N283AY

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 41,034 hrs · 6,079 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 4H EMERGENCY LIGHT HARNESS DAMAGED. REPLACED WIRE HARNESS PER CMM 25-02-38.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,815 hrs · 5,925 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING CRUISE, AT SEPARATE INTERVALS, L1 AND R1 FUEL PUMPS FAULTED WITH A LOW PRESSURE ECAM. EVENTS LASTED ONLY ABOUT 5 MINUTES A PIECE, THEN RETURNED TO NORMAL STATUS. MAINTENANCE ACCOMPLISHED OPERATIONAL TEST OF MAIN AND STBY PUMPS IAW AMM 28-21-00-710-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,804 hrs · 5,923 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 38DS DELAMINATED. REPLACED FLOOR PANEL PER AMM 25-27-51-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,804 hrs · 5,923 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 40DS DELAMINATED. REPLACED FLOOR PANEL PER AMM 25-27-51-400-801-A.

Part: SEAT TRACK — CORRODED (FRAMES 58-67) · airframe 39,804 hrs · 5,923 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 58 AND FR67 AT-Y450. REPLACED SEAT TRACK PER SRM 51-42-11 AND 51-72-11.

Part: A/C PACK — ODOR (RIGHT) · airframe 39,138 hrs · 5,805 cycles

DURING TAKEOFF, FLEX POWER, FLIGHT DECK ODOR, TRANSIENT, MILD, CLEARED WITHIN 5 MINUTES AFTER CLIMB THRUST. REPLACED THE RIGHT PACK COMPONENTS. LEAK CHECK AND OPERATIONS CHECK GOOD IAW TSI PERFORMED JC 33L00021001, AND JC 33L00071001.

Part: ENGINE — LEAKING (NR 2) · airframe 39,138 hrs · 5,805 cycles

AIRCRAFT WAS GROUNDED: CABIN ODOR REPORTED. SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. FOUND OIL STAINING ON ALL STAGES OF THE IPC AND LIGHT STAINING ON 1ST AND 2ND HPC. (CLOSED)

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 38,963 hrs · 5,771 cycles

CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. MAINTENANCE ADJUSTED THE PILLAR TRIM AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 38,487 hrs · 5,677 cycles

WHILE ACCOMPLISHING JC 33C20033002, THE R3 DOOR EMERGENCY POWER SUPPLY BATTERIES FAILED. MAINTENANCE REPLACED THE BATTERIES, AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 38,487 hrs · 5,677 cycles

WHILE ACCOMPLISHING JOBCARD 33C20033002, THE R1 DOOR EMERGENCY POWER SUPPLY BATTERIES FAILED. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: MEGAPHONE — FAULTY (CABIN) · airframe 38,054 hrs · 5,609 cycles

AIRCRAFT WAS NOT GROUNDED. MEGAPHONE LEFT HAND FORWARD REPORTED INTERMITTENT BEEPING SOUND. REPLACED MEGAPHONE AT FORWARD LEFT POSITION, CHECKS GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 37,961 hrs · 5,595 cycles

CAPTAIN`S WINDSHIELD ANTI-ICE FAILED. LEFT WINDSHIELD HEAT ECAM MESSAGE ILLUMINATED APPROXIMATELY 40 MINUTES AFTER TAKEOFF. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT WINDSHIELD IAW JC 33L21056001. SYSTEM OK FOR SERVICE.

Part: TOILET — LEAKING (LAVATORY) · airframe 37,891 hrs · 5,583 cycles

PHL FLT 717 EN-ROUTE MUC - PHL. THE AIRCRAFT WAS GROUNDED. CREW REPORTS URINE ODOR THROUGHOUT THE ENTIRE CABIN FROM PUSHBACK TO TAXI IN. MAINTENANCE ACCOMPLISHED J/C 33L00021001 AND J/C 33L13038001. R&R L74 TOILET ASSY AND CLEANED THOROUGHLY UNDER TOILET. ALSO REPLACED CARPET AT L74 LAV.

