N280AY

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 42,370 hrs · 6,340 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS 3R FLASH LIGHT BATT LOW. REPLACED BATTERY IN 3R FLASHLIGHT AND STRAP. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,896 hrs · 6,211 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ODOR IN CABIN. ON DESCENT FA AT 3L DOOR PUT ON OXYGEN MASK BECAUSE SMELL WAS SO BAD. LIGHT MUSTY SMELL ON TAKE OFF, NOT ENOUGH FOR OXYGEN MASK. MAINTENANCE ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLESHOOTING IAW JOB CARD 33L00021001 WITHOUT FINDINGS. NO EVIDENCE OF OIL OR FLUID LEAK. ENG + APU OIL LEVELS OK.

Part: AMU — FAILED (ZONE 100) · airframe 41,756 hrs · 6,192 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS HF DOES NOT TRANSMIT ON EITHER RADIO. RECIEVE IS OK ON BOTH. PROBLEM SURFACED AFTER ENCOUNTER WITH MODERATE TURBULENCE. MAINTENANCE PERFORMED TSM TASK 23-141-00-810-819A. BOTH HF TRANSMISSION FAILS. REMOVED AND REPLACED AMU IAW AMM 23-51-34. OPS TEST GOOD.

Part: CLOSEOUT PANEL — CRACKED · airframe 41,182 hrs · 6,119 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND MAIN LANDING GEAR FALSE SPAR CLOSEOUT PANEL NEXT TO AFT GEAR TRUNNION CRACKED. REPLACED PANEL PER AMM 57-51-15.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,924 hrs · 6,084 cycles

AIRCRAFT WAS NOT GROUNED: EMERGENCY FLASHLIGHT AT DOOR 4L INOPERATIVE. MAINTENANCE REPLACED FLASHLIHGT PER STANDARD PRACTICES.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 40,476 hrs · 6,023 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF #1 ENGINE BLEED FAULT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED #1 ENG PRV BLEED VALVE IAW AMM 36-11-52. LEAK AND OPS CHECKS GOOD.

Part: TIRE — FAILED (NR 4 MLG) · airframe 40,476 hrs · 6,023 cycles

AIRCRAFT WAS GROUNDED: DURING AN OVERWEIGHT LANDING, THE #4 MLG TIRE BURST AND CAUSED DAMAGE TO THE RH INBOARD FLAP AND ACOUSTIC LINER AND LINER SUPPORT BRACKET ATTACH POINT ON THE RH ENGINE. MAINTENANCE REMOVED AND REPLACED NBR 4 MAIN WHEEL AND TIRE ASSY IAW AMM 32-41-11-000-801A. ALL CHECKS OK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 37,744 hrs · 5,554 cycles

LAVATORY SMOKE MESSAGE ACTIVATED MOMENTAILY, SELF CLEARED, UNCONFIRMED. PREFORMED AN OPS CHECK OF THE LAVATORY SMOKE DETECTOR IAW AMM 26-17-00, OPS CHECKED GOOD.

Part: GIRT BAR — DIRTY (R4 DOOR SLIDE) · airframe 35,276 hrs · 5,177 cycles

R4 SLIDE DIFFICULT TO ARM-DISARM. REMOVED DEBRIS FROM THE GIRT BAR.

Part: SLIDE — LOW PRESSURE (R3 DOOR) · airframe 35,141 hrs · 5,143 cycles

R3 DOOR HAD A CAUTION FOR LOW SLIDE PRESSURE, THE AIRCRAFT WAS GROUNDED. REPLACED R3 SLIDE ASSEMBLY.

Part: SEAT TRACK — CORRODED (FRAME 71) · airframe 35,005 hrs · 5,123 cycles

CORROSION FOUND ON THE SEAT TRACK, Y450 AT FRAME 71. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11.

Part: SEAL — LEAKING (STARTER CLUTCH) · airframe 34,255 hrs · 5,014 cycles

ODOR IN CABIN AND FLIGHT DECK DURING DESCENT. FLIGHT ATTENDANTS AND COCKPIT CREW BOTH CONFIRMED A STRONG ODOR. REPLACED THE STARTER CLUTCH SEAL. AIRCRAFT WAS GROUNDED.

Part: LENS — BROKEN (EXIT SIGN) · airframe 33,950 hrs · 4,972 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT SIGN 3L FELL OFF. REPLACED 3L EXIT SIGN LENS.

Part: BATTERY — FAILED (CABIN) · airframe 33,681 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED. EPSU BATTERY AT 3L (15WL) FAILED TEST. REPLACED BATTERY AT 15WL POWER SUPPLY.

Part: BATTERY — FAILED (CABIN) · airframe 33,681 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED. DURING EPSU BATTERY CAPACITY TEST DOOR 2R (14WL) FAILED TEST. REPLACED EPSU BATTERY 14WL.

Part: BATTERY — FAILED (CABIN) · airframe 33,681 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED. DURING EPSU BATTERY CAPACITY TEST DOOR 3R (16WL) FAILED TEST. REPLACED EPSU BATTERY 16WL.

