA LOOSE. SECURED PROXIMITY SENSORS PER AMM 32-31-73 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — LOOSE (MLG) · airframe 52,494 hrs · 25,573 cycles

AIRCRAFT WAS GOUNDED: DURING GEAR RETRACTION ON TAKEOFF, LANDING GEAR UNLOCK ECAM ILLUMINATED FOR ONE MINUTE. MAINTENANCE FOUND NOSE LANDING GEAR PROXIMITY SENSORS 18GA (AALA202301181491), 19GA (AALA202301182194), 24GA (AALA202301186922) AND 25GA (AALA202301183274) LOOSE. RE-SECURED PROXIMITY SENSORS PER AMM 32-31-73 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT EMERGEN EXIT) · airframe 52,303 hrs · 25,464 cycles

AIRCRAFT WAS NOT GROUNDED: CLIMBING THROUGH 19,000 RIGHT OVERWING EXIT ECAM ALERT CAME ON FOR SEVERAL SECONDS. NO OTHER ANNOMOLIES AND EXTINGUISHED. MAINTENANCE PERFORMED TSM 52-21-00-810-807-A WITH NO FAULT NOTED ON ECAM .

Part: WARNING MESSAGE — FALSE ACTIVATION (RT OVERWING EXIT) · airframe 52,303 hrs · 25,464 cycles

AIRCRAFT WAS NOT GROUNDED: CLIMBING THROUGH 19,000 RIGHT OVERWING EXIT ECAM ALERT CAME ON FOR SEVERAL SECONDS. NO OTHER ANNOMOLIES AND EXTINGUISHED. OPEN

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 51,110 hrs · 24,726 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 27C. **SUPPLEMENTAL REPORT FOR AALA202206274836: MAINTENANCE FOUND BROKEN WIRE UNDER SEAT 27ABC AND REPAIRED IT AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS WAS ACCOMPLISHED. ** (CLOSED)

Part: NONE — NONE · airframe 51,110 hrs · 24,726 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 27C. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SWITCH — INOPERATIVE (ZONE 200 - FUSE) · airframe 50,115 hrs · 24,145 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHTS CAME ON WHILE SWITCH WAS IN "ARM" MODE. REPLACED SWITCH 4WL SIGN/EMERGENCY EXIT LIGHT PER TSM 33-51-00-810-881-A.

Part: A/C PACK — CRACKED (ZONE 100 - FUSE) · airframe 49,715 hrs · 23,902 cycles

AIRCRAFT WAS GROUNDED: CLIMBING THROUGH FLIGHT LEVEL 200 FELT A PRESSURE BUMP THEN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR CAME UP SHOWING THE CABIN CLIMBING AT 4100 FEET PER MINUTE. FINALLY SETTLED DOWN TO A 600 FEET PER MINUTE CLIMB - CABIN MADE IT TO 9200 FEET - RETURNED TO FIELD. FLIGHT WAS NOT OVERWEIGHT FOR LANDING. FOUND NUMBER 2 PACK OUTLET BELLOW CRACKED AND BLOWN OUT AT CONDENSER INSTALLED SERVICEABLE CONDENSER (AALA202112134812) AND REPLACED NUMBER 2 PACK OUTLET BELLOW.

Part: CONDENSER — INOPERATIVE (ZONE 100 - FUSE) · airframe 49,715 hrs · 23,902 cycles

AIRCRAFT WAS GROUNDED: CLIMBING THROUGH FLIGHT LEVEL 200 FELT A PRESSURE BUMP THEN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR CAME UP SHOWING THE CABIN CLIMBING AT 4100 FEET PER MINUTE. FINALLY SETTLED DOWN TO A 600 FEET PER MINUTE CLIMB - CABIN MADE IT TO 9200 FEET - RETURNED TO FIELD. FLIGHT WAS NOT OVERWEIGHT FOR LANDING. FOUND NUMBER 2 PACK OUTLET BELLOW CRACKED AND BLOWN OUT AT CONDENSER INSTALLED SERVICEABLE CONDENSER AND REPLACED NUMBER 2 PACK OUTLET (AALA202112139193) BELLOW.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 49,401 hrs · 23,691 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT EMERGENCY POWER SUPPLY UNIT FAILED EMERGENCY LIGHT TEST. REMOVED AND REPLACED LEFT AFT EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: UNKNOWN — VIBRATION · airframe 49,158 hrs · 23,541 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE FL 290 AT 310KTS .80M-FLIGHT ATTENDANTS NOTICED AIRFRAME VIBRATION. ONLY LIGHT IN COCKPIT LESSENED WHEN SLOWED. MODERATE VIBRATION FROM CABIN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: UNKNOWN — VIBRATION (AIR FRAME) · airframe 49,158 hrs · 23,541 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE FL 290 AT 310KTS .80M-FLIGHT ATTENDANTS NOTICED AIR FRAME VIBRATION. ONLY LIGHT IN COCKPIT LESSENED WHEN SLOWED. MODERATE VIBRATION FROM CABIN. MAINTENANCE ACCOMPLISHED FREE PLAY CHECKS ON THE LEFT AND RIGHT ELEVATORS AND THE RUDDER WITH NO FINDINGS NOTED. FOUND LEFT AND RIGHT NOSE LANDING GEAR DOORS TO HAVE PLAY BUT DETERMINED IT WAS WELL WITH IN LIMITS WITH NO MAINTENANCE ACTION REQUIRED. NO ADDITIONAL MAINTENANCE WAS ACCOMPLISHED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — LOOSE (FUEL PUMP) · airframe 48,922 hrs · 23,417 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL CENTER TANK PUMP 1 LOW PRESSURE. **SUPPLEMENTAL REPORT FOR AALA202108168408: MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION OF THE #1 CENTER TANK PUSH BUTTON SWITCH 33QA AND FOUND SWITCH UNSECURED & LOOSE RESULTING IN THE SWITCH BEING REPLACED PER ELECTRICAL STANDARD PRACTICES 2045110101. ALSO REPLACED INHIBIT RELAY 49QA (AALA202108193063) PER ELECTRICAL STANDARD PRACTICES 20-46-50. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 29-21-00-720-001 AS WELL AS TRANSFERRED FUEL TO AND FROM CENTER TANK USING #1 PUMP WITH NO FAULTS NOTED PER AMM 28-21-00-710-001. ** (CLOSED)