Part: THERMOSTAT — LOW (ZONE 400) · airframe 36,504 hrs · 5,387 cycles

THE AIRCRAFT WAS NOT GROUNDED. LHR FLIGHT 745 EN-ROUTE BCN - CLT. THE FLIGHT RECEIVED ECAM AIR BLEED LOW TEMPERATURE MESSAGE DURING CRUISE. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO LHR WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE LEFT BLEED SYSTEM ON MEL DEFERRAL. REPLACED NR 1 ENGINE FAN AIR VALVE (SEE SDR AALA201806089008) AND NR 1 ENGINE FAN AIR CONTROL THERMOSTAT PER AMM 36-11-43 AND 36-11-54. A SUPPLEMENTAL REPORT HAS BEEN ISSUED UPON RECEIPT OF FINAL CORRECTIVE ACTION. *** (CLOSED)

Part: VALVE — LOW (ZONE 400) · airframe 36,504 hrs · 5,387 cycles

THE AIRCRAFT WAS NOT GROUNDED. LHR FLIGHT 745 EN-ROUTE BCN - CLT. THE FLIGHT RECEIVED ECAM AIR BLEED LOW TEMPERATURE MESSAGE DURING CRUISE. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO LHR WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE LEFT BLEED SYSTEM ON MEL DEFERRAL. REPLACED NR 1 ENGINE FAN AIR VALVE AND NR 1 ENGINE FAN AIR CONTROL THERMOSTAT (SEE SDR AALA201806159014) PER AMM 36-11-43 AND 36-11-54.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 36,360 hrs · 5,367 cycles

WHILE PERFORMING J/C 33C20033002, AN EMERGENCY LIGHT BATTERY CAPACITY CHECK, THE POWER SUPPLY BATTERIES FAULTED ON THE LEFT AND RIGHT, 15WL AND 16WL,. REPLACED POWER SUPPLY UNIT 15WL AND 16WL PER AMM 33-51-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 36,360 hrs · 5,367 cycles

WHILE PERFORMING J/C 33C20033002, AN EMERGENCY LIGHT BATTERY CAPACITY CHECK, THE POWER SUPPLY UNIT BATTERIES FAULTED ON LEFT AND RIGHT, 15WL AND 16WL. REPLACED THE POWER SUPPLY 16WL IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 36,016 hrs · 5,316 cycles

EMERGENCY EXIT LENS ON BULKHEAD OF L53 LAVATORY IS MISSING. INSTALLED LENS ON EMERGENCY LIGHT AT L53 LAVATORY BULKHEAD IAW AMM 33-20-00.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,644 hrs · 5,260 cycles

SEAT 20GH EMERGENCY SEAT LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT HARNESS IAW CMM 25-23-54.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 35,579 hrs · 5,252 cycles

EMERGENCY LIGHT POWER SUPPLY BATTERIES FAILED A BITE CHECK IAW J/C 33C22033002 AT 13WL. REPLACED THE BATTERY PACK IAW AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 35,579 hrs · 5,252 cycles

EMERGENCY LIGHT POWER SUPPLY BATTERIES FAILED A BITE CHECK IAW J/C 33C22033002 AT 17WL. REPLACED THE BATTERY PACK IAW AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 35,579 hrs · 5,252 cycles

EMERGENCY LIGHT POWER SUPPLY BATTERIES FAILED A BITE CHECK IAW J/C 33C22033002 AT 14WL. REPLACED THE BATTERY PACK IAW AMM 33-51-38.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,396 hrs · 5,213 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT IAW AMM 33-52-00.

Part: GIRT BAR — DIRTY (L4 DOOR SLIDE) · airframe 35,146 hrs · 5,170 cycles

L4 DOOR WILL NOT ARM. REMOVED DEBRIS FROM THE GIRT BAR.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 34,428 hrs · 5,042 cycles

DELAMINATION FOUN ON THE FORWARD GALLEY FLOOR PANEL 242QF. REPLACED THE FLOOR PANEL IAW AMM 25-27-51-400-801-A.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 34,428 hrs · 5,042 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 242PF. REPLACED THE FLOOR PANEL IAW AMM 25-27-51-400-801-A.