Part: BATTERY — FAILED (CABIN) · airframe 33,681 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED. EPSU BATTERY AT 1L (11WL) FAILED TEST. REPLACED BATTERY AT 11WL POWER SUPPLY.

Part: GIRT BAR — DIRTY (R4 DOOR SLIDE) · airframe 32,877 hrs · 4,819 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR SLIDE SHOWS ARMED WITH LEVER IN DISARMED POSITION. REMOVED DEBRIS FROM GIRT BAR AREA.

Part: OVEN — SMOKE (GALLEY) · airframe 32,705 hrs · 4,796 cycles

OVEN STARTED SMOKING. NO FIRE OR FOOD SOURCE. REPLACED THE OVEN.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,267 hrs · 4,728 cycles

EMERGENCY LIGHT AT ROW 26HG HAS BROKEN LENS. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — BROKEN (CABIN) · airframe 32,252 hrs · 4,726 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHT AT LAV L38 IS BROKEN. LIGHT ASSEMBLY IN LAVATORY L38 WAS REPLACED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,937 hrs · 4,658 cycles

EMERGENCY FLASHLIGHT AT THE R4 DOOR FOUND USED AND REPLACED INCORRECTLY, BATTERY DISCHARGED. REPLACED BATTERY AND RESTOWED THE FLASHLIGHT CORRECTLY. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COFFEEMAKER — ODOR (FUSELAGE) · airframe 31,682 hrs · 4,576 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED DURING DECENT AND APPROACH DETECTED AN ODOR LIKE BURNT METAL ON TOAST, BETWEEN ROW 6-7, OF THE MID CABIN. MAINTENANCE NOTED SMELL IN MID GALLEY OVEN AND EXPRESSO MAKER AREAS. 2 MID GALLEY OVENS, 2 COFFEE MAKERS AND 2 EXPRESSO MAKERS WERE INSPECTED AND REPLACED. AMTS NOTED NO WIRING DEFECTS IN THE MID GALLEYS THEMSELVES. NO ODORS NOTED AFTER COMPONENTS WERE REPLACED. (SEE AALA201701179017 (COFFEEMAKER), AALA201701179018 (OVEN) & AALA201701179019 (ESPRESSO MAKER)

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 31,682 hrs · 4,576 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED DURING DECENT AND APPROACH DETECTED AN ODOR LIKE BURNT METAL ON TOAST, BETWEEN ROW 6-7, OF THE MID CABIN. MAINTENANCE NOTED SMELL IN MID GALLEY OVEN AND EXPRESSO MAKER AREAS. 2 MID GALLEY OVENS, 2 COFFEE MAKERS AND 2 EXPRESSO MAKERS WERE INSPECTED AND REPLACED. AMTS NOTED NO WIRING DEFECTS IN THE MID GALLEYS THEMSELVES. NO ODORS NOTED AFTER COMPONENTS WERE REPLACED. (SEE AALA201701179017 (COFFEEMAKER), AALA201701179018 (OVEN) & AALA201701179019 (ESPRESSO MAKER)

Part: OVEN — ODOR (GALLEY) · airframe 31,682 hrs · 4,576 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED DURING DECENT AND APPROACH DETECTED AN ODOR LIKE BURNT METAL ON TOAST, BETWEEN ROW 6-7, OF THE MID CABIN. MAINTENANCE NOTED SMELL IN MID GALLEY OVEN AND EXPRESSO MAKER AREAS. 2 MID GALLEY OVENS, 2 COFFEE MAKERS AND 2 EXPRESSO MAKERS WERE INSPECTED AND REPLACED. AMTS NOTED NO WIRING DEFECTS IN THE MID GALLEYS THEMSELVES. NO ODORS NOTED AFTER COMPONENTS WERE REPLACED. (SEE AALA201701179017 (COFFEEMAKER), AALA201701179018 (OVEN) & AALA201701179019 (ESPRESSO MAKER)

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 31,671 hrs · 4,569 cycles

AIRCRAFT WAS NOT GROUNDED. 4R DOOR SLIDE, ARMS BUT LEVER ONLY MOVES 1/4 INCH. MAINTENANCE REMOVED DEBRIS FROM GIRT BAR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: ENGINE — ODOR (NR 1) · airframe 31,669 hrs · 4,568 cycles

F/A REPORTS WET SOCKS MUSTY ODOR WORST AT 2L DOOR. ODOR SEEMED TO GET LESS WITH RIGHT PACK OFF. TURNED RT BLEED OFF. ODOR CAME BACK AT LOW THRUST IN DECENT. MAINTENANCE REPLACED THE NR 1 ENGINE IAW TASK CARD 33L40071003 AND THE APU IAW TASK CARD 33L31549001.

