N285AY

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,917 hrs · 6,149 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS WHILE ACCOMPLISHING JOB CARD 33C20033002 FOUND BATT FAULT FOR 17WL EPSU. REPLACED 17WL EPSU BATT IAW AMM 33-51-38-401.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 40,917 hrs · 6,149 cycles

AIRCRAFT WAS GROUNDED: R1 DOOR ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE PER TASK CARD 33C80052002.

Part: WATER HEATER — FAILED (LAVATORY) · airframe 40,129 hrs · 5,997 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS SMOKE. LAV SMOKE AURAL ALERT ALERTED " TURNED OFF WATER HEATER AND DISCONNNECTED CANNON PLUG" SMELL WAS COMING FROM LOWER VANITY. MAINTENANCE REMOVED AND REPLACED LAV L62 WATER HEATER IAW AMM 38-12-000-801B. OPS CHECKS GOOD.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 39,879 hrs · 5,964 cycles

AIRCRAFT WAS GROUNDED: FLIGHT AIR RETURNED TO CLT ON ACCOUNT OF RIGHT HAND ENGINE BLEED AIR PROBLEM. AFTER T/O #2 IP BLEED VALVE STAYED CLOSE WHICH RESULTED IN A SINGLE PACK OPERATION. EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED HP VALVE ON #2 ENGING IAW AMM 36-11-51. OPS CHECK GOOD.

Part: FLOW VALVE — FAILED (BLEED AIR SYS) · airframe 28,744 hrs · 5,819 cycles

AIRCRAFT WAS GROUNDED: PILOT DIVERTED TO LHR ON ACCOUNT OF DUAL BLEED FAILURE, RESET ATTEMPTS FAILED FOR ENGINE 2, SUCESSFUL FOR ENGINE 1. EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED ENGINE 1 FAN AIR VALVE IAW AMM 36-11-54-400-804-A. OPS CHECK GOOD. IN ADDITION, FAN AIR VALVE CONTROL THERMOSTAT REPLACED IAW AMM TASK 36-11-43-400-804-A. MAINTENANCE REPLACED ENGINE #2 PRSOV IAW AMM TASK 36-11-52-400-804-A. OPS CHECKED SATISFACTORY, LEAK TEST OF THE BLEED VALVE WITH ENGINE IN OPERATION C/O IAW AMM 36-11-52-790-807-A. ECAM MSG CLEARED @ ENG #2 BLEED OPS CHECKED NORMAL. (SEE SDR # AALA201907059027)

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 28,744 hrs · 5,819 cycles

AIRCRAFT WAS GROUNDED: PILOT DIVERTED TO LHR ON ACCOUNT OF DUAL BLEED FAILURE, RESET ATTEMPTS FAILED FOR ENGINE 2, SUCESSFUL FOR ENGINE 1. EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED ENGINE 1 FAN AIR VALVE IAW AMM 36-11-54-400-804-A. OPS CHECK GOOD. IN ADDITION, FAN AIR VALVE CONTROL THERMOSTAT REPLACED IAW AMM TASK 36-11-43-400-804-A. MAINTENANCE REPLACED ENGINE #2 PRSOV IAW AMM TASK 36-11-52-400-804-A. OPS CHECKED SATISFACTORY, LEAK TEST OF THE BLEED VALVE WITH ENGINE IN OPERATION IAW AMM 36-11-52-790-807-A. ECAM MSG CLEARED @ ENG #2 BLEED OPS CHECKED NORMAL. (SEE SDR # AALA201907039016)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,708 hrs · 5,814 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ABOVE SEAT 4H INOPERABLE. MAINTENANCE REPLACED EMERGENCY LIGHT PER AMM 33-50-00.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 38,622 hrs · 5,802 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF ELECTRIC FIRE /SMOKE MID GALLEY BEHIND EXPRESSO MAKER NR 1 & 2. MAINTENANCE FOUND NR 2 EXPRESSO MAKER FAULTY, AS PRECAUTIONNARY REMOVED BOTH EXPRESSO MAKERS 1 & 2 IN MID GALLEY POSITION 4-11 , 4-12 IAW EA 295462.

Part: FLOOR PANEL — DELAMINATED (MID GALLEY) · airframe 37,360 hrs · 5,601 cycles

MID GALLEY FLOOR PANEL 242QF WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW EA 290350.