Part: RELAY — DEFECTIVE (FUEL PUMP) · airframe 48,922 hrs · 23,417 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL CENTER TANK PUMP 1 LOW PRESSURE. **INITIAL REPORT ALA202108168408** MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION OF THE #1 CENTER TANK PUSH BUTTON SWITCH 33QA AND FOUND SWITCH UNSECURED & LOOSE RESULTING IN THE SWITCH BEING REPLACED PER ELECTRICAL STANDARD PRACTICES 2045110101. ALSO REPLACED INHIBIT RELAY 49QA PER ELECTRICAL STANDARD PRACTICES 20-46-50. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 29-21-00-720-001 AS WELL AS TRANSFERRED FUEL TO AND FROM CENTER TANK USING #1 PUMP WITH NO FAULTS NOTED PER AMM 28-21-00-710-001.

Part: PUMP — FAULTED (FUEL BOOST) · airframe 48,922 hrs · 23,417 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL CENTER TANK PUMP 1 LOW PRESSURE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: PUMP — FAULTED (CENTER FUEL CELL) · airframe 48,918 hrs · 23,414 cycles

AIRCRAFT WAS GROUNDED: FUEL AUTO FEED FAULT ECAM RECEIVED IN FLIGHT. ECAM PROCEDURE REQUIRES FUEL MODE SELECT SWITCH TO MANUAL AND CENTER TANK PUMP 1 ON. FLIGHT DISPATCHED WITH MEL 28-05A - CENTER TANK 1 INOP. COULD NOT COMPLY WITH ECAM AS A RESULT. NOTE: CROSS-FEED WAS REQUIRED TO MAINTAIN WING BALANCE IN FLIGHT. (LEFT WING LOW - RIGHT WING HIGH - FUEL FLOW NORMAL BETWEEN ENGINES) CREW OBSERVED CROSS FLOW BETWEEN WING TANKS - WING TO WING AT APROX 200 LBS EVERY 5 MINS DURING NON CROSS-FEED OPS. CREW OBSERVED IMBALANCE RATE WING TO WING DEVELOP AT APROX 100 LBS EVERY 3 MIN. DURING X FEED OPS, CREW OBSERVED FUEL RETURN TO CENTER TANK. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CENTER TANK PUMP 1 PER AMM 28-21-00. RESET GFCI (69QA) PER TSM 28-21-00-810-817A. AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TSM 28-21-00-810-825A.

Part: CONTROL UNIT — FAULTY (BRAKES) · airframe 47,319 hrs · 22,515 cycles

AIRCRAFT WAS GROUNDED. BRAKES SYSTEM 2 FAULT ON ECAM AFTER TAKEOFF. PERFORMED QRH RESET PROCEDURE AND RECEIVED BRAKES SYSTEM 1 FAULT ON ECAM. FLIGHT AIR INTERRUPTED AND RETURNED TO FIELD. REPLACED BRAKE/STEERING CONTROL UNIT WITH ROBBED UNIT, IAW AMM 32-42-34. OPERATIONS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (E&E BAY) · airframe 46,479 hrs · 22,045 cycles

AIRCRAFT NOT GROUNDED. AVIONICS SMOKE ECAM ON LANDING. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR PER AMM 26-15-15.

Part: RECTIFIER — FAILED (GENERATOR)

AIRCRAFT IN BASE VISIT: EMER GEN TEST FAILED. REMOVED AND REPLACED DC ESSENTIAL TRANSFORMER RECTIFIER (1PE) IAW AMM 24-34-51.