Part: LENS — MISSING (CABIN) · airframe 34,385 hrs · 5,036 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT COVER MISSING BY L38. REPLACED LENS COVER.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 33,390 hrs · 4,898 cycles

EMERGENCY LIGHT LENS AT FWD OF LAV 74 IS LOOSE. SECURED THE LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,041 hrs · 4,849 cycles

LENS MISSING ON WALL MOUNTED EXIT EMERGENCY LIGHT FORWARD OF THE L3 DOOR. INSTALLED MISSING LENS.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 31,290 hrs · 4,557 cycles

EMERGENCY LIGHT BATTERY 11WL, FLAGGED BY EMERGENCY POWER SUPPLY UNIT TEST. REPLACED THE BATTERY AT 11WL IAW AMM 33-51-38.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 31,290 hrs · 4,557 cycles

EMERGENCY LIGHT BATTERY 14WL, FLAGGED BY EMERGENCY POWER SUPPLY UNIT TEST. REPLACED THE BATTERY AT 14WL IAW AMM 33-51-38.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 31,290 hrs · 4,557 cycles

EMERGENCY LIGHT BATTERY 18WL, FLAGGED BY EMERGENCY POWER SUPPLY UNIT TEST. REPLACED THE BATTERY AT 18WL IAW AMM 33-51-38.

Part: CHECK VALVE — FAULTY (NR 2 ENGINE) · airframe 31,290 hrs · 4,557 cycles

NR 2 ENGINE STALLED AT 55KTS DURING TAKEOFF ROLL. FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE ACCOMPLISHED TSM 71-00-00-810-A14-A. REPLACED RIGHT ENGINE IP CHECK VALVE PER TASK 36-11-41. AIRCRAFT WAS GROUNDED.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 31,039 hrs · 4,508 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 3R EXIT SIGN COVER FELL OFF. NEEDS REINSTALL. MAINTENANCE REINSTALLED EXIT SIGN COVER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — NOT SEATED (L4) · airframe 30,508 hrs · 4,377 cycles

L4 JUMPSEAT NEEDS FLASHLIGHT. INSPECTED, AND REPOSITIONED IN THE CRADLE, CKECKED OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 29,961 hrs · 4,307 cycles

EMERGENCY LIGHT COVER AT L3 DOOR BROKEN AND NOT STAYING ATTACHED. REPLACED EMERGENCY EXIT LIGHT LENS COVER.

Part: COVER — MISSING (EXIT SIGN) · airframe 28,584 hrs · 4,114 cycles

AIRCRAFT WAS NOT GNDED. 3L EXIT SIGN MISSING A COVER. 3L EXIT SIGN LOCATED IN ADJACENT OVERHEAD BIN & REFITTED.

Part: GIRT BAR — OBSTRUCTED (ZONE 800) · airframe 28,568 hrs · 4,112 cycles

AIRCRAFT WAS NOT GNDED. DOOR 4L WOULD NOT ARM. CLEANED & REMOVED DEBRIS FROM THE GIRT BAR & FLOOR ATTACH HOOKS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAILED (CABIN) · airframe 28,347 hrs · 4,081 cycles

AIRCRAFT WAS NOT GNDED. IAW TASK CARD 33C22033002, EPSU 17WL FAILED TEST. REPLACED EPSU 17WL BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-802A.

Part: LENS — DETACHED (CABIN) · airframe 27,873 hrs · 4,011 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR EMER EXIT LIGHT LENS COVER FELL OFF ON LANDING. RE- INSTALLED LENS COVER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-17-04-01.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 27,015 hrs · 3,830 cycles

AIRCRAFT WAS NOT GNDED. WHILE PERFORMING JC 33C80052002, FOUND 3R DOOR ASSIST BOTTLE LOW. SERVICED 3R DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 27,015 hrs · 3,830 cycles