Part: CYLINDER — LOW PRESSURE (L4 DOOR ASSIST) · airframe 36,912 hrs · 5,511 cycles

L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER GAUGE TOUCHING YELLOW. SERVICED THE L4 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-600-802A.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,411 hrs · 5,421 cycles

EMERGENCY POWER SUPPLY BATTERY 13WL FAILED A CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51-38, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 36,247 hrs · 5,396 cycles

L4 DOOR EMERGENCY DOOR ASSIST CYLINDER PRESSURE WAS LOW. THE CYLINDER WAS SERVICED IAW AMM 52-10-00-600-802A. NO LEAKS EVIDENT.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 35,557 hrs · 5,295 cycles

L4 DOOR ASSIST BOTTLE IN YELLOW BAND. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 34,691 hrs · 5,175 cycles

AIRCRAFT WAS NOT GROUNDED. 4L DOOR ASSIST PRESSURE BOTTLE LOW. SERVICED 4L DOOR PER AMM 52-10-00. LEAK CHECKS GOOD.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 33,935 hrs · 5,071 cycles

L4 DOOR ASSIST BOTTLE IN THE YELLOW BAND. SERVICED DOOR ASSIST BOTTLE AS REQUIRED IAW AMM 52-10-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,845 hrs · 5,059 cycles

EMERGENCY LIGHT LENS WAS MISSING. REPLACED THE LENS IAW 33-50-00.

Part: CONTROL UNIT — FAULTY (R3 DOOR) · airframe 33,414 hrs · 4,987 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN DOOR 3R WOULD NOT DISARM. MAINTENANCE REPLACED ICE PROTECTION CONTROL UNIT (16DS) PER AMM 25-27-35-400-801A, NO FAULTS FOUND, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,351 hrs · 4,979 cycles

EMERGENCY LIGHT ON L53 WALL, CLEAR LENS IS MISSING. INSTALLED THE LENS.

Part: SIGN — BROKEN (CABIN) · airframe 33,254 hrs · 4,958 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN R3 FELL OFF. CLIPS BROKEN OFF. REPLACED EXIT SIGN AT DOOR R3.

Part: SIGN — BROKEN (CABIN) · airframe 33,254 hrs · 4,958 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN R3 FELL OFF. CLIPS BROKEN OFF. REPLACED EXIT SIGN AT DOOR R3.

Part: OVEN — ODOR (GALLEY) · airframe 32,588 hrs · 4,840 cycles

EMERGENCY DECLARED, DIVERTED DUE TO ELECTRICAL ODOR IN AFT GALLEY. OVEN OVERTEMPERATURE ACCOMPANIED BY SMOKE/FUMES (ACRID SMELL) WITH ELECTRICAL SMELL 6-11. OVER TIME, SMELL WENT AWAY. AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE PERFORMED OVERWEIGHT LANDING INSPECTION AS REQUIRED. AIRCRAFT RETURNED TO PHL AND REMOVED FROM SERVICE FOR REPAIRS. ACCOMPLISHED CABIN AIR TROUBLESHOOTING CARD TO VERIFY WORK PERFORMED IN BGR. ISOLATED ODOR TO AFT GALLEY OVEN. MAINTENANCE REPLACED AFT GALLEY OVEN PER AMM 25-35-19 AND ACCOMPLISHED CABIN AIR QUALITY JOB CARD 33L00021001 TO VERIFY OVEN AS THE CAUSE OF SMOKE/FUMES IN CABIN. NO FURTHER ACTION REQUIRED. AIRCRAFT WAS GROUNDED.

Part: ACTUATOR — MALFUNCTIONED (L3 DOOR) · airframe 32,508 hrs · 4,825 cycles

AIRCRAFT WAS GROUNDED. DOOR L3 DAMPER DUE DAMPING EFFECT DOES NOT OCCUR IN PASSENGER CABIN (1 EA). REPLACED L3 DOOR DAMPER.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 32,207 hrs · 4,779 cycles

R1 DOOREMERGENCY LIGHT LENS, FALLS OFF (KNEE LEVEL LIGHT). REPLACED EMERGENCY LIGHT LENS IAW 33-50-00.