Part: SEAL — LEAKING (APU) · airframe 44,017 hrs · 20,596 cycles

AIRCRAFT AS GROUNDED: PILOT REPORTS SWEET ODOR (LIKE DE-ICE FLUID) DETECTED BY F/A'S AND CABIN. MAINTENANCE ACCOMPLISHED CARD 26L00021001 A320F SMOKE ODOR FUMES INTIAL TROUBLESHOOTING, CARD 26L00021002 A320F APU SMOKE ODOR FUMES TROUBLESHOOTING. MAINTENANCE FOUND THE APU GENERATOR LEAKING AT THE SEAL. REMOVED AND REPLACED APU GENERATOR AND SEAL IAW AMM 24-23-51. ACCOMPLISHED J/C 26L00021004 A320F DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM.

Part: COVER — DETACHED (DOOR HANDLE) · airframe 42,189 hrs · 19,499 cycles

THE DOOR HANDLE COVER DETACHED. INSTALLED HANDLE COVER. OK SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 42,044 hrs · 19,420 cycles

EMERGENCY EXIT LIGHTS WERE ON WITH EXIT LIGHT SWITCH IN ARM POSITION. MAINTENANCE POWERED DOWN AIRCRAFT AND POWERED UP, WAITED FOR POWER-UP AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 24-00-00-710-003-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 41,977 hrs · 19,380 cycles

CREW ABORTED TAKE-OFF AT APPROXIMATELY 85 KNOTS. DUE TO A BRAKE WARNING MESSAGE. RETURNED TO THE GATE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE INSPECTED BRAKES. PERFORMED TASK 05-51-16-200-001A. NO DEFECT NOTED AT THIS TIME.

Part: COMPUTER — FAULTED (RUDDER) · airframe 41,856 hrs · 19,319 cycles

DURING DESCENT, AIRCRAFT MADE THREE UNCOMMANDED RUDDER INPUTS. A FEW MINUTES LATER ECAM MESSAGE FOR AUTO FLIGHT RUD TRIM 1 FAULT. INPUT FELT THROUGH RUDDER PEDALS. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 FLIGHT AUGMENTATION COMPUTER IAW 22-66-34-401. AIRCRAFT PASSES AFS BITE AND AFS LAND BITE PER 22-97-00. AIRCRAFT REMAINS IN CAR3B STATUS. ALSO REPLACED RELAY 7CC1.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN RT ELEVATOR NR 3 HINGE FITTING BEARING. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN RT ELEVATOR NR 5 HINGE FITTING BEARING. THE AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN RT ELEVATOR NR 6 HINGE FITTING BEARING, REPLACED THE NR 6 HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN LT ELEVATOR NR 1 HINGE FITTING BEARING . AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN RT ELEVATOR NR 4 HINGE FITTING BEARING. REPLACED THE HINGE FITTING IAW AMM 55-16-42

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 41,844 hrs · 19,312 cycles

WORN RT ELEVATOR NR 2 HINGE FITTING BEARING. AIRCRAFT WAS GROUNDED. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 41,645 hrs · 19,230 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. ADJUSTED AND FIXED THE AFT FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 41,046 hrs · 18,842 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.

Part: OVEN — FIRE (GALLEY) · airframe 40,316 hrs · 18,406 cycles

OVEN FIRE IN 1ST CLASS GALLEY, FIRE EXTINGUISHED WITHOUT FIRE EXTINGUSHER. REMOVED AND REPLACED THE OVEN. OPS CHECKED. OK FOR SERIVICE.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 39,860 hrs · 18,150 cycles

ILLEGIBLE PLACARD PASSENGER CREW DOOR 8311 "DISARMED" ON EMERGENCY CONTROL HANDLE AT FWD GALLEY AREA. REPLACED PLACARD IAW AMM.

Part: HINGE FITTING — MIGRATED (MLG DOOR) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. MIGRATED MAIN LANDING GEAR DOOR BEARING RIGHT HAND SIDE FORWARD FITTING IN MAIN WHEEL WELL (ACCESS DOOR 744). REPLACED HINGE FITTING ASSEMBLY PER CMM 52-81-18.

Part: HINGE — WORN (NLG DOOR) · airframe 39,860 hrs · 18,150 cycles

EXCESSIVE PLAY ON THE RIGHT NOSE LANDING GEAR AFT DOOR. REPLACED AFT HINGE ON THE DOOR AMM 32-22-13-410-001-A, AMM 32-22-00-220-002-A, AND CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE, DELAMINATION ON FLOOR PANEL 232EF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE BOX BEAM HAS CRACK INDICATION AT FR 43 AND +Y1650. REPAIRED BOX BEAM PER EA 5315Y066.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT STRINGER 23 LEFT. REPLACED SHEAR PLATE PER SRM 51-72-11 AND 51-42-11 AND DRAWING D53474180.