AIRCRAFT WAS NOT GNDED. WHILE PERFORMING JC 33C80052002, FOUND DOOR 1L ASSIST BOTTLE LOW. SERVICED DOOR 1L ASSIST BOTTLE IAW AMM 52-10-00-600-802.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 26,652 hrs · 3,743 cycles

AIRCRAFT WAS IN BASE MX. ENVOY CLASS, SEAT 4H HAS A BROKEN IN SEAT EMER LIGHT WIRE HARNESS. R & R SEAT 4H WIRE HARNESS IAW CMM 25-02-3.8. PERFORMED OPERATIONAL TEST IAW AMM 33-51-12-400-814. CHECKED GOOD.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 26,652 hrs · 3,743 cycles

AIRCRAFT WAS IN BASE MX. ENVOY CLASS SEAT 3H HAS BROKEN, IN SEAT EMER LIGHT WIRE HARNESS. R & R SEAT WIRE HARNESS IAW CMM 25-02-38 & PERFORMED OPERATIONAL TEST IAW AMM 33-51-12-400-814. CHECKED GOOD.

Part: THRESHOLD — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

CORROSION ON R4 DOOR THRESHOLD, BETWEEN FRAME 73A & 75A, AT STRINGER 26R. REPLACED THRESHOLD IAW SRM 51-42-11 & SRM 51-44-11.

Part: THRESHOLD — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

CORROSION ON L4 DOOR THRESHOLD, BETWEEN FRAME 73A & 75A AT STRINGER 26L. REPLACED THRESHOLD IAW SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK, BETWEEN FRAME 73 & 74 AT Y1220. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 & SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION BEAM AT FRAME 75 & Y450. REPAIRED BEAM IAW SRM 53-41-14 FIG 211.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT, BETWEEN FRAME 75 & 76 AT -Y2462. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT FRAME 74 & Y794.3. REPAIRED FLOORBEAM IAW SRM 53-41-14 FIG 211.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT FRAME 74 & -Y1137.1. REPAIRED FLOORBEAM IAW SRM 53-41-14 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT FRAME 53.3 & -Y2462. REPAIRED SEAT TRACK IAW SRM 53-31-15 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT FRAME 74 & Y1137.1. REPAIRED FLOORBEAM IAW SRM 53-41-14 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT FRAME 73A & Y2462. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 & SRM 51-44-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON ANGLE, BETWEEN FRAME 75 & 77 AT Y1930. REPLACED ANGLE IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT FRAME 74 & -Y794.3. REPAIRED FLOORBEAM IAW SRM 53-41-14 FIG 211.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON CROSSBEAM SHIM AT FRAME 75A & Y2014. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L4 DOOR THRESHOLD CROSSBEAM SHIM, BETWEEN FRAME 75 - 76 & Y2032. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L4 DOOR THRESHOLD SHIM, BETWEEN FRAME 73A & 74 AT Y2014. REPLACED SHIM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON SEAT TRACK, BETWEEN FRAME 32 & 33 AT Y1959. REPLACED SEAT TRACK IAW SRM 53-00-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON SEAT TRACK, BETWEEN FRAME 73 - 74 AT Y1625. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON SEAT TRACK, BETWEEN FRAME 32 & 33 AT -Y1959. REPLACED SEAT TRACK IAW SRM 53-00-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON SEAT TRACK, BETWEEN FRAME 32 & 33 AT Y1552.5. REPLACED SEAT TRACK IAW SRM 53-00-15, 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON FLOOR SUPPORT AT FRAME 75 & -Y400. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, 51-42-11 & 51-44-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON CABIN FLOOR CROSSBEAM, BETWEEN FRAME 75 & 76, Y1137.2 & Y1447.8. REPLACED FLOOR CROSSBEAM IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON CABIN FLOOR CROSSBEAM, BETWEEN FRAME 75 & 76, Y450 & Y794.3. REPLACED CROSSBEAM IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,651 hrs · 3,743 cycles

S1 CHECK, CORROSION ON CABIN FLOOR CROSSBEAM, BETWEEN FRAME 75A & 76 AT Y1520. REPLACED CROSSBEAM IAW SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,651 hrs · 3,743 cycles

AFT CABIN FLOOR PANEL 272JF, 40DS, DELAMINATED & HAS CORRODED FASTENERS. REPLACED CABIN FLOOR PANEL 272JF, 40DS.

