N282AY

Part: TEE FITTING — LEAKING (HYDRAULIC SYS) · airframe 40,066 hrs · 6,030 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO LHR ON ACCOUNT OF LOW LEVEL OF YELLOW HYDRAULIC SYSTEM INDICATION. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE FOUND A LEAKING T-FITTING DURING TROUBLESHOOTING. REMOVED AND REPLACED T-FITTING IAW AMM 29-13-03. OPS CHECK AND LEAK CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 39,620 hrs · 5,971 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-10-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,499 hrs · 5,822 cycles

AIRCRAFT WAS GROUNDED: F/A 1 REPORTED THAT THERE WAS AN ODOR ONBOARD. THE F/A STATED THAT THE ODOR WAS NOT PRESENT AT THEIR JUMPSEAT. THE ODOR WAS A CHEMICAL TYPE ODOR (CATEGORY A) AND NO EMERGENCY EQUIPMENT WAS USED AND IT WAS NOT AN OVEN FIRE. MAINTENANCE ACCOMPLISHED SMOKE ODOR FUMES CARD 33L00021001 COMPLETED. INSPECTED GALLEYS, GALLEYS'S EQUIPMENTS, RUN PACKS, TOILETS AND NO BURNING SMELL NOTICED.

Part: RECEPTACLE — SPARKS (EXTERNAL POWER) · airframe 38,364 hrs · 5,805 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS AFTER HOOKING UP EXTERNAL POWER TO RECEPTACLE A & B, RECEPTACLE A BEGAN SPARKING. ON SECOND ATTEMPT RECEPTACLE A MADE POPPING SOUND WITH VISIBLE SMOKE PRESENT. REMOVED AND REPLACED EXTERNAL POWER RECEPTACLE A IAW AMM 24-41-51, PERFORMED BITE IAW AMM 24-41-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 38,355 hrs · 5,804 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED R1 DOOR ASSIST BOTTLE TO PROPER PRESSURE PER M/M 52-10-00-600-802-A.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,181 hrs · 5,778 cycles

AIRCRAFT IN BASE VIST: MAINTENANCE FOUND R1 ESPU BATTERY FAULT. REMOVED AND REPLACED BATTERY FOR ESPU AT R1. OPS TEST GOOD.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 37,523 hrs · 5,677 cycles

CORROSION FOUND ON THE SEAT TRACK AT FRAME 33 AND +Y1552.5. REPLACED THE SEAT TRACK IAW SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 32-35) · airframe 37,523 hrs · 5,677 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 32 AND 35, +Y1552.5. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 37,523 hrs · 5,677 cycles

CORROSION ON THE SEAT TRACK BETWEEN FRAMES 73 AND 74, YB1. REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 37,523 hrs · 5,677 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73, AND 74 , YB1. REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 37,523 hrs · 5,677 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 AND 74, YC1. REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 37,523 hrs · 5,677 cycles

CORROSION FOUND ON THE SEAT TRACK, BETWEEN FRAMES 73 AND 74, YC1. REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,459 hrs · 5,656 cycles

ODOR PRESENT DURING TAXI. ISOLATED BLEED SYSTEM, LEFT BLEED WITH LEFT PACK NO ODOR. RIGHT BLEED WITH RIGHT PACK ONLY, ODOR PRESENT. LEFT BLEED WITH RIGHT PACK ONLY, ODOR PRESENT. THE AIRCRAFT WAS GROUNDED. CHECKED THE PACKS, NO ODOR NOTED FROM ANY BLEED SOURCE.

Part: APU — ODOR (ZONE 200) · airframe 37,458 hrs · 5,655 cycles

THE AIRCRAFT WAS GROUNDED. FCF FAILED, ODOR STILL PRESENT IN PACKS. MORE SO ON RIGHT PACK. REPLACED APU ASSEMBLY AS PER JOB CARD 33L31549001. OPERATIONS AND LEAK CHECKS GOOD.

Part: ENGINE — ODOR (LEFT) · airframe 37,458 hrs · 5,655 cycles

CABIN ODOR PRESENT DURING CLIMB, RECURRING DURING DESCENT. FLIGHT ATTENDANTS REPORTED THE ODOR AT THE L2 & R2 DOORS DURING CRUISE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE LEFT ENGINE IAW JC 33L40071003. MAINTENANCE ALSO ACCOMPLISHED JC 33L00021001, 33L00071001, AND 33L0002102.