Part: APU — ODOR (APU BAY) · airframe 31,669 hrs · 4,568 cycles

FLIGHT ATTENDANT REPORTS WET SOCKS, MUSTY ODOR WHICH IS WORSE AT L2 DOOR. ODOR SEEMED TO GET LESS WITH RIGHT PACK OFF. TURNED RIGHT BLEED OFF. ODOR CAME BACK AT LOW THRUST DURING DESENT. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE NR 1 ENGINE AND THE APU.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 31,666 hrs · 4,566 cycles

CORROSION ON SEAT TRACK AT YB1 BETWEEN FRAMES 73 AND 74. REPLACED THE SEAT TRACK IAW SRM 51-42-11-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,666 hrs · 4,566 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT YC1, 10 INCHES AFT OF FR 73. REPLACED SEAT TRACK PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 72-74) · airframe 31,666 hrs · 4,566 cycles

CORROSION ON SEAT TRACK FITTING AT -Y1137.1 BETWEEN FRAMES 72 AND 74. REPLACED THE SEAT TRACK IAW SRM 53-41-15 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 72-74) · airframe 31,666 hrs · 4,566 cycles

CORROSION ON SEAT TRACK AT -Y1447.8 BETWEEN FRAMES 72 AND 74. REPLACED THE SEAT TRACK IAW SRM 53-41-15 AND SRM 51-42-11.

Part: AIR FILTER — CONTAMINATED (ZONE 100) · airframe 31,654 hrs · 4,557 cycles

5 MINS FROM LANDING F/A'S IN BACK OF A/C SAID THE SMELLED FUMES. MAINTENANCE ACTION PENDING. THE AIRCRAFT WAS GROUNDED. R&R HEPA FILTER AND C/W J/C 21-00-00-615-807-A, DECONTAMINATION OF ECS.

Part: ENGINE — ODOR (NR 2) · airframe 31,651 hrs · 4,555 cycles

AIRCRAFT EXPERIENCED A DIRTY SOCK ODOR DURING APPROACH TO MIA. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS CURRENTLY OUT OF SERVICE. THE AIRCRAFT WAS GROUNDED. TROUBLESHOT CABIN ODOR TO THE NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE. OPS AND LEAK CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 30,709 hrs · 4,413 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS MISSING AT RT AFT LAV. REPLACED LENS COVER.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 30,112 hrs · 4,329 cycles

EMERGENCY EXIT LIGHT AT SEAT 18B INOPERATIVE. MAINTENANCE FOUND EMERGENCY EXIT LIGHT CONNECTOR FOR SEAT 18 A-B DISCONNECTED AT FLOOR. RECONNECTED LIGHT CONNECTOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 29,971 hrs · 4,309 cycles

R4 DOOR SLIDE WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR TRACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 29,684 hrs · 4,267 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 23G EMERGENCY LIGHT LENS MISSING. REPLACED SEAT 23G EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-12.

Part: LENS — BROKEN (CABIN) · airframe 29,545 hrs · 4,247 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT LENS COVER IS BROKEN AT LAVATORY L38. REPLACED LENS COVER.

Part: LENS — MISSING (CABIN) · airframe 28,730 hrs · 4,105 cycles

AIRCRAFT WAS NOT GNDED. DURING DAILY CHECK, FOUND 3R CROSS AISLE EMER LIGHT RED LENS MISSING. REPLACED LENS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 27,824 hrs · 3,888 cycles

RECEIVED ECAM SMOKE, LAVATORY SMOKE, FOR ONE MINUTE AT CRUISE. MX FOUND NO MESSAGES. ACCOMPLISHED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION SYS IAW AMM 26-17-00-710-802-A, WITH NO FAULTS NOTED.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 27,399 hrs · 3,818 cycles

FUEL AFT TRANSFER VLV INOPERATIVE. REPLACED FUEL INLET VLV ACTUATOR 603QL2. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-26-53-401.

Part: SIGN — BROKEN (CABIN) · airframe 27,396 hrs · 3,817 cycles

OVERHEAD EMER EXIT SIGN IN AISLE, BEHIND LAVATORY L61, HOUSING BROKEN. REPLACED EMER EXIT LIGHT ASSEMBLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EXIT SIGN) · airframe 26,738 hrs · 3,727 cycles

EXIT SIGN LENS IN AISLE, AT 3L DOOR MISSING. INSTALLED NEW EXIT SIGN LENS ON 3L DOOR IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 25,567 hrs · 3,579 cycles

EXIT SIGNS NEAR 3F FELL DOWN. SECURED EXIT SIGNS NEAR 3F AS REQUIRED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 25,279 hrs · 3,545 cycles

DURING CABIN EMER LIGHTING BATTERY CAPACITY CHECK, EXIT SIGN EPSU 14WL, DOOR 2 FAILED. REPLACED THE EPSU 14WL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, FLOOR PANEL 4E4643-4 IS DELAMINATED. NEW PANEL FABRICATED IAW EA 506180.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, FLOOR PANEL PART 4E4640-6 WAS FOUND DELAMINATED. NEW PANEL FABRICATED IAW EA 506180.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

1S CHECK, AFT CABIN DOOR SILL FLOOR PANEL 271LF CORRODED. REPLACED PANEL 271LF IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

1S CHECK, CABIN SEAT TRACK AT Y-1552.5, FRAME 33 HAS CORROSION. R & R DAMAGED SEAT TRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