Part: LENS — MISSING (CABIN) · airframe 26,308 hrs · 3,689 cycles

EMERGENCY PATH LENS COVER MISSING NEXT TO DOOR 3L. INSTALLED LENS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAULTED (CABIN) · airframe 25,604 hrs · 3,599 cycles

EMERGENCY LIGHT BATTERIES SHOWED FAULT WHILE ACCOMPLISHING JC 33C22033002 AT DOORS L2 & R2. REPLACED EMER LIGHT BATTERIES AT DOORS L2 & R2 IAW AMM 33-51-38-400-802A. OPERATIONS CHECKED OK.

Part: BATTERY — FAULTED (CABIN) · airframe 25,604 hrs · 3,599 cycles

EMERGENCY LIGHT BATTERY AT DOOR 3R SHOWING BATTERY FAULT. REPLACED BATTERY IAW AMM 33-51-38-400-802A. OPERATIONS CHECKED OK.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 25,326 hrs · 3,561 cycles

L4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L4 DOOR ASSIST BOTTLE WITH DRY NITROGEN IAW AMM 52-13-14.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 21,996 hrs · 3,023 cycles

C1 CHECK 3R DOOR ASSIST BOTTLE IS SHOWING PRESS LOWER THAN 1700 PSI. REMOVED & INSTALLED NEW ACTUATOR, DOOR EMER EXIT DOOR 3R IAW AMM 52-22-14-400-801-A & AMM 52-22-14-000-801-A.

Part: SIGN — UNSECURE (CABIN) · airframe 21,523 hrs · 2,962 cycles

3R DOOR EXIT LIGHT ABOVE DOOR FELL OFF & IS CRACKED. REPLACED SIGN.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 21,380 hrs · 2,943 cycles

A CHECK 1R DOOR ASSIST BOTTLE PRESS IS LOW. SERVICED 1R DOOR ASSIST BOTTLE IAW JOB CARD 33C80052002.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 21,380 hrs · 2,943 cycles

A CHECK 2R DOOR ASSIST BOTTLE PRESS IS LOW. SERVICED 2R DOOR ASSIST BOTTLE IAW JOB CARD 33C80052002.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 21,380 hrs · 2,943 cycles

A CHECK 2L DOOR ASSIST BOTTLE PRESS IS LOW. SERVICED 2L DOOR ASSIST BOTTLE IAW JOB CARD 33C80052002.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 21,380 hrs · 2,943 cycles

A CHECK 4L DOOR ASSIST BOTTLE PRESS IS LOW. SERVICED 4L DOOR ASSIST BOTTLE IAW JOB CARD 33C80052002.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,380 hrs · 2,943 cycles

EMERGENCY LIGHT TEST CLASS 1 FAULT 15WL, 16WL & 17WL BATTERY. REPLACED BATTERY'S ON EMER POWER SUPPLY UNITS 15WL, 16WL & 17WL.

Part: DAMPENER — LOW PRESSURE (R3 DOOR) · airframe 21,371 hrs · 2,942 cycles

3R DOOR AMBER LIGHT SLIDE LOW PRESS. MX SERVICED 3R DOOR DAMPENER.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 21,354 hrs · 2,940 cycles

R3 DOOR ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE.

Part: SIGN — DETACHED (CABIN) · airframe 21,041 hrs · 2,896 cycles

EXIT SIGN AT 3L DOOR NEAR FLIGHT ATTENDANT JUMP SEAT HAS DETACHED. EXIT SIGN SECURED IN PLACE, NOW SATISFACTORY.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 20,917 hrs · 2,880 cycles

CIDS PANEL & SERVICE REPORT INDICATE DOOR 3R PRESS LOW. BOTTLE SERVICED TO NOMINAL PRESS. LEAK CHECKED SATISFACTORY.