Part: ENGINE — CONTAMINATED (NR 1) · airframe 37,430 hrs · 5,642 cycles

DURING CLIMB OUT, BOTH PILOTS NOTICED A DIRTY-SOCK ODOR. RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE IAW JC 33L40071003 DUE TO OIL INJESTION.

Part: ENGINE — OVERSERVICED (NR 2) · airframe 37,428 hrs · 5,640 cycles

DIRTY SOCK MIXED WITH AIRCRAFT DEICE FLUID ODOR IN THE CABIN. THE AIRCRAFT WAS GROUNDED. PERFORMED CABIN ODOR CARDS 33L00071001, 33L00021001, 33L00021001, AND 33L00021002. FOUND THE NR 2 ENGINE OVERSERVICED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 36,669 hrs · 5,508 cycles

POWER SUPPLY 14WL FAILED AN OPS CHECK. REPLACED THE POWER SUPPLY, AND BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD. THE AIRCRAFT WAS OK FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 35,462 hrs · 5,346 cycles

AIRCRAFT WAS GROUNDED. AIR RETURN - CLT ACCOUNT MECHANICAL ISSUE. GREEN HYDRAULIC PUMP FAILURE. ECAM MESSAGE "HYD G ENG PUMP LO PR" AFTER TAKEOFF. NO EMERGENCY DECLARED, FLIGHT BURNING FUEL, NOT EXPECTED TO LAND OVERWEIGHT. REPLACED NR 2 ENGINE PUMP PRESSURE SWITCH (4001JG1). LEAK AND OPERATIONS CHECKS GOOD REF AMM 29-11-17.

Part: WIRE — CHAFED (FIRE DETECTOR) · airframe 35,001 hrs · 5,283 cycles

NR 1 ENGINE FIRE LOOP B, FAULTED, COMBINED WITH OIL ODOR THROUGHOUT THE ACFT. EMERGENCY DECLARED LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. IAW TSM 26-12-00-810-936-A22, ACCOMPLISHED WIRE CHECKS FROM FDU 1 TO THE NR 1 ENG, MANIPULATED WIRING AT ALL LOCATIONS ON THE NR 1 ENGINE, AND AT TB 3801VT1. FOUND A CHAFED WIRE 1Z001R20, THREE INCHES FROM DETECTOR 4012WD. RAN REPLACEMENT WIRE PAIR FROM 3806VC-1 A TO DETECTOR 4012WD IAW AMM 70-71-40-300-801-A AND EA 280694. ACCOMPLISHED A SATISFACTORY OPS TEST AND BITE IAW AMM 26-12-00. REPLACED APU PER J/C 33L31549001. ACCOMPLISHED INITIAL T/S FOR SMOKE ODOR PER J/C 33L00021001. FOUND APU ISOLATORS BAD, REPLACED / PER AMM 49-12-42.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 34,788 hrs · 5,253 cycles

R1 DOOR EMERGENCY LIGHT POWER SUPPLY 12WL FAILED. REPLACED THE POWER SUPPLY IAW AMM 33-51-38.

Part: FCU — INOPERATIVE (APU) · airframe 33,889 hrs · 5,112 cycles

FLIGHT ATTENDENTS REPORTED A CABIN ODOR. AIRCRAFT WAS GROUNDED. REPLACED APU FCU.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,326 hrs · 5,006 cycles

AIRCRAFT WAS GROUNDED. EXIT SIGN LENS ABOVE R2 DOOR IS BROKEN. REPLACED EMERGENCY EXIT OVERHEAD SIGN.

Part: LIGHT — BROKEN (ROW 23D) · airframe 31,617 hrs · 4,754 cycles

ROW 23D EMERGENCY ROW LIGHT ASSEMBLY BROKEN. REPLACED ROW 23 EMERGENCY LIGHT ASSEMBLY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,617 hrs · 4,754 cycles

ROW 26G EMERGENCY LIGHT LENS MISSING. REPLACED LIGHT ASSEMBLY.

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 31,554 hrs · 4,743 cycles

FLIGHT ATTENDANTS IN AFT GALLEY/ AFT AIRCRAFT DETECTED AND ODOR OF ELECTRICAL FUMES. ISOLATED PROBLEM TO CABIN FANS. REPLACED LEFT RECIRCULATION FAN ASSEMBLY. AIRCRAFT WAS GROUNDED.