Part: METER — MALFUNCTIONED (FUEL) · airframe 32,047 hrs · 4,755 cycles

AFTER TAKEOFF, RECEIVED A NR 1 ENGINE CONTROL 1 SYS FAULT. RETURNED TO FIELD. REPLACED FUEL METER. AIRCRAFT WAS GROUNDED.

Part: ACTUATOR — UNKNOWN (VSV) · airframe 32,047 hrs · 4,755 cycles

AFTER TAK OFF RECEIVED A NR 1 ENGINE CONTROL 1 SYS FAULT. RETURNED TO FIELD. REPLACED THE VARIABLE STATER VANE ACTUATOR. AIRCRAFT WAS GROUNDED.

Part: BATTERY — FAILED (EMERGENCY LIGHTS)

EMERGENCY POWER SUPPLY UNIT 17WL BATTERY FAILED. REMOVED AND REPLACED THE BATTERY IAW AMM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 31,966 hrs · 4,743 cycles

L4 DOOR FORWARD FACING FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 31,703 hrs · 4,707 cycles

EMERGENCY LIGHT OUTSIDE OF THE L38 LAVATORY FOUND BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 31,159 hrs · 4,632 cycles

L4 FLASHLIGHT LED DOES NOT FLASH. REPLACED FLASHLIGHT BATTERY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 30,983 hrs · 4,600 cycles

EMERGENCY FLASHLIGHT AT THE R3 DOOR INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: FUEL FILTER — CLOGGED (NR 1 ENGINE) · airframe 30,029 hrs · 4,473 cycles

AIRCRAFT WAS GROUNDED. FLIGHT RETURNED TO PHL ACCOUNT DUEL FUEL FILTER CLOG INDICATION. CREW DECLARED EMERGENCY AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED ENGINE 1 FUEL FILTER. ALSO SEE AALA201705039011, AALA201705039012 & AALA201705039013.

Part: PRESSURE SWITCH — UNSERVICEABLE (NR 1 ENGINE) · airframe 30,029 hrs · 4,473 cycles

AIRCRAFT WAS GROUNDED. FLIGHT RETURNED TO PHL ACCOUNT DUEL FUEL FILTER CLOG INDICATION. CREW DECLARED EMERGENCY AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED ENGINE 1 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. ALSO SEE AALA201705039012, AALA201705039013 & AALA201705039014.

Part: FUEL FILTER — CLOGGED (NR 2 ENGINE) · airframe 30,029 hrs · 4,473 cycles

AIRCRAFT WAS GROUNDED. FLIGHT RETURNED TO PHL ACCOUNT DUEL FUEL FILTER CLOG INDICATION. CREW DECLARED EMERGENCY AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED ENGINE 2 FUEL FILTER. ALSO SEE AALA201705039011, AALA201705039013 & AALA201705039014.

Part: PRESSURE SWITCH — UNSERVICEABLE (NR 2 ENGINE) · airframe 30,029 hrs · 4,473 cycles

AIRCRAFT WAS GROUNDED. FLIGHT RETURNED TO PHL ACCOUNT DUEL FUEL FILTER CLOG INDICATION. CREW DECLARED EMERGENCY AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED ENGINE 2 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. ALSO SEE AALA201705039011, AALA201705039012 & AALA201705039014.

Part: SLIDE — FAULTED (R3 DOOR) · airframe 29,753 hrs · 4,408 cycles

DURING AN EMERGENCY LIGHT BATTERY CAPACITY CHECK, CIDS 1 FAULT ESCAPE SLIDE LIGHT EPSU AT THE R3 DOOR. REPLACED THE SLIDE. AIRCRAFT WAS GROUNDED.

Part: APU — ODOR (ZONE 100) · airframe 29,543 hrs · 4,349 cycles

AIRCRAFT WAS GROUNDED. AT MCO, FLIGHT ATTENDANTS REPORTED CABIN ODOR ON DESCENT PASSING THROUGH 8,000 FEET. MAINTENANCE FOUND STRONG CABIN ODOR WITH ENGINE BLEED OFF APU ON. SOURCE OF ODOR ISOLATED TO APU ON FERRY FLIGHT FROM MCO TO CLT. MAINTENANCE REPLACED APU PER JOB CARD 33L31549001.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 29,372 hrs · 4,310 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR ASSIST BOTTLE LOW. SERVICED L4 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — LOOSE (EMERGENCY LIGHT)