Part: LOCK TAB — OUT OF ALIGNMENT (EXIT SIGN) · airframe 20,597 hrs · 2,834 cycles

EMERGENCY EXIT SIGN FALLS OFF 3L DOOR. RESET LOCK TAB ON 3L DOOR EMER EXIT SIGN LENS. CHECKED OK.

Part: VALVE — FAILED (AC BAY)

RIGHT AFTER TAKEOFF A STRONG BURNING SMELL ORIGINATED NEAR FWD ACFT. SMELL STARTED NEAR FRONT 1L DOOR & MOVED THRU CABIN TO REAR. COCKPIT COULD ALSO SMELL IT. ODOR LASTED FOR ABOUT A MINUTE THEN SLOWLY DISSIPATED. THE CAPTAIN RETURNED TO CLT & LANDED UNEVENTFULLY. R & R THE TRIM AIR VLV.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,912 hrs · 2,733 cycles

EPSU SYS TEST GAVE FAULT MSGS BATTERY & EPSU, 11WL, DOOR 1 & BATTERY & ESPU, 14WL, DOOR 2. REPLACED BATTERIES AT DOOR 1L & DOOR 2R, OPERATIONS & BITE CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,205 hrs · 2,608 cycles

R2 DOOR EMERGENCY LIGHT SUPPLY BATTERY FAILED BITE TEST. R & R POWER SUPPLY BATTERY. OPERATIONAL CHECK IS GOOD.

Part: LENS — UNSECURE (CABIN) · airframe 19,199 hrs · 2,607 cycles

COVER ON EMERGENCY LIGHT BETWEEN LAVATORY L38 & ROW 6 ON ACFT RT CAME OFF. RE-ATTACHMENT REQUIRED, REPLACED EMERGENCY LIGHT LENS AS REQUIRED.

Part: GENERATOR — LEAKING (APU) · airframe 18,769 hrs · 2,513 cycles

A STRONG ODOR OF OIL REPORTED IN THE AFT OF THE AIRCRAFT DURING CLIMB & DESCENT. MAINTENANCE REPLACED THE APU GENERATOR. ALSO CLEANED THE APU INLET RAM AIR DOOR AND ACCOMPLISHED COMPRESSOR WAST. THE APU INLET DUCT AS REMOVED DUE TO DAMAGE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 18,318 hrs · 2,418 cycles

R3 DOOR ASSIST BOTTLE LOW, SERVICED R3 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 17,863 hrs · 2,330 cycles

DURING ETOPS CHECK, FOUND R3 DOOR ASSIT BOTTLE LOW PRESSURE. MAINTENANCE SERVICED AS REQUIRED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,864 hrs · 2,202 cycles

EMERGENCY LIGHT LENS BROKEN. MX REPLACED LENS.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 16,737 hrs · 2,185 cycles

ON BATHROOM WALL 3/R DOOR AREA, COVER FOR EMERGENCY LIGHT IS DETACHED. MX REPLACED COVER, OK FOR SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 15,220 hrs · 1,997 cycles

EMERGENCY LIGHT IN CEILING 23 RT INOPERATIVE. MAINTENANCE REPAIRED WIRING, OPERATIONAL CHECK IS GOOD.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 15,048 hrs · 1,973 cycles

CLT - 3R DOOR ASSIST BOTTLE PRESSURE BELOW GREEN BAND. SERVICED 3R DOOR ASSIST BOTTLE.

Part: WARNING LIGHT — FALSE ACTIVATION (L4 DOOR SLIDE) · airframe 14,403 hrs · 1,869 cycles

L4 DOOR SLIDE SHOWS LOW PRESSURE ON CIDS PANEL. MAINTENANCE TROUBLESHOT WITH NO FAULTS FOUND. OKAY FOR SERVICE.