Part: FAN — FAILED (RECIRCULATION) · airframe 31,554 hrs · 4,743 cycles

FLIGHT ATTENDANTS IN AFT GALLEY, AFT AIRCRAFT DETECTED AND ODOR OF ELECTRICAL FUMES. ISOLATED PROBLEM TO CABIN FANS. REPLACED RT RECIRCULATION FAN ASSEMBLY. AIRCRAFT WAS GROUNDED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,403 hrs · 4,719 cycles

FOUND OVERHEAD CABIN EMERGENCY LIGHT BETWEEN 3F AND 3H INOP. REVERSED POLARITY. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,388 hrs · 4,717 cycles

L3 EMERGENCY LIGHT BATTERY REQUIRES REPLACEMENT. REPLACE THE BATTERY.

Part: COVER — BROKEN (DOOR HANDLE) · airframe 31,234 hrs · 4,692 cycles

L2 DOOR ASSIST HANDLE COVER DETACHED. ATTACHED THE ASSIST HANDLE COVER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,201 hrs · 4,688 cycles

EMERGENCY LIGHT LENS MISSING OUTSIDE LAVATORY L38. REPLACED THE LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,201 hrs · 4,688 cycles

EMERGENCY LIGHT LENS MISSING OUTSIDE LAVATORY L53. REPLACED THE LENS.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 31,099 hrs · 4,673 cycles

PRIMARY 1 FAULT ON RUNWAY AT CLEARED FOR TAKEOFF. TAXIED CLEAR OF RUNWAY TO RESOLVE FAULT. NO MAINTENANCE ACTION TAKEN.

Part: LIGHT — BROKEN (CABIN) · airframe 30,337 hrs · 4,561 cycles

ROW 20R AISLE EMERGENCY LIGHT BROKEN. REPLACED SEAT MOUNTED LIGHT AT SEAT 20 RIGHT.

Part: GIRT BAR — BENT (ZONE 800) · airframe 30,132 hrs · 4,512 cycles

AIRCRAFT WAS GROUNDED. 4L DOOR GIRT BAR BENT, DOOR WILL NOT CLOSE. ACCOMPLISHED TIME LIMITED REPAIR PER EA 268690.

Part: CONNECTOR — BROKEN (CABIN) · airframe 30,104 hrs · 4,505 cycles

AIRCRAFT WAS GROUNDED. SEAT 3H EMERGENCY LIGHT INOP. REPLACED SEAT 3H EMERGENCY LIGHT CONNECTOR.

Part: CASE — CORRODED (NR 1 COMPRESSOR) · airframe 29,938 hrs · 4,464 cycles

WHILE ACCOMPLISHING TERMINATING MONITOR, REMOVED LOWER ACCOUSTIC PANEL AND FOUND CORROSION ON THE LP COMPRESSOR CASE AT THE 6:00 O'CLOCK POSITION. REMOVED CORROSION THE COMPRESSOR CASE AND FOUND TO BE OUT OF LIMITS. MAINTENANCE REPLACED THE NR 1 ENGINE IAW JOB CARD 33L40071003.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 29,934 hrs · 4,463 cycles

CRACKED FORWARD CABIN L2 DOOR CEILING EXIT SIGN LENS. REPLACED THE LENS IAW AMM 33-51-17.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 29,727 hrs · 4,409 cycles

UNABLE TO DISARM L4 DOOR. CLEANED DEBRIS AT GIRT BAR RECEPTACLE. IAW AMM 52-13-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 29,471 hrs · 4,350 cycles

L4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED THE ASSIST BOTTLE IAW AMM 52-20-00. AIRCRAFT WAS GROUNDED.

Part: COVER — UNSECURE (CABIN) · airframe 29,232 hrs · 4,305 cycles

AIRCRAFT WAS NOT GROUNDED. RED COVER FELL OFF LAV L53 EMERGENCY EGRESS LIGHT. MAINTENANCE REINSTALLED COVER PER AMM 33-51-00.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR SLIDE) · airframe 29,166 hrs · 4,296 cycles

L1 DOOR ARMING LEVER WILL NOT GO FULLY TO ARM POSITION. REMOVED DEBRIS FROM GIRT BAR FITTING, DOOR ARMS AND DISARMS NORMAL IAW AMM 25-61-00.

Part: LENS — MISSING (CABIN) · airframe 28,936 hrs · 4,266 cycles

FOUND EMERGENCY LIGHT COVER (RED) ON WALL FORWARD OF DOOR 3L MISSING. REPLACED RED LIGHT COVER AT 3L. THE AIRCRAFT WAS NOT GROUNDED.