1S CHECK, CORROSION ON FLOORBEAM BETWEEN FRAME 75 & 76 AT STRINGER 26R. R & R FLOORBEAM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 33 - 34 AT BL -Y1959. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 & SRM 51-44-11.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, GALVANIC CORROSION ON FLOOR SUPPORT SHIM BETWEEN FRAME 75 - 76 AT BL Y2462. REPLACED SHIM IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FRAME 75 - 76 AT STRINGER 26L. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 73 TO 74 AT BL -Y1660. REPLACED SEAT TRACK IAW SRM 53-41-15, SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FRAME 75 - 76 AT STRINGER 26R. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORROSION ON SEAT TRACK BETWEEN Y+1959 - Y+1456 AT FRAME 33. REMOVED CORROSION, R & R SEAT TRACK AT BL Y+1552.5, FRAME 33 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORROSION ON FLOORBEAM AT FRAME 74, BL -Y1137.1. REPLACED FLOORBEAM AT FRAME 74, BL -Y1137.1 IAW SRM 53-41-14, SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORROSION ON SEAT TRACK BETWEEN FRAME 68 - 72 AT BL -Y450. REPLACED SEAT TRACK BETWEEN FRAME 68 - 72 AT BL -Y450 IAW SRM 53-00-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED FLOORBEAM BETWEEN FRAME 75 & 76 AT Y450. REPLACED FLOORBEAM IAW SRM 53-41-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, FWD CABIN FLOOR PANEL 242HF HAS SURFACE DAMAGE. FABRICATED PANEL 242HF IAW SRM 53-02-00 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED SEAT TRACK BETWEEN FRAME 73 - 74 AT -Y1250. REPLACED SEAT TRACK BETWEEN FRAME 73 - 74 AT -Y1250 IAW SRM 53-41-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, AFT CABIN FLOOR PANEL 261XG HAS SURFACE DAMAGE. FABRICATED NEW PANEL 261XG IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, AFT CABIN FLOOR PANEL 271GF HAS SURFACE DAMAGE. FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 211.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED FLOORBEAM BETWEEN FRAME 74 - 76 AT -Y794.3. REPLACED FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED SEAT TRACK AT FRAME 47 & -Y450. REPLACED SEAT TRACK AT FRAME 47 & -Y450 IAW SRM 53-31-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, MID CABIN FLOOR PANEL 252MG HAS SURFACE DAMAGE. FABRICATED NEW PANEL 252MG IAW SRM 53-02-00 FIG 211.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED FLOOR SUPPORT AT FRAME 75.5 BETWEEN -Y450 & -Y794.3. REPLACED FLOOR SUPPORT IAW SRM 53-41-14 FIG 103 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED SEAT TRACK AT FRAME 53.3 & -Y450. REPLACED SEAT TRACK IAW SRM 53-31-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, FLOOR PANEL 242EF HAS CHIPPED MATERIAL AT FASTENER HOLE. FABRICATED NEW PANEL 242EF IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED SEAT TRACK BETWEEN FRAME 73 - 74 AT Y1250. REPLACED SEAT TRACK IAW SRM 53-41-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED SEAT TRACK BETWEEN FRAME 73 - 74 & Y1660. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 & SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED FLOORBEAM AT FRAME 76 BETWEEN -Y1447.8 & -Y1517.8. REPLACED FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11 & SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,207 hrs · 3,369 cycles

S1 CHECK, CORRODED BEAM BETWEEN FRAME 75 - 76 AT -Y380. REPLACED BEAM IAW SRM 53-41-14 FIG 101 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, CABIN FLOOR PANEL 261BF HAS SURFACE DAMAGE & DELAMINATION. FABRICATED PANEL 261BF IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 24,207 hrs · 3,369 cycles

1S CHECK, BULK CARGO FLOOR PANEL 162BF DELAMINATED ON UPPER SURFACE. FABRICATED NEW PANEL 162BF IAW SRM 53-02-00 FIG 211.

Part: COVER — UNSECURE (CABIN) · airframe 23,865 hrs · 3,306 cycles

COVER OF THE 3L EMER EXIT LIGHT OFF, OVER FLIGHT ATTENDANT JUMP SEAT. REPLACED EMER LIGHT COVER AT DOOR 3L.

Part: SLIDE — LOW PRESSURE (ZONE 200) · airframe 23,266 hrs · 3,214 cycles

LOW PRESS INDICATED ON L3 & R3 SLIDE PRESS GAGE, BAD FROM STOCK, NEVER INSTALLED ON THE ACFT. CONFIRMED FAILURE & REPAIRED IAW THE CMM 25-62-14 REV 11.

Part: HEATER — INOPERATIVE (R4 DOOR) · airframe 22,335 hrs · 3,086 cycles

GIRT BAR HEATER 24DH AT DOOR 4R INOPERATIVE. R & R GIRT BAR HEATER.

Part: HEATER — INOPERATIVE (ZONE 800) · airframe 22,335 hrs · 3,086 cycles

GIRT BAR HEATER FITTINGS INOPERATIVE ON DOOR 2L 13DH. REPLACED DOOR 2L HEATER 13DH.