Part: HANDLE — DEFECTIVE (DOOR) · airframe 14,392 hrs · 1,867 cycles

PHL - AT APPROXIMATELY 5000 FEET AGL, THE "DOOR R MID CABIN" ANNUNCIATION ILLUMINATED. CABIN PRESSURE WAS NORMAL. VISUAL INSPECTION OF DOOR FROM CABIN CONFIRMED DOOR WAS SEALED. NO OTHER PROBLEMS NOTED. REPLACED EXTERIOR DOOR HANDLE.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 14,391 hrs · 1,866 cycles

C2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR73 & FR76 AT R4 DOOR AREA. REPAIRED FLOOR PANEL BETWEEN FR73 & FR76 AT R4 DOOR AREA IAW EA 104470A & EO 2511U084.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 14,391 hrs · 1,866 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 40DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA. REPLACED CABIN FLOOR PANEL 40DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA IAW EA 104470A & EO 2511U084.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 14,391 hrs · 1,866 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 112DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA. REPLACED CABIN FLOOR PANEL 112DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA IAW EA 104470A & EO 2511U084.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 14,391 hrs · 1,866 cycles

C2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 38DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA. REPLACED CABIN FLOOR PANEL 38DS BETWEEN FR73 TO FR76 AT R4 DOOR AREA IAW EA 104470A & EO 2511U084.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 13,607 hrs · 1,739 cycles

EMERGENCY DOOR CYLINDER PRESSURE LOW AT 3R. MAINTENANCE SERVICED EMERGENCY OPS CYLINDER AT DOOR 3R.

Part: UNKNOWN — SMOKE (CABIN) · airframe 13,578 hrs · 1,735 cycles

SEAT 7F VIDEO SCREEN WAS TURNED ON, THERE WAS AN IMMEDIATE ELECTRICAL ODOR AND SMOKE CAME OUT FROM BETWEEN THE SEAT BACK AND THE TOP OF THE VIDEO SCREEN. THE UNIT WAS TURNED OFF AND THE ODOR DISSIPATED QUICKLY. THE SCREEN WAS NOT USED DURING THE REMAINDER OFTHE FLIGHT. MAINTENANCE TURNED ON VIDEO SYSTEM SEAT 7F CHECKED OK. NO SMOKE OR ODOR. REPLACED SDU PRECAUTIONARY.

Part: APU — LEAKING (APU BAY) · airframe 13,278 hrs · 1,697 cycles

PHL - THE CREW NOTICED A CABIN ODOR AFTER BOARDING THE AIRCRAFT. THE APU AND A/C SYSTEM HAS AN OIL SMELL WITH APU AIR OR EXTERNAL AIRSOURCE. MAINTENANCE ACCOMPLISHED JC FOR CABIN AIR QUALITY AND DECONTAMINATION OF THE ECS. AFTER AN UNSUCCESSFUL TEST FLIGHT THE APU WAS REMOVED AND REPLACED. AIR QUALITY AND JC FOR ENGINE CABIN ODOR WERE ACCOMPLISHED ON THE LEFT AND RIGHT ENGINES WITH NO DEFECTS NOTED AT THIS TIME.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 12,972 hrs · 1,660 cycles

FOUND 3R DOOR ASSIST BOTTLE SHOWING "LOW PRESSURE" ON POST FLT REPORT. MAINTENANCE SERVICED 3R DOOR ASSIST BOTTLE. OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 12,713 hrs · 1,628 cycles

EXIT DOOR LIGHT FELL OFF ABOVE 3L DOOR. MAINTENANCE RE-INSTALLED EXIT COVER.

Part: LENS — MISSING (CABIN) · airframe 12,527 hrs · 1,606 cycles

EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT LAV L54 MISSING LENS. MAINTENANCE INSTALLED LENS ON L54 EMERGENCY ESCAPE PATH LIGHT. OPERATIONAL CHECK IS OK.

Part: SIGN — LOOSE (CABIN)

EXIT SIGN AT 2L FELL OFF. MAINTENANCE REPOSITIONED COVER OF EXIT SIGN AND SECURED. OPERATIONAL CHECK IS OK.

Part: COVER — MISSING (CABIN) · airframe 12,390 hrs · 1,590 cycles

WALL EMERGENCY LIGHT COVER MISSING OUTSIDE OF L54 LAV. MAINTENANCE REPLACED MISSING LENS COVER ON WALL EMERGENCY LIGHT. OK FOR SERVICE.