Part: FMU — DEFECTIVE (NR 1 ENGINE) · airframe 28,575 hrs · 4,221 cycles

AFTER TAKEOFF, THE FLIGHT CREW REPORTED THE NR 1 ENGINE WAS SLOW TO RESPOND AND THE DECISION WAS MADE TO DIVERT, LANDED SAFELY WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE LEFT ENGINE FUEL METERING UNIT AND ACCOMPLISHED A SATSTIFACTORY OPS CHECK IAW AMM 73-21-52.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,294 hrs · 4,184 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERATIVE, FORWARD OF THE R2 DOOR AT RT LAV VERTICAL. RESECURED LIGHT ASSY AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: PIN — UNSECURE (CABIN) · airframe 28,294 hrs · 4,184 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT FORWARD OF 2R DOOR AT BULKHEAD AISLE SIDE INOPERATIVE. SECURED PIN 7253VS-B IN REUSABLE CONNECTOR, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,397 hrs · 4,044 cycles

AIRCRAFT WAS NOT GROUNDED, EMERGENCY FLASHLIGHT INOPERATIVE AT DOOR 2 LT F/A JUMPSEAT STOWAGE. REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 14WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

EMERGENCY POWER SUPPLY 13WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 15WL BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 16WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGNECY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 12WL, BATTERY FAILED CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 17WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

POWER SUPPLY 18WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 27,292 hrs · 4,027 cycles

EMERGENCY POWER SUPPLY 11WL, BATTERY FAILED CABIN EMER LIGHTING BATTERY CAPACITY CHECK IAW A CHECK TASK CARD 33C20033002. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400.

Part: BRAKE — FIRE (MLG) · airframe 26,516 hrs · 3,896 cycles

AIRCRAFT WAS GNDED. AT ARRIVAL & PARKING RAMP REPORTED NR 5 BRAKE FIRE, EXTINGUISHED WITHOUT EXTINGUISHING AGENT, BRAKE TEMP SHOWED 605 DEGREES. PERFORMED BRAKE OVERHEAT INSPECTION & REPLACED NR 5 WHEEL & BRAKE ASSEMBLY IAW AMM 05-51-16-200-801-A, 32-41-11-000-801-A & 32-42-27-000-801-A. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA 201603309006 FOR ADDITIONAL PART.

Part: WHEEL — DAMAGED (MLG) · airframe 26,516 hrs · 3,896 cycles

AIRCRAFT WAS GNDED. AT ARRIVAL & PARKING, RAMP REPORTED NR 5 BRAKE FIRE, EXTINGUISHED WITHOUT EXTINGUISHING AGENT, BRAKE TEMP SHOWED 605 DEGREES. PERFORMED BRAKE OVERHEAT INSPECTION & REPLACED NR 5 WHEEL & BRAKE ASSEMBLY IAW AMM 05-51-16-200-801-A, 32-41-11-000-801-A & 32-42-27-000-801-A. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SEE AALA 201603309002 FOR ADDITIONAL PART.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,198 hrs · 3,817 cycles

DIVERTED, ACFT WAS GNDED. ODOR IN CABIN REPORTED AROUND DOORS L2 & R2 WHICH SMELLED LIKE DE-ICE FLUID & RESULTED IN 2 CREW MEMBERS BECOMING ILL. ACCOMPLISHED TASK CARD 33L00021001, NO ODOR PRESENT FROM APU, OR EITHER ENG. BLEED SOURCE CHECKED OK & THE DRAINS AT THE L2 & R2 DOORS WERE CLEAR. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — MISINSTALLED (CABIN) · airframe 26,194 hrs · 3,815 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN AT 3R DOOR IS INSTALLED UPSIDE DOWN. INSTALLED EXIT SIGN TO PROPER POSITION.

Part: COVER — MISSING (CABIN) · airframe 25,923 hrs · 3,737 cycles

AIRCRAFT WAS NOT GNDED. COVER PLATE DISPLAYING EXIT MISSING CEILING AND WALL AT 3L DOOR. R & R CEILING & WALL EXIT LIGHT COVER PLATES.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 25,833 hrs · 3,724 cycles

AIRCRAFT WAS NOT GNDED. MID GALLEY ACFT RT EMER EXIT SIGN LOOSE & FELL OFF. REPLACED EMER EXIT LENS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — DEFECTIVE (FUEL SYSTEM) · airframe 25,833 hrs · 3,724 cycles

AIRCRAFT WAS NOT GNDED. FUEL TRIM LINE FAULT ECAM ON DESCENT. REPLACED TRIM TANK ISOLATION VLV ACTUATOR. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-27-52-000-802-A & 28-27-54-400-802-A.

Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 25,833 hrs · 3,724 cycles

ACFT LT MID GALLEY EMER LIGHT NEAR COMPARTMENT 3 - 14 LOOSE & MISSING SCREW. TIGHTENED LOOSE HARDWARE & REPLACED MISSING HARDWARE AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 25,421 hrs · 3,629 cycles

EMERGENCY ESCAPE PATH LIGHT ON LAVATORY L53 MISSING LENS. INSTALLED LENS ON LAVATORY L53 EMER LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-12-000-816-A & 33-51-12-400-816-A.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,336 hrs · 3,616 cycles

R2 DOOR EMER EXIT SIGN INOPERATIVE. REPLACED R2 DOOR EMER EXIT LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-16.

Part: CONNECTOR — LOOSE (ZONE 800) · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, EMER EXIT DOOR L3 SHOWS, SLIDE ARMED LIGHT, DURING DOOR OPENING. REMOVED L3 DOOR SLIDE IAW AMM 25-62-41, RESET PLUG 35MJ IAW AMM 52-71-12. OPERATIONS TESTED GOOD IAW AMM 52-71-00. REINSTALL SLIDE IAW AMM 25-62-41 CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON DOOR SILL, BETWEEN FRAME 73A & 75A AT Y210. REPLACED DOOR SILL IAW SRM 53-41-14 & 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON L4 DOOR SILL SUPPORT SHIM, BETWEEN FRAME 74 & 75 AT +Y2462. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON L4 DOOR SILL SUPPORT SHIM, BETWEEN FRAME 75 & 76 AT +Y2462. REPLACED SHIM IAW SRM 51-42-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON L4 DOOR SILL SUPPORT SHIM, BETWEEN FRAME 73 & 74 AT +Y2462. REPLACED SHIM IAW SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN FLOOR STRUCTURE PROFILE Z SUPPORT, BETWEEN FRAME 75 & 76 AT +Y2462. REPLACED PROFILE Z SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN SEAT TRACK, BETWEEN FRAME 73 & 74 AT +Y2462. REPLACED SEAT TRACK IAW SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN SEAT TRACK, BETWEEN FRAME 73 & 74 AT +Y1137. REPLACED SEAT TRACK IAW SRM 53-00-15 FIG 101 & 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN FLOOR STRUCTURE PROFILE Z SUPPORT AT FRAME 78 & +Y2462. REPLACED PROFILE Z SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN SEAT TRACK, BETWEEN FRAME 73 & 74 AT +Y1447. REPLACED SEAT TRACK IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,301 hrs · 3,609 cycles

S1 CHECK, CORROSION ON CABIN SEAT TRACK, BETWEEN FRAME 47 & 53.2 AT -Y450. REPLACED SEAT TRACK IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 25,241 hrs · 3,601 cycles

FLIGHT 786 FORWARD LAVATORY FLOOR IS SPONGY. REPLACED THE LAVATORY FLOOR PAN MOON MAT COVERING IAW AMM 25-28-42.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 24,101 hrs · 3,462 cycles

4R AFT FACING JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED GALLEY PACK. OPERATIONS CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 23,823 hrs · 3,427 cycles

EXIT SIGN IN AISLE 3R DOOR FELL DOWN ON TAKEOFF. SECURED EXIT SIGN IN AISLE 3R DOOR. OPERATIONAL CHECKED WITH NO DEFECTS NOTED.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 23,793 hrs · 3,423 cycles

3R EMER EXIT SIGN LENS FELL OFF. RE-INSTALLED 3R EMER EXIT SIGN LENS.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 23,015 hrs · 3,315 cycles

EPSU BATTERY FAILS TEST. REPLACED EPSU BATTERY ON EPSU 13WL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,481 hrs · 3,219 cycles

FLIGHT 1728, AFTER TAKEOFF CABIN & COCKPIT CREW HAD UNUSUAL ODOR COMING FROM CABIN & COCKPIT, SEEMED TO SUBSIDE IN CABIN WHILE IN CRUISE, BUT REMAINED SOMEWHAT STRONG IN THE COCKPIT. THE FLIGHT CREW WENT ON OXYGEN, WHILE IN DESCENT STRONG ODOR RETURNED AGAIN TO CABIN. MAINTENANCE RAN BOTH THE LEFT AND RIGHT ENGINE WITH NO ODOR DETECTED.

Part: SIGN — DETACHED (CABIN) · airframe 22,379 hrs · 3,201 cycles

EMERGENCY EXIT SIGN ABOVE 3R DOOR NEEDS REATTACHED. ATTACHED EMER EXIT SIGN ABOVE 3R DOOR.

Part: COVER — UNSECURE (CABIN) · airframe 22,097 hrs · 3,143 cycles

EXIT LIGHT COVER 1R WILL NOT STAY ON. SECURED EMER EXIT LIGHT COVER 1R.