Part: HEATER — INOPERATIVE (R2 DOOR) · airframe 22,335 hrs · 3,086 cycles

GIRT BAR HEATER 12DH AT DOOR 2R INOPERATIVE. R & R GIRT BAR HEATER.

Part: HEATER — INOPERATIVE (ZONE 800) · airframe 22,335 hrs · 3,086 cycles

GIRT BAR HEATER FITTINGS INOPERATIVE ON DOOR 1L 7DH. REPLACED DOOR 1L HEATER 7DH.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 1R ASSIST BOTTLE LOW, APPROX 1750 PSI. SERVICED & LEAK CHECKED DOOR 1R ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 3R ASSIST BOTTLE LOW, APPROX 1725 PSI. MAINTENANCE SERVICED & CHECKED 3R ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 1L ASSIST BOTTLE LOW PRESS. MAINTENANCE SERVICED DOOR 1L DAMPER BOTTLE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 2L ASSIST BOTTLE LOW PRESS. MAINTENANCE SERVICED DOOR 2L DAMPER BOTTLE.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 4R ASSIST BOTTLE LOW PRESS. MAINTENANCE SERVICED DOOR 4R DAMPER BOTTLE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 21,617 hrs · 2,993 cycles

DOOR 2R ASSIST BOTTLE LOW, APPROX 1750 PSI. MAINTENANCE SERVICED & LEAK CHECKED 2R ASSIST BOTTLE.

Part: COVER — DETACHED (CABIN) · airframe 21,334 hrs · 2,949 cycles

EXIT LIGHT COVER OVER 3L DOOR FELL OFF. REINSTALLED EXIT LIGHT COVER.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 21,203 hrs · 2,931 cycles

PHL R3 DOOR ASSIST BOTTLE PRESS LOW. SERVICED R3 DOOR ASSIST BOTTLE.

Part: LENS — MISSING (CABIN) · airframe 21,028 hrs · 2,896 cycles

4R EXIT LIGHT LENS IS MISSING. INSTALLED EXIT LENS AT R4 DOOR OVERHEAD, CHECKED OK.

Part: SIGN — UNSECURE (CABIN) · airframe 20,916 hrs · 2,875 cycles

EXIT SIGN 4R FELL OFF. SECURED EXIT SIGN, CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN)

EPSU SYS TEST FAULTED L4 BATTERY, 17WL. R & R L4 EPSU BATTERY, 17WL.

Part: BATTERY — DISCHARGED (CABIN)

EPSU SYS TEST FAULTED L2 BATTERY, 13WL. R & R L2 EPSU BATTERY.

Part: LIGHT — BROKEN (CABIN) · airframe 20,718 hrs · 2,828 cycles

SEAT 13B EMERGENCY LIGHT BROKEN. R & R SEAT 13B EMERGENCY LIGHT ASSEMBLY.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 20,412 hrs · 2,747 cycles

C1 CHECK DELAMINATION ON FLOOR PANEL 232KG AT BS 17638, LBL 96.5. REPLACED FLOOR PANEL 232KG IAW SRM 53-02-00-201.

Part: DOOR ACTUATOR — LEAKING (L4 DOOR) · airframe 19,712 hrs · 2,597 cycles

PHL 4 DOOR DAMPER & EMERGENCY OPERATION CYLINDER REQUIRES REPLACEMENT DUE TO LEAK BETWEEN STRIKER HOUSING & HOUSING ASSEMBLY. R & R 4L DOOR DAMPNER & EMERGENCY OPERATION CYLINDER.

Part: SIGN — UNSECURE (EMERGENCY LIGHT) · airframe 19,625 hrs · 2,581 cycles

EXIT SIGN UNSECURE AT L3 DOOR. MAINTENANCE REFITTED EXIT SIGN COVER.

Part: BOTTLE — LOW PRESSURE (L4 DOOR SLIDE) · airframe 19,525 hrs · 2,557 cycles

L4 DOOR SLIDE BOTTLE LOW PRESSURE. MX SERVICED L4 DOOR CYLINDER.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 19,097 hrs · 2,488 cycles

ON CIDS PANEL, L4 DOOR HAS AMBER CAUTION "CHECK DOOR PRESSURE". MX SERVICE DOOR ASSIST BOTTLE.

Part: SLIDE — NO TEST (L3 DOOR) · airframe 18,721 hrs · 2,440 cycles

L3 SLIDE FAILED OPS CHECKED, SLIDE JAMMED DOOR PART OPENED. MX R & R L3 DOOR SLIDE/RAFT PACK ASSY.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 18,469 hrs · 2,408 cycles

EMERGENCY LIGHT SEAT 1H INOPERATIVE. MX INSTALLED ELECTRICAL CONNECTOR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,259 hrs · 2,382 cycles

LAVATORY "L38" FLOOR LEVEL EMERGENCY LIGHT COVER MISSING. MX REPLACED LENS.