Part: SIGN — UNSECURE (CABIN)

TLV - 3L EMERGENCY EXIT SIGN FELL OFF. EMERGENCY EXIT SIGN AT 3L RE-INSTALLED.

Part: LENS — MISSING (CABIN) · airframe 12,225 hrs · 1,569 cycles

FLOOR ESCAPE PATH LIGHT OUTSIDE OF LAV L54 MISSING LENS. MAINTENANCE INSTALLED LENS AT FLOOR ESCAPE PATH LIGHT AT L54, OPERATIONAL CHECKS OKAY.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 12,225 hrs · 1,569 cycles

R3 DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED R3 DOOR EMERGENCY OPERATIONAL CYLINDER, LEAK CHECK OKAY.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 11,006 hrs · 1,419 cycles

R3 DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED EMERGENCY OPERATION CYLINDER PER MM 52-10-00-600-802, LEAK CHECK IS OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 10,301 hrs · 1,331 cycles

RED EMERGENCY EXIT LIGHT LENS MISSING AT LAV L53. MAINTENANCE INSTALLED EMERGENCY EXIT LENS AT L53, OPERATIONAL CHECKED OK.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 9,578 hrs · 1,240 cycles

LHR - EMERGENCY EXIT DOOR 3R ASSIST BOTTLE PX IN YELLOW BAND. MAINTENANCE SERVICED EMERGENCY ASSIST BOTTLE IAW AMM TASK 52-10-00-600-802-A.

Part: TRANSDUCER — INOPERATIVE (BRAKE SYSTEM) · airframe 9,535 hrs · 1,235 cycles

FLIGHT 1073, PHL-SJU - ECAM BRAKES RESIDUAL BRAKING ON BRAKE 1, 2, 5, 6. MAINTENANCE FOLLOWED TSM 32-40-00-810-927A REPLACED PRESSURE TRANSDUCER -BRAKE BLUE AS PER 32-44-18-000-801/32-44-18--400-801A PERFORMED OPS TEST AS PER 32-43-00-710-801/32-43-00-710-801A OPS CHECKS OK, NO MSG.

Part: LIGHT — INOPERATIVE (CABIN)

TLV - CABIN OVHD EMERGENCY LIGHT RT SIDE BETWEEN ROW 2 AND 3 INOP LOCATION 32WL. REPLACED EMEGENCY LIGHT DIODE ASSEMBLY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 9,512 hrs · 1,232 cycles

MAD - SPANISH SAFA INSPECTION REPORT: EMERGENCY LIGHT AT 3H INOP. MAINTENANCE FOUND CONNECTION TO LAMP HOLDER LOOSE, RECONECTED AND TESTED OK.

Part: LENS — MISSING (CABIN)

FLIGHT 796, PHL - TLV - EMERGENCY EXIT COVER MISSING NEAR SEAT 23F. MAINTENANCE APPLIED LENS AT POSITION 23F.

Part: LENS — BROKEN (CABIN)

CLT - AT 3L JUMPSEAT FORWARD EXIT SIGN BROKEN. MAINTENANCE REPLACED BROKEN LENS.

Part: SIGN — UNSECURE (CABIN)

PHL - THE EXIT SIGN AT ROW 23, AIRCRAFT RIGHT, WILL NOT STAY ATTACHED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 5,161 hrs · 629 cycles

CWF - C1 - MAJOR REPAIR - NR 6315230 - AREA OF DISBONDING ON FLOOR PANEL 232PF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 232PF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: CYLINDER — READS LOW (R3 DOOR)

CDG - R3 DOOR PRESSURE WAS LOW ON CIDS PANEL. DOOR R3 EMERGENCY OPERATION CYLINDER WAS SERVICED.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MAD - DURING DAILY CHECK, MAINTENANCE FOUND THE FLASHLIGHT AT JUMPSEAT DOOR R4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT AT DOOR R4. INSTALLED SEAL. OPS OK.