Part: SIGN — DETACHED (CABIN) · airframe 22,070 hrs · 3,133 cycles

EXIT SIGN & 3R FELL OFF. REATTACHED EXIT SIGN AT 3R.

Part: SIGN — BROKEN (CABIN) · airframe 21,916 hrs · 3,101 cycles

3R EXIT SIGN BROKEN 3R DOOR. REINSTALLED 3R EXIT SIGN, CHECKED OK.

Part: RIB — CRACKED (RT WING) · airframe 20,404 hrs · 2,847 cycles

CRACK FOUND IN RT WING RIB 6. REPLACED RIB IAW EA 1051997A, 105998, 105999, 106000 & 106049.

Part: OVEN — DIRTY (GALLEY) · airframe 20,404 hrs · 2,847 cycles

NUMBER 3 OVEN, REAR GALLEY, CREATES STRONG ODOR OF MELTING PLASTIC WHEN OPERATING. CLEANED OVEN.

Part: OVEN — CONTAMINATED (GALLEY)

ON DEPARTURE FROM TLV A FUME REPORT WAS GIVEN TO THE FLIGHT CREW. FUMES WERE REPORTED IN THE REAR OF ACFT CAUSING BURNING EYES & THROATS. DIVERTED TO ATHENS. REPLACED GALLEY 6 POSITION 1 & 2, & GALLEY 7 POSITION 1 OVENS.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 20,207 hrs · 2,819 cycles

L4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L4 DOOR ASSIST BOTTLE TO REQUIRED LEVEL.

Part: LIGHT — BURNED (CABIN) · airframe 20,162 hrs · 2,813 cycles

FLIGHT ATTENDANTS REPORTED A MELTING PLASTIC SMELL IN FWD GALLEY DURING TAKEOFF. PERFORMED A330 TROUBLESHOOT CABIN AIR QUALITY JOB CARD. INSPECTED FWD CABIN, LAVATORIES, GALLEYS & CREW REST AREAS FOR SOURCE OF REPORTED SMELL, NONE FOUND. DID INSPECTION OF CABIN SEATS, IFE SYS & MONITORS. ALL FOUND WORKING SATISFACTORY. FOUND CEILING LIGHTS AT ROW 3E & 1L DOOR WITH BURNT LIGHT BULBS, WHICH WERE CHANGED & OPERATES NORMAL. INSPECTED FWD E & E & CARGO BIN NO DEFECTS.

Part: ACTUATOR — INOPERATIVE (L4 DOOR) · airframe 19,939 hrs · 2,773 cycles

PHL L4 DOOR ASSIST BOTTLE PRESS GAGE INOPERATIVE. R & R DOOR ASSIST ACTUATOR .

Part: COVER — BROKEN (EXIT SIGN) · airframe 19,901 hrs · 2,765 cycles

3L EMERGENCY EXIT SIGN COVER BROKEN, FALLS OFF SUPPORT. R & R 3L EMERGENCY EXIT SIGN COVER.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,501 hrs · 2,697 cycles

WHILE ACCOMPLISHING JC 33C22033002. FOUND EPSU, 12WL, BATTERY INOPERATIVE. R & R EPSU, 12WL, BATTERY SYS TESTED IS GOOD.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 18,883 hrs · 2,589 cycles

ENVOY CLASS SEATS, SEVERAL EMERGENCY ESCAPE PATH LIGHTING ARE NOT PROJECTING ON THE FLOOR. REPOSITIONED SEVERAL EMERGENCY ESCAPE PATH LIGHTING IAW A330 AMM 33-51-12.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY POWER SUPPLY UNITS 11WL, 16WL, 15WL & 17WL FAILED CABIN EMERGENCY LIGHTING BATTERY CAPACITY TEST. R & R EPSU BATTERIES AT 11WL, 16WL, 15WL & 17WL.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 18,667 hrs · 2,541 cycles

2L DOOR ASSIST BOTTLE HAS LOW PRESS. SERVICED 2L DOOR ASSIST CYLINDER.

Part: LENS — MISSING (CABIN) · airframe 18,528 hrs · 2,518 cycles

D3L EMERGENCY LIGHTING RED LENS MISSING. REPLACED RED LENS.