Part: BATTERY — FAULTY (CABIN) · airframe 18,044 hrs · 2,356 cycles

EPSU SYS TEST SHOWS FAULT ATA 33-51-00 BAT/ EPSU (18WL) DOOR 4. EPSU TEST SHOWS " BATT FAULT". MX REPLACED EPSU 18WL (DOOR R4) BATTERY.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 18,026 hrs · 2,354 cycles

MEGAPHONE IN AFT LT STORAGE COMPARTMENT, THE TRIGGER MECHANISMIS INOP. MX REPLACED AFT LT STORAGE COMPARTMENT MEGAPHONE.

Part: COVER — MISSING (EXIT SIGN) · airframe 17,680 hrs · 2,312 cycles

EXIT SIGN AT 3L OVERHEAD COVER FELL OFF. MX REPLACED MISSING EXIT SIGN.

Part: LENS — MISSING (CABIN) · airframe 17,476 hrs · 2,287 cycles

EMERGENCY ESCAPE PATH MARKING LIGHT AT LAV L54 MISSING LENS. MX INSTALLED LENS ON EMERG LIGHT AT LAV L54, OPS CHECK IS GOOD.

Part: COFFEEMAKER — ODOR (MID GALLEY) · airframe 17,270 hrs · 2,263 cycles

ELECTRIC BURNING ODOR BY MID GALLEY EXPRESSO MAKER LT. MX R & R MID GALLEY ESPRESSO MAKER NR 2. OPS CHECKED OK.

Part: COFFEEMAKER — SMOKE (MID GALLEY) · airframe 17,262 hrs · 2,262 cycles

MID GALLEY RT ESPRESSO MAKER SMOKING. MX R & R MID GALLEY RT ESPRESSO MAKER.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,724 hrs · 2,194 cycles

BATTERY 15WL DOOR 3L FAILED EPSU TEST. MAINTENANCE REPLACED 15WL BATTERY.

Part: RESERVOIR — LOW PRESSURE (R3 DOOR) · airframe 16,248 hrs · 2,124 cycles

ON TAXI OUT FLIGHT ATTENDANT CIDS PANEL - PSI ON 3R. MAINTENANCE SVC R3 PASSENGER EXIT DOOR WITH NITROGEN SERVICE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 15,565 hrs · 2,019 cycles

L2 DOOR CHECK LOW PRESSURE. MAINTENANCE SERVICED L2 DOOR ASSIST.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 15,474 hrs · 2,001 cycles

L4 LOW BOTTLE PRES ON DOOR. MAINTENANCE SERVICED L-4 DOOR EMERGENCY OPERATIONAL CYLINDER.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 15,121 hrs · 1,942 cycles

ON F/A CIDS {AT 1-L DOOR} THE DOOR PAGE SHOWS 2-L DOOR IS AMBER AND MESSAGE "CHECK DOOR PRESSURE". ALL DOORS AND SLIDES SHOW CLOSED AND ARMED ON ECAM DOOR PAGE IN FLIGHT DECK. MAINTENANCE SERVICED 2L DOOR DAMPER CYLINDER.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 14,738 hrs · 1,878 cycles

C2 CHECK - SEVERAL AREAS OF DELAMINATION ON UPPER & LOWER SURFACE OF FORWARD CARGO FLOOR PANEL 131DG BETWEEN FR37.4 & FR39.2. REPAIRED FORWARD CARGO FLOOR PANEL 131DG IAW EA 104340.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 14,738 hrs · 1,878 cycles

C2 CHECK - CRACK ON BULK CARGO FLOOR PANEL 161CF APPROX 19 INCHES FROM FORWARD EDGE & 29 INCHES FROM LEFT SIDE BETWEEN FR67 TO FR69. REPAIRED BULK CARGO FLOOR PANEL 161CF IAW A330 SRM 53-02-00 DATES OCT 01/12 & EA 104353.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 14,738 hrs · 1,878 cycles

C2 CHECK - CRACK ON BULK CARGO FLOOR PANEL 161CF APPROX 7.33 INCHES FROM FORWARD EDGE & 24 INCHES FROM RIGHT SIDE BETWEEN FR67 TO FR69. REPAIRED BULK CARGO FLOOR PANEL 161CF IAW A330 SRM 53-02-00 DATES OCT 01/12 & EA 104353.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 14,738 hrs · 1,878 cycles

C2 CHECK - CRACK ON BULK CARGO FLOOR PANEL 161CF APPROX. 16 INCHES FROM FORWARD EDGE & 29 INCHES FROM LEFT SIDE BETWEEN FR67 TO FR69. REPAIRED BULK CARGO FLOOR PANEL 161CF IAW A330 SRM 53-02-00 DATES OCT 01/12 & EA 104353.

Part: LENS — BROKEN (CABIN) · airframe 14,369 hrs · 1,833 cycles

FLOOR LEVEL LIGHT LENS BROKEN 2R DOOR. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK IS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,167 hrs · 1,809 cycles

FLIGHT ATTENDANT FLASHLIGHT AT DOOR L3 HAS LOW BATTERY. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK IS OKAY.