Part: FLOOR PANEL — DELAMINATED (FRAMES 51-54) · airframe 39,860 hrs · 18,150 cycles

DELAMINATION FOUND ON FLOOR PANEL 251GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE, DELAMINATION ON FLOOR PANEL 232XG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE, DELAMINATION ON FLOOR PANEL 211EF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FRAME 24-28) · airframe 39,860 hrs · 18,150 cycles

DELAMINATION FOUND ON FLOOR PANEL 231LF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FRAMES 24-28) · airframe 39,860 hrs · 18,150 cycles

DELAMINATION ON FLOOR PANEL 231KF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE, DELAMINATION ON FLOOR PANEL 212EF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED ON PASSENGER CABIN FLOOR PANEL 251HF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 242LF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 241JF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222CF. REPLACED FLOOR PANEL ASSEMBLY PER AMM 53-12-12-400-001-A.

Part: FLOOR PANEL — DELAMINATED (FRAME 16-20) · airframe 39,860 hrs · 18,150 cycles

DELAMINATION ON FLOOR PANEL 221EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261PF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIG 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261BG. REPLACED FLOOR PANEL PER SRM SRM 53-12-00-300-006 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 221PF. REPLACED FLOOR PANEL PER SRM 53-17-00-300-006 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261AG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 262BG. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 FIG 20106 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261DF. REPLACED FLOOR PANEL PER AMM 53-42-12-400-002-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE, DELAMINATION ON FLOOR PANEL 222EF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXISTING REPAIR ON STRINGER AT FR 27 AND STRINGER 34 LEFT. REPLACED REPAIR PER SRM 53-00-13-300-001.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 151HE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIG 20109 AND IRM 9701 REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND SIDE DOOR LOWER SILL PLATE AT FR 66 AND STRINGER 23 LEFT. REPAIRED DOOR SILL PLATE PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 9.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND SIDE DOOR CUTOUT LOWER SILL AT FR 66 AND -Y1450. REPLACED SILL PER SRM 51-72-11, DWG D534-80505.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND DOOR CUTOUT LOWER SILL AT FR 66 AND STRINGER 23 LEFT. REPAIRED DOOR SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 9.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151TG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152TG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT GALLEY SHEAR PLATE AT STRINGER 23R, BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-72-11 AND DRAWING D53474180.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

CORROSION ON THE AFT GALLEY SEAT TRACK BETWEEN FRAMES 64 AND 66, -Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472816.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON BULK CARGO COMPARTMENT FLOOR PANEL162BF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL151DE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 59-63) · airframe 39,860 hrs · 18,150 cycles

DELAMINATION ON FLOOR PANEL 161CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-11, FIG. 20109.

Part: HINGE FITTING — EXCESS PLAY (NLG DOOR) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE GEAR AFT LEFT HAND DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON BULK CARGO COMPARTMENT FLOOR PANEL 161EF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151GE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 162EF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIG 20109 AND IRM 9701 REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND DOOR CUTOUT LOWER SILL AT FR 68 AND STRINGER 23 LEFT. REPAIRED SILL PER SRM 53-41-14-300-001 AND DRAWING D53480043.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151BE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,860 hrs · 18,150 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151CE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,364 hrs · 17,901 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY LED FLASHLIGHT BY THE L1 DOOR DOES NOT FLASH. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-65-00. OPERATIONAL CHECK GOOD.

Part: SDAC — FAULTED (COCKPIT) · airframe 38,733 hrs · 17,499 cycles

AIRCRAFT WAS NOT GROUNDED. ON TAKE OFF, ADVANCING THRUST LEVERS TO FLEX DENT, MASTER WARNING LIGHT CAME ON AND MESSAGE "CONFIG PARK BRAKE ON" WARNING. PARKING BRAKE HAD BEEN RELEASED AND THERE WAS NO STATUS MESSAGE. REJECTED TAKEOFF AT ABOUT 50 KTS. NOTIFIED TOWER AND RETURNED TO GATE. MAINTENANCE REPLACED SDAC 2 PER AMM 31-55-34. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 38,048 hrs · 17,142 cycles

AIRCRAFT NOT GROUNDED. AFT FWD FACING JUMPSEAT FLASHLIGHT INOPERATIVE .REMOVED AND INSTALLED NEW BATTERY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED

Part: RESERVOIR — WARNING MESSAGE (ZONE 800 - DOORS) · airframe 36,473 hrs · 16,262 cycles

CIDS CAUTION LIGHT ON LEFT OVERWING SLIDE RESERVOIR PRESSURE. AIRCRAFT WAS GROUNDED. REPLACED LEFT OVERWING SLIDE INFLATION RESERVOIR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-62-46.