Part: LENS — MISSING (CABIN) · airframe 18,172 hrs · 2,447 cycles

EMERGENCY LIGHT LENS COVER MISSING A/C LT. REPLACED EMERGENCY LIGHT LENS COVER AS REQUIRED A/C LT, LIGHT OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,970 hrs · 2,409 cycles

L1 ENTRY DOOR F/A SEAT FLASHLIGHT BATTERY DISCHARGED. MAINTENANCE REPLACED THE BATTERY. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (ZONE 800)

DOOR ASSIST HAS LOW PRESSURE. MAINTENANCE ACCOMPLISHED CHARGING OF DOOR DAMPER EMERGENCY ACTUATOR.

Part: BOTTLE — LOW PRESSURE (ZONE 800)

DOOR PRESSURE MESSAGE FOUND ON FAP 2L. MX ADJUSTED 2L DAMPER PRESSURE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 17,683 hrs · 2,361 cycles

FWD CIDS PANEL INDICATES CHECK DOOR PRESSURE ON SLIDE AT DOOR 2L. MAINTENANCE 2L DOOR DAMPER CYLINDER SERVICED TO GREEN ZONE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR ASSIST) · airframe 17,517 hrs · 2,339 cycles

L2 DOOR PRESSURE LOW AT DEPARTURE. SERVICED L2 DOOR PRESSURE. OPS AND INDICATIONS NOW NORMAL.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 16,878 hrs · 2,262 cycles

AREA OF DELAMINATION ON HEATED FLOOR PANEL 112DS AT R4 DOOR ENTRYWAY. REPLACED FLOOR PANEL 112DS IAW EA 105052.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 16,878 hrs · 2,262 cycles

AREA OF DELAMINATION ON HEATED FLOOR PANEL 38DS AT R4 DOOR ENTRYWAY. REPLACED FLOOR PANEL 38DS IAW EA 105052.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 16,878 hrs · 2,262 cycles

AREA OF DELAMINATION ON HEATED FLOOR PANEL 40DS AT R4 DOOR ENTRYWAY. REPLACED FLOOR PANEL 40DS IAW EA 105052.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 16,702 hrs · 2,241 cycles

EMERGENCY LIGHT AT L3 DOOR MISSING LENS. MX FOUND LENS UNDER SEAT. INSTALLED LENS, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,992 hrs · 2,145 cycles

1A EMERGENCY FLASHLIGHT INOPERATIVE. MX R & R EMERGENCY FLASH LIGHT BATTERY.

Part: LENS — MISSING (CABIN) · airframe 15,787 hrs · 2,119 cycles

ON WALK AROUND, FOUND L53 EMERGENCY ESCAPE PATH LIGHT RED LENS MISSING. MX REPLACED L53 EMERGENCY ESCAPE PATH LIGHT RED LENS.

Part: LENS — MISSING (CABIN) · airframe 14,656 hrs · 1,961 cycles

MTC REPORTED THE CEILING MOUNTED EMERGENCY EXIT LIGHT LENS WAS MISSING NEAR THE R3 DOOR. MAINTENANCE REPLACED LENS.

Part: LENS — MISSING (CABIN) · airframe 14,343 hrs · 1,913 cycles

LENS MISSING FROM EMERGENCY EXIT PATH LIGHT ON AFT CORNER OF LAVL53. MAINTENANCE INSTALLED LENS ON L53 LAV AFT EE LIGHT ASSEMBLY, OPERATIONAL CHECK IS OK.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 13,308 hrs · 1,743 cycles

FLIGHT 754, PHL-CDG - THE CREW REPORTED A STRONG ODOR THROUGHOUT THE CABIN AND COCKPIT ESPECIALLY IN THE AFT. THE CREW AND SOME PASSENGERS EXPERIENCED SOME THROAT AND LUNG IRRITATION. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT CABIN AIR QUALITY, BLEED AIR ANALYSIS, AND ENGINE CABIN ODOR ON LEFT AND RIGHT ENGINES. THE RIGHT ENGINE WAS REMOVED AND REPLACED AND THE RIGHT ENGINE IP CHECK VALVE.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 13,251 hrs · 1,736 cycles

FLIGHT 796, PHL - TLV - FLIGHT ATTENDANT REPORTED AFT GALLEY OVEN NR 2 POS 6-12 WAS EMITTING HIGH HEAT FROM FRONT SIDES AND TOP OF OVEN. LONG AFTER ELECTRICAL POWER WAS REMOVED AND CONTINUED TO INCREASE. FLIGHT ATTENDANT EXPENDED 1 FIRE EXTINGUISHER INSIDE OPEN DOOR OF OVEN AND TEMPERATURE CONTINUED TO ESCALATE. ELECTRICAL SMOKE WAS LIGHT AND PRESENT. THE AIRCRAFT LANDED AT NEAREST SUITABLE AIRPORT (YQM). YQM MAINTENANCE REPLACED USED FIRE EXTINGUISHER AND ELECTRICALLY DISCONNECTED BOTH OVENS AND THE CIRCUIT BREAKERS PULLED FOR FERRY FLIGHT TO PHL. PHL MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY OVENS 6-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,234 hrs · 1,733 cycles