Part: LENS — MISSING (CABIN) · airframe 13,178 hrs · 1,687 cycles

EMERGENCY ESCAPE PATH LIGHT MISSING LENS AT LAV L54. MAINTENANCE INSTALLED LENS ON EMERGENCY ESCAPE LIGHT LAV 54, OPERATIONAL CHECKS OK.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 13,091 hrs · 1,677 cycles

L-2 DOOR EMERGENCY OPS CYLINDER PRESSURE LOW. MAINTENANCE SERVICED L2 DOOR EMERGENCY OPS CYLINDER, LEAK CHECK OK.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 13,091 hrs · 1,677 cycles

CAB PSI INDICATION ON 3R DOOR (UPON ARRIVAL AT PHL) LOCATED ON CIDS PANEL NOT NORMAL. MAINTENANCE SERVICED R3 DOOR EMERGENCY OPS CYLINDER, LEAK CHECK OK.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 12,447 hrs · 1,596 cycles

CIDS PAGE CABIN STATUS L2 DOOR UNARMED, DOOR/SLIDES PAGE CHECK DOOR PRESSURE. MAINTENANCE SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802-A LEAK CHECK GOOD. NO SCEPTRE HISTORY 30 DAYS OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 12,062 hrs · 1,546 cycles

PHL - COVER PLATE MISSING ON EMERGENCY LIGHT, NEXT TO LAV 54, A/C RIGHT MID-SECTION. REPLACED MISSING LENS COVER.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 11,789 hrs · 1,513 cycles

DURING DAILY CHECK - FOUND DOOR 2L ASSIST BOTTLE INDICATION IN YELLOW BAND. MAINTENANCE DOOR BOTTLE SERVICED IAW AMM 52-10-00-600-802-B.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 11,603 hrs · 1,488 cycles

C1 CHECK - AREA OF DELAMINATION ON HEATED FLOOR PANEL 40DS BETWEEN FR74 TO FR76 AT R4 DOORWAY. REPLACED HEATED FLOOR PANEL 40DS IAW EA 103726.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 11,603 hrs · 1,488 cycles

C1 CHECK - AREA OF DELAMINATION ON HEATED FLOOR PANEL 38DS BETWEEN FR74 TO FR76 AT R4 DOORWAY. REPLACED HEATED FLOOR PANEL 38DS IAW EA 103726.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 11,603 hrs · 1,488 cycles

C1 CHECK - AREA OF DELAMINATION ON HEATED FLOOR PANEL 112DS BETWEEN FR74 TO FR76 AT R4 DOORWAY. REPLACED HEATED FLOOR PANEL 112DS IAW EA 103726.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 10,689 hrs · 1,370 cycles

PHL - 2L DOOR CHECK DOOR PRESS LIGHT AMBER ON CIDS PANEL. MAINTENANCE SERVICED 2L DOOR ASSIST BOTTLE AS REQUIRED PER AMM 52-12-14. OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 10,008 hrs · 1,284 cycles

CDG - CABIN DOOR 2L SHOWS OPEN AND UNARMED WHILE INFLIGHT ON THE CIDS PANEL. IT INDICATES CORRECTLY ON THE FLIGHT DECK ECAM PAGE. ON GROUND IT HAS A CHECK PRESSURE WARNING ON CIDS PANEL. MAINTENANCE - DOOR 2L OPENED AND CLOSED. ARM - DISARMED OPS CKD OK ALL INDICATIONS NORMAL. SERVICED 2L DOOR EMERGENCY CYLINDER PER MM 52-10-00-600-802 CKD OK. FAP MSG CLEARED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,748 hrs · 1,129 cycles

CDG - FLASHLIGHT AT DOOR 3R IS INOP. SEAL BROKEN. MAINTENANCE RELEASED ON MEL. ON JULY 16, 2011 THE FLASHLIGHT AT DOOR 3R WAS REMOVED AND REPLACED, MEL REMOVED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 8,570 hrs · 1,105 cycles

MOC - ETOPS P1 TSI - PLEASE CHECK THE 2L DOOR ASSIST BOTTLE FOR PROPER SERVICING. MAINTENANCE SERVICED 2L DOOR ASSIST BOTTLE TO PROPER LEVEL PER AMM 52-10-00-991-012.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - FOUND CREW REST FLASHLIGHT REMOVED FROM HOLDER AND BATTERY DEAD. REMOVED AND REPLACED CREW REST FLASHLIGHT BATTERY. OPS CHECKED OK. RESEALED IN HOLDER.

Part: LIGHT — UNSECURE (CABIN)

PHL - THE EMERGENCY EXIT LIGHT WAS UNATTACHED FROM SEAT 2A. MAINTENANCE RE-SECURED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

PHL - CHECKED THE DOOR PRESSURE FOR THE L2 DOOR ASSIST BOTTLE, AND FOUND LOW. MAINTENANCE SERVICED THE L2 DOOR ASSIST BOTTLE PRESSURE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

PHL - THE CAPTAIN AND FIRST OFFICER'S FLASHLIGHTS WERE INOPERATIVE. THE FLIGHT DECK FLASHLIGHTS ARE NOT REQUIRED FOR THIS AIRCRAFT AND FLEET, AND WERE SUBSEQUENTLY REMOVED.