Part: FAN — MALFUNCTIONED (ZONE 100) · airframe 33,908 hrs · 14,960 cycles

FLIGHT 793 EN-ROUTE, EXTRACT FAULT, SMELLED BURNING SMELL & VIBRATION ON FLOOR. SMELL WENT AWAY AFTER TURNING OFF EXTRACT. SMELL CAME BACK ON DESCENT. R & R EXTRACT FAN IAW AMM 21-26-51-400-001-A. OPERATIONS CHECKED GOOD IAW AMM21-26-00-710-001A.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 32,552 hrs · 14,276 cycles

RIGHT REAR COPILOTS WINDOW DELAMINATED ON FWD EDGE. R & R WINDOW.

Part: DIAPHRAGM — FAULTY (R2 DOOR) · airframe 32,530 hrs · 14,268 cycles

C11 CHECK R2 DOOR ASSIST BOTTLE AT ZERO PRESS. REPLACED DIAPHRAGM IN PERCUSSION MECHANISM OF DOOR DAMPER CYLINDER IAW AMM 52-10-00-610-001-A.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 32,392 hrs · 14,194 cycles

EMERGENCY LIGHTS IN CABIN CAME ON WHILE IN ARM POSITION. CYCLED SEVERAL TIMES & LIGHTS WOULDN'T EXTINGUISH. ALL SYSTEMS CHECKED OK. FOLLOWING OPERATIONAL CHECK IAW AMM 33-51-00-710-004-A.

Part: UNKNOWN — SMOKE (NR 2 EXHAUST) · airframe 31,843 hrs · 13,906 cycles

PASSENGER REPORTED SEEING BLUE SMOKE OUT TAIL CONE OF NR 2 ENG ON LANDING. ACCOMPLISHED ENG RUN IAW AMM 71-00-00. OPERATIONS TESTED OK, NO FAULTS NOTED. NO SMOKE COMING FROM TAIL CONE. OK TO RETURN TO SERVICE.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 31,647 hrs · 13,788 cycles

EMERGENCY VEHICLES CALLED OUT FOR LANDING DUE TO CLASS 1 ECAM HYD GREEN LOW LEVEL DURING CRUISE. TURNED GREEN PUMP ON DURING APPROACH IAW ECAM SYS RECOVERED. REPLACED ENG NR 1 HYD PUMP PRESS SWITCH IAW AMM 29-11-17 PB0401.

Part: FAN — SEIZED (CABIN) · airframe 30,970 hrs · 13,383 cycles

A HEAVY ELEC ODOR IN CABIN & COCKPIT. EVENTUALLY FOUND CABIN FAN FAULT ON COND PAGE. CB W18 RECIRC FAN RT SUPPLY TRIPPED. R & R SEIZED RT CABIN RECIRC FAN. OPERATIONS CHECKED GOOD. NO SMOKE OR SMELL PRESENT IN CABIN. IAW 21-21-51-400-001-A & 21-21-00-710-001-A.

Part: COVER — BROKEN (CABIN) · airframe 30,356 hrs · 13,031 cycles

THE R2 DOOR EMERGENCY EXIT LIGHT COVER IS BROKEN. REPLACED R2 DOOR EMERGENCY LIGHT COVER.

Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 30,073 hrs · 12,901 cycles

THE L1 GUST LOCK NOT LOCKING. CLEANED & LUBED L1 GUST LOCK MECHANISM. OPERATIONS CHECKED GOOD.

Part: O-RING — DAMAGED (APU) · airframe 29,638 hrs · 12,725 cycles

EN ROUTE FROM SJC TO PHX, CREW REPORTED A DIRTY SOCK SMELL COMING FROM ACFT ENVIRONMENTAL SYS. ACCOMPLISHED JOB CARDS 26L00021001, 26L00021002, 26L00021004 & INSPECTED NR 1 & NR 2 ENG NOSE CONES & HOT SECTIONS FOR DAMAGE OR LEAKS. NO DAMAGE OR LEAKS NOTED IAW AMM 72-38-11. FOUND APU INLET DOOR FULL OF OIL, APU DRAIN PLUG WAS LEAKING. WASHED APU INLET DOOR & REMOVED & REPLACED APU DRAIN PLUG O RING. LEAK CHECKED & OPERATIONS CHECKED GOOD IAW AMM 49-90-01. ACCOMPLISHED ECS DECONTAMINATION CARDS, OK FOR SERVICE.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 29,523 hrs · 12,679 cycles

MAINTENANCE REPORTED A SMOKE DETECTOR FAULT ON ECAM. R & R LAVATORY D SMOKE DETECTOR IAW 26-17-15. NO FAULTS NOTED ON GND AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,433 hrs · 12,644 cycles

AFTER LIFTOFF & ONCE AT CRUISE DURING MOMENTARY TURBULENCE. CREW REPORTED A STRONG ODOR IN CABIN, ODOR DISSIPATED QUICKLY. FLIGHT CONTINUED & LANDED WITHOUT INCIDENT AT DESTINATION AIRPORT PHL. ACCOMPLISHED JOB CARDS 26L00021001, 26L00021003 & 26L00021004. NO CABIN ODOR PRESENT AT THIS TIME.