EMERGENCY EXIT SIGN OVER L3 DOOR CAME LOOSE. REINSTALLED THE LENS.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 28,502 hrs · 4,126 cycles

LAVATORY SMOKE ECAM. FLIGHT ATTENBDANT IDENTIFIED LAVATORY L62. ECAM SELF EXTINGUISHED AFTER 15 SEC. MAINTENANCE ACCOMPLISHED TSM 26-17-00-810-812A. NO FAULTS FOUND AND NO SMOKE REPORTED.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 28,408 hrs · 4,114 cycles

WHILE PERFORMING A-17 CHECK TASK CARD 33C22033002, FOUND EMERGENCY POWER SUPPLY 14WL BATTERY BAD AT THE 2R DOOR. REPLACED BATTERY.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 28,408 hrs · 4,114 cycles

WHILE PERFORMING A-17 CHECK TASK CARD 33C22033002, FOUND EMERGENCY POWER SUPPLY 15WL BATTERY BAD AT THE 3L DOOR. REPLACED THE BATTERY.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 28,401 hrs · 4,113 cycles

PLASTIC EXIT COVER CAME OFF THE 3L DOOR. REINSTALLED 3L DOOR EXIT COVER.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,682 hrs · 4,014 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING A-16 CHECK, TASK CARD 33C20033002, FOUND EMERGENCY POWER SUPPLY UNIT 16WL BATTERY INOPERATIVE. REPLACED 16WL BATTERY AND ACCOMPLISHED A SATISFACTORY. OPS CHECK IAW AMM 33-51-38-80-802-A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,682 hrs · 4,014 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING A-16 CHECK, TASK CARD 33C20033002, FOUND EMERGENCY POWER SUPPLY UNIT 18WL BATTERY INOPERATIVE. REPLACED 18WL BATTERY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-38-80-802-A.

Part: COVER — MISSING (EXIT SIGN) · airframe 26,636 hrs · 3,861 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN COVER MISSING AT SEAT 23B. INSTALLED EXIT SIGN COVER AT SEAT 23B.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 26,456 hrs · 3,837 cycles

AIRCRAFT WAS NOT GNDED. DURING DAILY CHECK FOUND EMER LIGHT MID GALLEY 2R AISLE INOPERATIVE. FOUND CONNECTOR ABOVE IFE CTR OFF & BAGGED. RE-INSTALLED CONNECTOR ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: MONITOR — DEFECTIVE (CABIN) · airframe 25,756 hrs · 3,693 cycles

AIRCRAFT WAS NOT GNDED. MONITOR AT SEAT 7C HAD ELEC SMELL & VISIBLE SMOKE. IT WAS SHUT DOWN WITH NO ADDITIONAL PROBLEMS. REPLACED SEAT MONITOR ASSEMBLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 23-32-08.

Part: SIGN — LOOSE (CABIN) · airframe 25,598 hrs · 3,657 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN AT 3L OVERHEAD AISLE AREA WILL NOT STAY ENGAGED WITH FRAME. SECURED EXIT COVER POS 3L OVERHEAD.

Part: MONITOR — DEFECTIVE (CABIN) · airframe 25,552 hrs · 3,650 cycles

AIRCRAFT WAS NOT GNDED. SHUTDOWN INFLIGHT ENTERTAINMENT SYS. SEAT 8E IS REPORTED SMOKING BY PAX. REPLACED SMART MONITOR AT SEAT 8E IAW MFG 23-32-08. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION FLOORBEAM AT FRAME 74, L4 DOOR THRESHOLD, AT FRAME 74 & +Y2028. REPAIRED IAW EA 257488.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SHIM INBD OF L4 DOOR THRESHOLD, BETWEEN FRAME 75 & 75A AT Y2030. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SHIM INBD OF L4 DOOR, BETWEEN FRAME 73A & 74A AT Y2030. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SHIM INBD OF L4 DOOR THRESHOLD, BETWEEN FRAME 74 & 75 AT Y2030. REPLACED SHIM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 73 & 74 AT Y1220. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 47 & 53.2. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON BEAM, BETWEEN FRAME 75 & 78 AT Y380.L REPLACED BEAM IAW SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON LONGITUDINAL BEAM AT FRAME 73A & -Y2462. REPLACED BEAM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 40.3 & 46 AT -Y2462. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 53.2 & 55 AT -Y2462. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACKS, BETWEEN 73 & 74 AT Y510, 2 LOCATIONS. REPLACED SEAT TRACKS IAW SRM 51-42-11. SEE AALA201602059001 FOR ADDITIONAL PART INFORMATION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK AT FRAME 73A & Y2462. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACKS, BETWEEN 73 & 74 AT Y510, 2 LOCATIONS. REPLACED SEAT TRACKS IAW SRM 51-42-11. SEE AALA201602059002 FOR ADDITIONAL PART INFORMATION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK AT FRAME 32 & -Y1552.5. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 271CF IS CRACKED ON BOTTOM SIDE INSERT HOLES. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON FLOOR SUPPORT, BETWEEN FRAME 71 & 76 AT YO. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 71 & 75 AT -Y450. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 73 & 74 AT -Y1230. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. FWD CABIN FLOOR PANEL 221EF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. FWD CABIN FLOOR PANEL 222JF HAS CRACKS. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,464 hrs · 3,623 cycles