CABIN AFT LEFT JUMPSEAT FLASHLIGHT (4L) DOOR INOPERATIVE. MAINTENANCE INSTALLED NEW BATTERY AND SAFETY STRAP ON AFT JUMP SEAT FLASHLIGHT, OPERATIONAL CHECK IS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,091 hrs · 1,594 cycles

DURING CRUISE FLIGHT ATTENDANT AND SEVERAL PASSENGERS DETECTED ODOR NEAR ROW 14AC. AN ON BREAK PILOT DETECTED NO ODOR. DURING LATER PORTION OF FLIGHT TWO OTHER PILOTS DETECTED NO ODOR. DURING DESCENT, FLIGHT ATTENDANT ADVISED 3 OTHER FLIGHT ATTENDANTS EXPERIENCING HEADACHES AND NAUSEA. 1 FLIGHT ATTENDANT UTILIZED OXYGEN & WAS MET BY PARAMEDICS FOR EVALUATION. WE WERE INFORMED THESE SYMPTOMS WERE EXPERIENCED BY THE 3 FLIGHT ATTENDANTS WORKING LEFT SIDE OF A/C. THEY INDICATED NO ODOR PRESENT AT THAT TIME. MAINTANCE RAN AIRCRAFT WITH PACKS AND ALL ELECTRICAL POWER FOR APPROXIMATELY 12 HOURS, NO SMELL OR ODORS NOTED AT THIS TIME.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 11,496 hrs · 1,523 cycles

CEILING EMERGENCY LIGHT INOPERATIVE 2F. MAINTENANCE FOUND WIRES NOT CEMENTED PROPERLY. RE-INSTALLED WIRES, OPERATIONAL CHECK IS GOOD.

Part: SIGN — UNSECURE (CABIN)

EXIT SIGN AC RIGHT BY 3R DOOR FALLING OFF MOUNTING. MAINTENANCE FOUND EXIT SIGN AND RE-INSTALLED AT DOOR 3R. FUNCTION SATISFIED.

Part: LIGHT — ILLUMINATED (CABIN) · airframe 10,553 hrs · 1,403 cycles

EMERGENCY LIGHTS 2R OVERHEAD LIGHTS WILL NOT EXTINGUISH DURING FLIGHT. MAINTENANCE RESET CIDS 1 AND 2. EMERGENCY LIGHTS OPERATIONAL TEST WITH EMERGENCY LIGHT SWITCH. OPERATES SATISFACTORY, NO FURTHER ACTION TAKEN.

Part: SIGN — DETACHED (CABIN) · airframe 9,307 hrs · 1,245 cycles

LHR - EXIT SIGN AT ROW 22 FELL OFF CEILING. MAINTENANCE - EXIT PANELS RE-FITTED NOW SERVICEABLE.

Part: SEAT BACK — DEFECTIVE (COCKPIT) · airframe 7,881 hrs · 1,059 cycles

LHR - CAPTAIN'S SEAT WHEN RECLINE LEVER IS ACTIVATED, THE SEATBACK FLOPS BACK TO FULL RECLINE. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SEAT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,686 hrs · 1,031 cycles

MUC - EMERGENCY FLASHLIGHT NO LED FLASH AT DOOR 1L, FWD INBOARD FLIGHT ATTENDANT POSITION. MAINTENANCE REMOVED AND REPLACED 1L DOOR EMERGENCY FLASHLIGHT AND BATTERY, OPS CHECK OK, REF MM 25-60-00, THIS CLEARS MEL 25-65-01A CONTROL NUMBER 0431C14.

Part: WHEEL — DEFECTIVE (MLG)

PHL - FLT 729 EN-ROUTE LHR TO PHL. APPROXIMATELY ONE HOUR UNTIL LANDING, THE NUMBER FOUR TIRE PRESSURE 180 PSI GENERATED ON ECAM. THE CREW FOLLOWED QRH PROCEDURES, AND DECLARED AN EMERGENCY AS A PRECAUTION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE NUMBER FOUR MAIN LANDING GEAR TIRE WAS BELOW RE-INFLATION LIMIT. REMOVED AND REPLACED NUMBER FOUR MAIN WHEEL ASSEMBLY.