Part: COMPUTER — FAULTY (TE FLAPS) · airframe 28,687 hrs · 12,322 cycles

CREW RECEIVED A FLT CONTROL FLAP SYS 1 FAULT DURING CRUISE. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R SFCC 1. CHECKED GOOD IAW AMM 27-51-34. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 28,660 hrs · 12,305 cycles

FLASHLIGHT UNDER FWD RT F/A JUMPSEAT INOPERATIVE. REPLACED FLASHLIGHT AT FWD RT F/A JUMPSEAT.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 28,415 hrs · 12,184 cycles

AFTER TAKEOFF, CREW REPORTED A STRONG ACRID ODOR IN COCKPIT AND CABIN, BURNING CHEMICAL ODOR BURNED EYES. ODOR WAS INTERMITTENT DURING DESCENT, 15,000 FT TO GROUND. ODOR WAS STRONGER IN COCKPIT THAN CABIN. RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AVEC EXTRACT AND BLOWER FANS AND ASSOCIATED DUCTING. NO SIGNS OF CONTAMINATION OR IRREGULARITIES. CHECKED CONDITION OF BOTH CABIN AIR RECIRCULATION FANS 15HG AND 14HG. FANS IN GOOD CONDITION. NO SIGNS OF ELECTRICAL ODOR. REPLACED BOTH FANS AS PRECAUTION. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,412 hrs · 12,182 cycles

ENROUTE, CREW REPORTED A RANCID ODOR AT TOP OF DECENT. BOTH PILOTS NOTICED SORE THROATS. F/A REPORTED FOWL ODOR, NOT LAVATORY. FLIGHT LANDED WITHOUT INCIDENT. MX WAS UNABLE TO DUPLICATE ODOR ON GROUND IAW ODOR TROUBLESHOOTING, ENGINE 1 AND 2. PERFORMED ENGINE RUNS TO TROUBLESHOOT CABIN ODOR. NO RANCID FOWL ODOR NOTED ON ENGINE 1 BLEED, ENGINE 2 BLEED OR APU. INSPECTED APU OIL LEVEL AND INSPECTED APU FOR FUEL/OIL LEAKS. NO LEAKS NOTED. ACCOMPLISHED COMPRESSOR WASH ON ENGINE 1 AND 2 IAW JC 26L00072012. ACCOMPLISHED SATISFACTORY TEST FLIGHT.

Part: APU — ODOR (APU BAY) · airframe 28,361 hrs · 12,156 cycles

DURING TAKE OFF AND CLIMB IN MODERATE RAIN, APU AND BLEED ON, AFTER THRUST REDUCTION AND BLEED RECONFIGURATION, A STRONG DIRTY SOCKS ODOR WAS REPORTED BY F/A IN CABIN AND COCKPIT. MX COMPLIED WITH TROUBLESHOOTING AND DETERMINED APU TO BE SOURCE OF ODOR. REPLACED APU IAW J/C 26L31049005. FUNCTIONAL CHECK NORMAL. FOUND RUBBER BOOT TO SURGE VALVE BLOWN OUT. R & R BOOT. LEAK CHECKED GOOD. COMPLIED WITH DECONTAMINATION OF ESC IAW J/C 26L00021002 AND 26L00021004.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 28,043 hrs · 12,017 cycles

CREW REPORTED THE EMERGENCY EXIT COVER BELOW 1ST F/A SEAT BROKEN. MX R & R EXIT COVER AT F/A SEAT.

Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 27,455 hrs · 11,753 cycles

CREW REPORTED LAVATORY E SMOKE DETECTOR ALARMING - FILTER CLOGGED. MAINTENANCE REMOVED FILTER, CLEANED FILTER AND REINSTALLED FILTER. OPS CHECK IAW AMM 26-17-00-4710-001. CHECKS GOOD.

Part: HOUSING — LEAKING (APU) · airframe 27,032 hrs · 11,551 cycles

FLIGHT ATTENDANT REPORTED A STRONG DIRTY SOCK SMELL ON TAKEOFF (SHORT TIME) AND DESCENT THROUGH LANDING AND TAXI-IN. APU OFF. MAINTENANCE FOUND AN APU OIL LEAK AT THE CHIP DETECTOR HOUSING. RESEALED CHIP DETECTOR HOUSING AND SERVICED OIL AS REQUIRED PER 49-90-00-600-002-A. ALSO, DURING DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM, FOUND NR 1 ENGINE LEAKING OIL OUT OF DRAIN MAST, STARTER PORT AT 90 PLUS DROPS PER MINUTE. REMOVED AND REPLACED STARTER DRIVE SEAL ASSEMBLY (GARLOCK SEAL) PAR AMM 72-60-22. LEAK CHECK GOOD.