AIRCRAFT IN BASE MX. FWD CABIN FLOOR PANEL 231JF HAS CRACKS. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,966 hrs · 3,545 cycles

DOOR L2 EMER LIGHT BATTERY WILL NOT TEST. REPLACED L2 DOOR EMER LIGHT BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: LENS — DAMAGED (CABIN) · airframe 24,828 hrs · 3,521 cycles

TAPE HOLDING EMER LENS IN CTR AISLE AT ROW 23. REPLACED LENS COVER.

Part: BATTERY — FAILED (CABIN) · airframe 22,877 hrs · 3,275 cycles

EPSU BATTERIES 14WL & 17WL FAILED BITE TEST. REPLACED EPSU BATTERIES.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,858 hrs · 3,273 cycles

4L JUMP SEAT FLASHLIGHT BLINK INDICATION VERY DIM. REPLACED THE 4L JUMP SEAT FLASHLIGHT BATTERY.

Part: LENS — BROKEN (CABIN) · airframe 21,922 hrs · 3,129 cycles

AFT LT EMER LIGHT BROKEN. REPLACED BROKEN LENS.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY POWER SUPPLY AT DOOR 1R IS INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,928 hrs · 2,937 cycles

EMERGENCY FLASHLIGHT AT L1 OTBD JUMP SEAT LED NOT FLASHING. REPLACED THE L1 OTBD JUMP SEAT FLASHLIGHT BATTERY.

Part: FLOOR PANEL — SEPARATED (FUSELAGE) · airframe 20,742 hrs · 2,907 cycles

C1 CHECK TOP COMPOSITE SURFACE OF FLOORBOARD PULLED UP BETWEEN FRAME 22 TO 25 ON LT SIDE. REPLACED FLOOR PANEL 231NF IAW SRM 53-02-00 & IRM 9701 REV G.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 20,060 hrs · 2,812 cycles

A5 CHECK R1 DOOR ASSIST BOTTLE PRESS FOUND BELOW SERVICEABLE LIMIT IAW JOB CARD 33C80052002. SERVICED R1 DOOR ASSIST BOTTLE PRESS IAW JOB CARD 33C80052002.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 20,067 hrs · 2,813 cycles

EPSU 15WL FAILS TEST WITH BATTERY FAULT. REPLACED EPSU 15WL BATTERY.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 20,060 hrs · 2,812 cycles

A5 CHECK L4 DOOR ASSIST BOTTLE PRESS FOUND BELOW SERVICEABLE LIMIT IAW JOB CARD 33C80052002. SERVICED L4 DOOR ASSIST BOTTLE PRESS IAW JOB CARD 33C80052002.

Part: LENS — MISSING (CABIN) · airframe 19,923 hrs · 2,795 cycles

LAVATORY L38 MISSING EMER LIGHT LENS. INSTALLED EMER LIGHT LENS AT LAVATORY L38. OK FOR SERVICE.

Part: LENS — CRACKED (CABIN) · airframe 17,610 hrs · 2,430 cycles

PHL EMERGENCY LIGHT LENS BROKEN AT LAVATORY L38. MX REPLACED BROKEN LENS.