Part: CYLINDER — LOW PRESSURE (L2 DOOR)

PHL - DURING CHECK, FOUND THE L2 DOOR ASSIST CYLINDER PRESSURE LOW. SERVICED DOOR L2 ASSIST CYLINDER.

Part: CYLINDER — LOW PRESSURE (R3 DOOR)

PHL - MAINTENANCE FOUND THE R3 DOOR ASSIST CYLINDER PRESSURE LOW. SERVICED THE R3 DOOR ASSIST CYLINDER.

Part: CYLINDER — LOW PRESSURE (L2 DOOR)

CDG - THE L2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. MAINTENANCE SERVICED THE L2 DOOR EMERGENCY CYLINDER.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 5,792 hrs · 755 cycles

CWF - C1 - EEL - LIGHT BULB BURNT OUT IN FLASHLIGHT AT G6 GALLEY ATTENDANT SEAT. REPLACED FLASHLIGHT AT G6 GALLEY ATTENDANT SEAT IAW A330 AMM 25-22-00-210-059.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

PHL - FLASHLIGHTS AT POSITIONS L4 & R4 ARE NOT CHARGING. REMOVED AND REPLACED FLASHLIGHTS.

Part: SKIN — CRACKED (LE SLAT) · airframe 5,792 hrs · 755 cycles

CWF - MAJOR REPAIR - C1 - CRACK ON NR 2 SLAT UPPER SURFACE TRAILING EDGE 16 INCHES FROM INBOARD EDGE OF SLAT. REPAIRED NR 2 SLAT UPPER SURFACE TRAILING EDGE 16 INCHES FROM INBOARD EDGE OF SLAT IAW A330 SRM 57-40-00.

Part: CYLINDER — LOW PRESSURE (EVAC SLIDE)

MUC - DOOR L2 SLIDE LOW PRESSURE ON CIDS PANEL. GAUGE ON DOOR SHOWS GREEN. EMERGENCY OPERATION CYLINDER ACC SERVICED.

Part: CYLINDER DAMPER — LOW PRESSURE (EMERGENCY EXIT)

TLV - FOUND THE RIGHT EMERGENCY DOOR ACCUMULATOR/DAMPER PRESSURE LOW. ACCUMULATOR SERVICED TO NOMINAL PRESSURE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

CLT - CHECK DOOR PRESSURE ANNUNCIATION ON THE FORWARD CIDS PANEL BY L1 FOR DOOR L2. DOOR ARMING WAS GOOD ON THE PILOT'S PANEL. SERVICED THE L2 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

PHL - PILOT REPORTED "CHECK DOOR PRESSURE" APPEARED ON CIDS PANEL FOR 2L DOOR. MAINTENANCE SERVICED 2L DOOR BOTTLE PER AMM PROCEDURES. CHECKS OK.

Part: FILTER — FOULED (CABIN)

PHL FLT 1024 EN ROUTE SJU TO PHL. ON CLIMBOUT FROM SJU, ABOUT 20,000 FEET, TURNED ON ENGINE ANTI-ICE AND NOTICED A BURNT RUBBER SMELL. SMELL LASTED FOR ABOUT FIVE MINUTES AFTER THE ANTI-ICE WAS TURNED OFF, IT WAS NOTICED THROUGHOUT THE CABIN. REPLACED ALL EIGHT RECIRCULATION FILTERS, FORWARD AND AFT, LEFT AND RIGHT POSITIONS. NO SMELL NOTICED ON GROUND RUN. A SATISFACTORY TEST FLIGHT WAS ACCOMPLISHED, WITH THE ANTI-ICE OPERATED ABOVE FL 200 FOR ABOUT 30 MINUTES. NO ODORS NOTED.

Part: DAMPER — LOW PRESSURE (L2 DOOR)

TLV - DURING THE DAILY CHECK, FOUND DOOR 2 LEFT DAMPER/EMERGENCY ACCU PX LOW. DOOR 2 LEFT DAMPER/EMERGENCY ACCU PX SERVICED TO NOMINAL PRESSURE. NO LEAK OBSERVED.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

LHR - FOUND THE FLIGHT ATTENDANT FLASHLIGHT 4 LEFT INOPERATIVE. REPLACED FLASHLIGHT AND BATTERY.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

PHL - F/A CIDS PANEL INDICATES AMBER L2 CHECK DOOR PRESSURE ANNUNCIATOR. SERVICED L2 DOOR ASSIST BOTTLE TO FULL.

Part: UNKNOWN — MALFUNCTIONED (ICE PROTECTION)

PHL - CIDS PANEL DISPLAYS WASTE WATER ICE PROTECTION INOP - MAINT REQUIRED. TROUBLESHOT, FOUND IPCU 16DS FAULTED ON BITE CHECK. IPCU 16DS CONTROLS 3L/3R AND 4L/4R DOOR SLIDE ATTACH HEATERS - SLIDE LOCKING MECHANISM ICE PROTECTION INOP. CHECKED ALL FUSES. NO FAULTS FOUND. PERFORMED BITE CHECK. NO FAULTS FOUND. OPS CHECK GOOD.