Part: COVER — MISSING (CABIN) · airframe 26,696 hrs · 11,387 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS COVER MISSING AT SEAT 6C. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT LENS COVER AT SEAT 6C. OPS CHECK NORMAL PER AMM 33-51-00.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 26,567 hrs · 11,327 cycles

FLIGHT ATTENDENT'S AND PASSENGERS REPORT A DIRTY SOCK SMELL AND TOILET SMELL (AFT RIGHT LAV FLOOR FLOODED AND LEAK SUSPECTED). MAINTENANCE COMPLIED WITH TROUBLESHOOTING CARD 26L00021001, 26L00021002 AND 26L00021004. FOUND GLYCOL INGESTION IN APU AND PACKS. ACCOMPLISHED BURNOUT CARD AND CLEANED APU PER 49-16-00. CLEANED AFT RIGHT LAV, REMOVED TOILET SHROUD AND FLUSHED TOILET SEVERAL TIMES. LOOKED AT LINES UNDER SINK. ALL LINES DRY. NO LEAKS NOTED. OK FOR SERVICE PER AMM 38-31-00.

Part: PACKING — LEAKING (APU) · airframe 26,330 hrs · 11,223 cycles

CREW REPORTED A CABIN ODOR. MAINTENANCE FOUND EVIDENCE OF OIL LEAK ON APU TURBINE NR 4 CAVITY VENT TUBES. REMOVED AND REPLACED PACKINGS ON APU TURBINE NR 4 CAVITY VENT TUBES. COMPLIED WITH DECONTAMINATION J/C'S 26L00021004 AND 26L00021002I, APU COMPRESSOR WASH J/C 26L31049009 AND APU WASH J/C 26C31049016.

Part: VALVE — FAULTY (LT ENGINE) · airframe 26,003 hrs · 11,090 cycles

DURING TAXI OUT, MAINTENANCE REPORTED A STRONG FUEL ODOR NOTED IN THE AFT HALF OF CABIN AFTER ENGINE START. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FUEL DISTRIBUTION VALVE PER AIRBUS AMM 73-13-43-0401-13. LEAK CHECK GOOD. OPS CHECK GOOD. NO ODOR IN CABIN. ALSO, ACCOMPLISHED J/C 26L00021001, 26L00021003 AND 26L00021004. NO ODORS NOTED IN CABIN.

Part: BELLCRANK — OUT OF ADJUST (L1 DOOR) · airframe 26,001 hrs · 11,089 cycles

MAINTENANCE REPORTED THE L1 AND R1 DOOR PERCUSSION STRIKER KNURLED KNOB IS NOT SEATED. MAINTENANCE ADJUSTED PERCUSSION BELLCRANK FINGER OF THE EMERGENCY OPERATING CYLINDER OF THE FORWARD PASSENGER CREW DOORS LI AND R1 PER AMM 52-11-14-820-02A AND 52-11-14-200-001-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,997 hrs · 11,088 cycles

UPON TAXI OUT, CREW REPORTED A PASSENGER HEARD A RYTHMIC THUMPING SOUND (OVERWING PASSENGER) AND SMELLED A BURNING RUBBER ODOR. UPON TAXI BACK, ODOR BECAME STRONGER. AFTER SHUTTING DOWN RIGHT ENGINE, (WITH APU BLEED AND APU ON), A VERY STRONG ODOR OF JET FUEL PERMEATED THE CABIN. ODOR WAS STRONG ENOUGH TO CAUSE EYE IRRITATION. MAINTENANCE TAXIED AIRCRAFT. NO NOISE OR THUMPING SOUNDS NOTED (OTHER THAN PTU CLACKING). COMPLIED WITH J/C 26L00021001. APU NOT LEAKING OR OVERSERVICED. RAN PACKS WITH INDIVIDUAL AIR SOURCES. NO ODORS NOTED AT ANY TIME DURING ENTIRE TROUBLESHOOTING. REMOVED AND REPLACED CABIN HEPA FILTERS PER AMM 21-21-41-400-001. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: LINKAGE — LACK OF LUBE (L1 DOOR) · airframe 25,943 hrs · 11,058 cycles

CREW REPORTED THE GUST LOCK ON L1 DOOR NOT ENGAGING WITH DOOR OPEN. MAINTENANCE LUBRICATED L1 DOOR GUST LOCK LINKAGE AND LATCH ASSEMBLY. OPS CHECK GOOD.