Part: CIRCUIT CARD — BURNED (ZONE 100) · airframe 16,716 hrs · 2,239 cycles

UPON ACFT POWER UP AT GATE SMOKE VISIBLE FROM BEHIND GLARESHIELD ECAM ELECTRIC CIRCUIT BREAKER TRIPPED ANNUNCIATOR LIGHT RELAY ESS 8LP DISPLAYED. MAINTENANCE REMOVED AND BURNED 1LPS CONTROL UNIT CIRCUIT BOARD, ANNUNCIATOR LIGHTS OPS CHECK IS GOOD.

Part: COVER — MISSING (ZONE 200) · airframe 16,574 hrs · 2,209 cycles

EMERGENCY LIGHT COVER MISSING. MAINTENANCE REPLACED AND SECURED EMERGENCY LIGHT LENS.

Part: LENS — MISSING (ZONE 200) · airframe 15,653 hrs · 2,082 cycles

EMERGENCY ESCAPE PATH LIGHT AT LAV L53 AFT END MISSING LENS. MX INSTALLED L53 AFT EMERGENCY LIGHT LENS.

Part: LENS — MISSING (CABIN) · airframe 14,880 hrs · 1,984 cycles

EMERGENCY EXIT LIGHT LENSE MISSING AT LAV 37 & 53. MX REPLACED MISSING EMERGENCY LIGHT LENS AT LAV'S 53 & 37.

Part: COVER — MISSING (EXIT SIGN) · airframe 14,836 hrs · 1,978 cycles

EMERGENCY EXIT SIGN OVER 2L DOOR MISSING COVER. MX INSTALLED NEW SIGN COVER. OPS CHECKS OK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 13,500 hrs · 1,805 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 38DS BETWEEN FR73 & FR76 INBOARD OF R-4 DOOR AT S25R. REPLACED CABIN FLOOR PANEL 38DS IAW IRM 9701, REV G, A330 SRM 53-02-00 & EA 104645.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 13,500 hrs · 1,805 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 112DS BETWEEN FR73 & FR76 INBOARD OF R-4 DOOR AT S25R. REPLACED CABIN FLOOR PANEL 112DS IAW IRM 9701, REV G, A330 SRM 53-02-00 & EA 104645.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 13,500 hrs · 1,805 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 40DS BETWEEN FR73 & FR76 INBOARD OF R-4 DOOR AT S25R. REPLACED CABIN FLOOR PANEL 40DS IAW IRM 9701, REV G, A330 SRM 53-02-00 & EA 104645.

Part: LENS — LOOSE (EXIT SIGN) · airframe 12,644 hrs · 1,667 cycles

EXIT COVER (SIGN) AT SEAT 3L DOOR CAME OFF. MAINTENANCE SECURED EMERGENCY EXIT SIGN LENS.

Part: LENS — MISSING (CABIN) · airframe 12,561 hrs · 1,656 cycles

SEAT 28HG ESCAPE PATH LIGHT MISSING LENS. MAINTENANCE REMOVED & REPLACED 28HG ESCAPE PATH LIGHT MODULE. OPERATIONAL CHECK IS OK.

Part: MONITOR — MALFUNCTIONED (CABIN)

VIDEO SCREEN OF ENTERTAINMENT SYSTEM WERE SMOKING WITH FUMES AT SEAT 27 A AND B. SYSTEM WAS SHUTDOWN. MAINTENANCE REPLACED VIDEO MONITOR AT 27A.

Part: LENS — MISSING (CABIN) · airframe 12,020 hrs · 1,584 cycles

EMERGENCY EXIT LENS COVERS MISSING AT BULKHEAD NEAR ROW 23. MAINTENANCE REMOVED & REPLACED EMERGENCY EXIT LENS COVERS AS NEEDED .

Part: LENS — MISSING (CABIN) · airframe 11,399 hrs · 1,506 cycles

RED LENS EMERGENCY LIGHT MISSING L53 WALL. MAINTENANCE INSTALLED LENS, OPS CHECKS GOOD.

Part: LENS — MISSING (CABIN) · airframe 11,214 hrs · 1,484 cycles

PHL - EMERGENCY ESCAPE PATH MARKING LIGHT ON LAV L53 WALL MISSING LENS. INSTALLED LENS ON LAV L53 EE LIGHT, OPS CHECKS OK.

Part: COVER — OUT OF POSITION (CABIN) · airframe 10,840 hrs · 1,440 cycles

EMERGENCY LIGHT COVER FOUND LOCATION UNKNOWN. MAINTENANCE REPLACED EMERGENCY LIGHT COVER AT L35. OK FOR SERVICE.

Part: CONTROL UNIT — INOPERATIVE (EVAC SLIDE) · airframe 9,872 hrs · 1,321 cycles

L3 AND R3 DOORS SLIDE MECHANISM ICE PROTECTION INOPERATIVE. MAINTENANCE REPLACED AFT IPCU (16DS). OPERATIONAL TEST IS SATISFACTORY.

Part: FITTING — INOPERATIVE (GIRT BAR) · airframe 9,572 hrs · 1,282 cycles

REFERENCE TSI - TROUBLESHOT FOUND GIRT BAR HEATED FITTINGS INOPERATIVE ON L1 DOOR FORWARD FITTING (FIN 5DH) & R1 DOOR FORWARD FITTING (FIN 6DH). MAINTENANCE REMOVED AND REPLACED GIRT BAR FITTINGS 5DH AND 6DH.

Part: HEATER — INOPERATIVE (L2 DOOR) · airframe 9,572 hrs · 1,282 cycles

ESCAPE SLIDE LOCKING MECHANISMS ICE PROTECTION AT DOORS 2L AND 4L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR HEATER 13DH.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 4A SEAT MOUNTED EMERGENCY ESCAPE PATH MARKING INOPERATIVE. MAINTENANCE LIGHT REPLACED THE LIGHT ASSEMBLY.

Part: OVEN — OVERHEATED (GALLEY) · airframe 7,069 hrs · 967 cycles

PHL- OVEN NR 1 4-2 BECAME VERY HOT. CABINETS ABOVE AND WALL BESIDE OVEN BECAME SO HOT THEY WERE TO HOT TO TOUCH. ODOR OF MELTING PLASTIC IN AREA MOST LIKELY FROM WALL COVERING PULLED CB DISCONTIUED USING. MAINTENANCE REMOVED AND REPLACED THE OVEN AND PERFORMED A SATISFACTORY OPERATIONAL TEST.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 6,751 hrs · 927 cycles

FLIGHT 743, BCN - PHL - CAPTAIN STATED THAT UPON GEAR RETRACTION THE GREEN HYDRAULIC SYSTEM LIGHT ILLUMINATED. THE GEAR WOULD NOT RETRACT, GEAR DOORS OPENED AND REMAINED OPEN. IT WAS AGREED TO RETURN TO BCN. THE FLIGHT LANDED UNEVENTFULLY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVES MANIFOLD AND PERFORMED FUNCTIONAL TEST OF NORMAL EXTENSION AND RETRACTION SYSTEM.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 6,751 hrs · 927 cycles

FLIGHT 742, PHL-BCN - CAPTAIN REPORTED AN ECAM - HYD G SYSTEM LEAK, HYDRAULIC PRESSURE WAS STILL 3450 PSI. AFTER GEAR EXTENSION AND LOCKED IN DOWN POSITION FLIGHT LOST THE ENTIRE GREEN HYD SYSTEM. EMERGENCY WAS DECLARED, THE FLIGHT LANDED WITHOUT INCIDENT BUT NEEDED TOWED TO THE GATE. MAINTENACE REPLACED THE GREEN ENGINE 1 HYDRAULIC PUMP.

Part: COVER — OUT OF POSITION (CABIN)

FLIGHT 754, PHL-CDG - EMERGENCY EXIT LIGHT MISSING COVER OPPOSITE 1L DOOR. MAINTENANCE FOUND THE COVER ON THE FLOOR, RESECURED COVER. OPERATIONAL CHECK IS SATISFACTORY.

Part: UNKNOWN — ODOR (AC SYSTEM)

PHL - FLT 796 EN ROUTE PHL TO TLV. AFTER TAKEOFF, THE CREW NOTICED A PUNGENT ODOR. AFTER CYCLING THE PACKS, IT WAS DECIDED THAT THE ODOR WAS COMING FROM ONE OF THEM. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION IS PENDING.