Part: OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 25,707 hrs · 10,953 cycles

ONE HOUR OUT OF DTW, ECAM - FUEL IMBALANCE INDICATION. FLIGHT ATTENDANT CONFIRMED VAPOR STREAMING OFF OF LEFT ENGINE PYLON. DIVERTED TO OMA. REMOVED AND REPLACED NR 1 ENGINE FCOC (FUEL OIL COOLER) IAW AMM 79-21-43. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 24,099 hrs · 10,212 cycles

LAST SEAT 22C LEFT SIDE EMERGENCY LIGHT IS BROKEN DUE TO CATERING PASSING THRU AISLE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECKED GOOD.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON LEFT ELEVATOR HINGE FITTING NR 2 BETWEEN STAB STA 82 TO STAB STA 181 & BETWEEN RIB 3 TO RIB 5. REPLACED ELEVATOR HINGE FITTING NR 2 IAW A319 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON LEFT ELEVATOR HINGE FITTING NR 1 BETWEEN STAB STA 0 TO STAB STA 69 & BETWEEN RIB 1 TO RIB 2. REPLACED ELEVATOR HINGE FITTING NR 1 IAW A319 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON LEFT ELEVATOR HINGE FITTING NR 6 BETWEEN STAB STA 527 TO STAB STA 601 & BETWEEN RIB 12 TO RIB 14. REPLACED ELEVATOR HINGE FITTING NR 6 IAW A319 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 1 AT VERTICAL STAB STA 78 & AT RIB 2. REPLACED RUDDER HINGE FITTING NR 1 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4 AT VERTICAL STAB STA 263 & AT RIB 6. REPLACED RUDDER HINGE FITTING NR 4 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 5 AT VERTICAL STAB STA 299 & AT RIB 7. REPLACED RUDDER HINGE FITTING NR 5 IAW A319 AMM 55-36-41.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 151PE BETWEEN FR51 TO FR53 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151PE IAW A319 SRM 53-02-00 FIG 209, IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46, -Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR46, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57130147.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,125 hrs · 9,774 cycles

1S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 22,685 hrs · 9,572 cycles

EMERGENCY LIGHTS INOPERATIVE 16L. SWAPPED WIRES ON LIGHT ASSY. SYSTEM OPS CHECKED GOOD. REF AMM 33-51-19.

Part: TRANSMITTER — INOPERATIVE (OIL SYSTEM) · airframe 21,987 hrs · 9,255 cycles

TWENTY MINUTES AFTER TAKEOFF, NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO. REMOVED AND REPLACED NR 1 ENGINE OIL QUANTITY TRANSMITTER PER AIRBUS MAITNENANCE MANUAL 79-31-15PB 401.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - DELAMINATION ON FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO -Y254 IAW MCGILL IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR12 TO FR16. REPLACED FLOOR PANEL 222CF BETWEEN FR12 TO FR16 IAW MCGILL IRM 9701 REV G.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT PASSENGER DOOR SILL BETWEEN FR66 TO FR68, Y1292. REPLACED LEFT AFT PASSENGER DOOR SILL BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, S23L, Y1292. REPLACED FLOORBEAM AT FR68, S23L, Y1292 IAW A319 SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1292. REPLACED FLOORBEAM AT FR68, -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,618 hrs · 8,672 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,194 hrs · 8,480 cycles

FLT 524 - PHX EMERGENCY LIGHTS - AFT EMERGENCY FLASHLIGHT IS NOT BLINKING. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 19,401 hrs · 8,118 cycles

FLT 506 - BOS-PHX - EMERGENCY LIGHT - FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT TRICKLE CHARGE INDICATOR NOT SHOWING PROPER CHARGE INDICATION. REMOVED AND REPLACED EMERGENCY FLASHLIGHT UNDER FORWARD INBOARD FLIGHT ATTENDANT JUMPSEAT. OPERATIONAL CHECK WAS GOOD.

Part: APU — LEAKING (APU BAY) · airframe 17,251 hrs · 7,183 cycles

FLT 210 - SMF-PHX - ODOR - WITH APU BLEED ON AND BOTH PACKS ON, AIRCRAFT SMELLS OF DIRTY SOCK SMELL. SMELL COMING FROM THE APU. REMOVED AND REPLACED APU PER CARD R6D49301. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 14,872 hrs · 6,058 cycles

FLT 493 - PHX-DEN - EMERGENCY LIGHTS - EMERGENCY LIGHT AT 4C OUT. FOUND EMERGENCY LIGHT OF SEAT 4C POPPED OUT OF ITS MOUNT. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: OVEN — ODOR (GALLEY) · airframe 14,282 hrs · 5,796 cycles

FLT 367 - BOS-PHX - BURNING SMELL - FLIGHT ATTENDANT REPORTS HOT ELECTRICAL SMELL FROM NR 1 OVEN FORWARD GALLEY WHEN IN USE. REMOVED AND REPLACED OVEN INSERT AND FORWARD GALLEY OVEN NR 1.

Part: SKIN — CRACKED (ZONE 100) · airframe 11,414 hrs · 4,643 cycles

SAL - MAJOR REPAIR - BC2 CHECK - CRACKED FUSELAGE SKIN, BS 3117 / FR 73, S22L - S23L. REPAIRED FUSELAGE SKIN, BS 3117 / FR 73, S22L - S23L IAW EA 120733.