Part: ACTUATOR — DEACTIVATED (R1 DOOR)

CDG - DURING THE DAILY CHECK, WHILE PERFORMING A DOOR ASSIST BOTTLE PRESSURE CHECK FOR THE R1 DOOR, FOUND THE R1 DOOR WITH A SAFETY PIN INSTALLED INTO THE PERCUSSION HOUSING, PREVENTING OPERATION OF THE DOOR ASSIST/DAMPER ASSEMBLY. MAINTENANCE REMOVED THE SAFETY PIN FROM THE R1 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER.

Part: ACTUATOR — DEACTIVATED (L2 DOOR)

CDG - DURING THE DAILY CHECK, WHILE PERFORMING A DOOR ASSIST BOTTLE PRESSURE CHECK FOR THE L2 DOOR, FOUND THE L2 DOOR WITH A SAFETY PIN INSTALLED INTO THE PERCUSSION HOUSING, PREVENTING OPERATION OF THE DOOR ASSIST/DAMPER ASSEMBLY. MAINTENANCE REMOVED THE SAFETY PIN FROM THE L2 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER.

Part: ACTUATOR — DEACTIVATED (L1 DOOR)

CDG - DURING THE DAILY CHECK, WHILE PERFORMING A DOOR ASSIST BOTTLE PRESSURE CHECK FOR THE L1 DOOR, FOUND THE L1 DOOR WITH A SAFETY PIN INSTALLED INTO THE PERCUSSION HOUSING, PREVENTING OPERATION OF THE DOOR ASSIST/DAMPER ASSEMBLY. MAINTENANCE REMOVED THE SAFETY PIN FROM THE L1 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER.

Part: ACTUATOR — DEACTIVATED (L4 DOOR)

CDG - DURING THE DAILY CHECK, WHILE PERFORMING A DOOR ASSIST BOTTLE PRESSURE CHECK FOR THE L4 DOOR, FOUND THE L4 DOOR WITH A SAFETY PIN INSTALLED INTO THE PERCUSSION HOUSING, PREVENTING OPERATION OF THE DOOR ASSIST/DAMPER ASSEMBLY. MAINTENANCE REMOVED THE SAFETY PIN FROM THE L4 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER.

Part: ACTUATOR — DEACTIVATED (R2 DOOR)

CDG - DURING THE DAILY CHECK, WHILE PERFORMING A DOOR ASSIST BOTTLE PRESSURE CHECK FOR THE R2 DOOR, FOUND THE R2 DOOR WITH A SAFETY PIN INSTALLED INTO THE PERCUSSION HOUSING, PREVENTING OPERATION OF THE DOOR ASSIST/DAMPER ASSEMBLY. MAINTENANCE REMOVED THE SAFETY PIN FROM THE R2 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 4,334 hrs · 614 cycles

CWF - C1 - MAJOR REPAIR - CABIN FLOOR PANEL 272KF IS SPONGY BETWEEN FR72 TO FR74 & BETWEEN -Y1456 TO -Y1959. REPLACED CABIN FLOOR PANEL 272KF BETWEEN FR72 TO FR74 & BETWEEN -Y1456 TO -Y1959 IAW EA 140298 & MCGILL IRM 9701 REV G.

Part: BATTERY — DISCHARGED (MEGAPHONE)

PHL - THE FORWARD AND AFT MEGAPHONES REQUIRE SERVICING. REPLACED THE MEGAPHONE BATTERIES.

Part: OVEN — MALFUNCTIONED (GALLEY)

EN ROUTE, AT FL400, CREW REPORTED AN ELECTRICAL, SCORCH, BARNYARD LIKE ODOR ENTERED THE COCKPIT & CABIN. FLIGHT ATTENDANT IN CENTER CABIN REPORTED BURNING EYES. CREW SWITCHED PACK TO HIGH FLOW AND SMELL RECEDED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MID GALLEY OVEN NR 2 PRODUCING BURNING SMELL. REMOVED AND REPLACED NR 2 GALLEY OVEN PER MM 25-35-19. OPERATIONAL CHECK GOOD. ALSO, REMOVED AND REPLACED RECIRCULATION FILTERS PER MM 21-21-41. NO FURTHER DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

CDG - DURING THE DAILY CHECK, FOUND, AT DOOR L4, THE AFT ATTENDANT SEAT FLASHLIGHT INOPERATIVE AND SEAL BROKEN. REPLACED THE L4 FLASHLIGHT.