N272AY

Part: UNKNOWN — ODOR (CABIN) · airframe 85,919 hrs · 12,559 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED ON ACCOUNT OF CABIN DIRTY SOCK ODOR. EMERGANCY WAS DECLARED. MAINTENANCE DETERMINED APU TO BE SOURCE OF ODOR. MAINTENANCE ACCOMPLISHED BORESCOPE INSPECTION OF APU LOAD COMPRESSOR, NO FINDINGS. ACCOMPLISHED JOB CARD 33L000021003. NO FURTHER ODORS WERE NOTED.

Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 85,569 hrs · 12,512 cycles

AIRCRAFT WAS GROUNDED: PILOT RETURNED TO CLT ON ACCOUNT OF NUMBER 1 ENGINE OVER TEMPERATURE INDICATION. EMERGENCY DECLARED. MAINTENANCE ACCOMPLISHED VISUAL INSPECTION IAW AMM 72-00-00-200-808A, FOUND WITHIN LIMITS OF AREA A. IAW TSM 71-00-00-700-825A.

Part: CYLINDER — NO TEST (R3 DOOR)

DURING AN OPERATIONAL TEST OF THE R3 DOOR DAMPING FAILED TO TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-22-14-400-801-A.

Part: SUPPORT BRACKET — CRACKED (FRAMES 39) · airframe 84,065 hrs · 12,295 cycles

CRACKED LOWER FUSELAGE FAIRING SUPPORT BRACKET AT FRAME 39 LEFT. REPLACED THE SUPPORT BRACKET IAW SRM 51-72-11-911-001.

Part: SUPPORT BRACKET — CRACKED (FRAME 39) · airframe 84,065 hrs · 12,295 cycles

CRACKED LOWER FUSELAGE FAIRING SUPPORT BRACKET AT FRAME 39 RIGHT. REPLACED THE SUPPORT BRACKET IAW SRM 51-72-11-911-001.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 84,065 hrs · 12,295 cycles

LEFT WING OTBD TRAILING EDGE FLAP SKIN WAS DEBONDED. REPAIRED THE FLAP IAW SRM 57-55-00-300-028.

Part: PUMP — LEAKING (FUEL BOOST) · airframe 83,593 hrs · 12,229 cycles

REAR GALLEY HAD A FUEL ODOR AROUND THE SERVICING CARTS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE TRIM TANK BOOST PUMP LEAKING, ROUTED TO THE SHROUD SYSTEM AND REPLACED THE TRIM TANK PUMP IAW AMM 28-27-48. MAINTENANCE ALSO PERFORMED SATISFACTORY OPERATIONAL CHECK, NO LEAKS NOTED.

Part: SOLENOID VALVE — FAULTY (NR 1 ENGINE) · airframe 83,593 hrs · 12,229 cycles

AFTER TAKEOFF, A CONTROL SYSTEM MESSAGE FOR THE NR 1 ENGINE OVERHEAT AND LARGE FUEL FLOW DISCREPANCY BETWEEN THE NR 1 & 2 ENGINES. RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED TSM 71-00-00-810-825-A, AND 75-32-00-810-845-A. REPLACED THE BLEED VALVE SOLENOID IAW AMM 75-32-13, 75-32-16, AND 75-32-15. ENGINE RUNS CARRIED OUT AND ALL OPS NORMAL. OK FOR SERVICE.

Part: THERMOCOUPLE — MALFUNCTIONED (NR 1 ENGINE) · airframe 83,593 hrs · 12,229 cycles

CAPTAIN CALLED AFTER TAKEOFF, A CONTROL SYSTEM FLIGHT MESSAGE FOR THE NR 1 ENGINE OVERHEAT AND LARGE FUEL FLOW DISCREPANCY BETWEEN THE NR 1 & 2 ENGINES. THE FLIGHT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED TSM 71-00-00-810-825-A, AND 75-32-00-810-845-A. REPLACED THE BLEED VALVE THERMOCOUPLE PROBE IAW AMM 75-32-13, 75-32-16, AND 75-32-15. ENGINE RUNS CARRIED OUT AND ALL OPS NORMAL. OK FOR SERVICE.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 83,593 hrs · 12,229 cycles

CAPTAIN CALLED AFTER TAKE OFF, WITH CTRL SYSTEM FLIGHT MESSAGE FOR ENGINE NR 1 OVERHEAT AND LARGE FUEL FLOW DISCREPANCY BETWEEN ENGINE NR 1 AND 2. PATCHED WITH TECH AND DETERMINED ETOPS ENTRY NOT POSSIBLE IAW QRH AND WILL RETURN TO DEPARTURE. ACCOMPLISHED TSM TASK 71-00-00-810-825-A AND 75-32-00-810-845-A. REPLACED THE BLEED VALVE, IAW AMM 75-32-13, 75-32-16, AND 75-32-15. ENGINE RUNS CARRIED OUT AND ALL OPS NORMAL. OK FOR SERVICE.

Part: AIR FILTER — FAULTY · airframe 83,593 hrs · 12,229 cycles

AFTER TAKEOFF, A CONTROL SYSTEM MESSAGE FOR THE NR 1 ENGINE OVERHEAT AND LARGE FUEL FLOW DISCREPANCY BETWEEN THE NR 1 & 2 ENGINES. RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED TSM 71-00-00-810-825-A, AND 75-32-00-810-845-A. REPLACED THE BLEED VALVE SOLENOID IAW AMM 75-32-13, 75-32-16, AND 75-32-15. ENGINE RUNS CARRIED OUT AND ALL OPS NORMAL. OK FOR SERVICE.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 82,345 hrs · 12,061 cycles

AIRCRAFT RETURNED TO FIELD DUE TO A HYDRAULIC G, NR 1 ENGINE PUMP LOW PRESSURE ECAM MESSAGE (ELECT PUMP OFF). THE AIRCRAFT WAS GROUNDED. NO FLUID LOSS. REPLACED THE NR 1 ENGINE GREEN SYSTEM HYDRAULIC PUMP IAW AMM 29-11-51. OPS AND LEAK CHECKED GOOD.

Part: TRANSMITTER — DEFECTIVE (TOILET) · airframe 82,240 hrs · 12,049 cycles

LEFT LAVATORY TANK LEVEL WENT TO 100% AFTER TAKEOFF. LEFT SIDE SYSTEM SHUTDOWN FLUID IN BOWLS SPILLED OUT. AN EMERGENCY WAS DECLARED AND RETURNED TO FIELD. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED LEFT WASTE LEVEL TRANSMITTER IAW AMM 33-31-11-400-801A. OPS CHECKED GOOD. REPLACED TOILET AND PERFORMED A VACCUM CHECK IAW AMM 38-31-00-790-801A. LEAK AND VACUUM TESTED GOOD.

Part: TOILET — DEFECTIVE (LT LAVATORY) · airframe 82,240 hrs · 12,049 cycles

LEFT LAVATORY TANK LEVEL WENT TO 100% ON AFTER TAKEOFF, LEFT SIDE SYSTEM SHUTDOWN, FLUID IN BOWLS SPILLED OUT. DECLARED AN EMERGENCY, AND RETURNED TO FIELD. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED LEFT WASTE LEVEL TRANSMITTER IAW AMM 33-31-11-400-801A. OPS CHECKED GOOD. REPLACED TOILET AND PERFORMED A VACCUM CHECK IAW AMM 38-31-00-790-801A. LEAK AND VACUUM TEST GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 81,752 hrs · 11,985 cycles

FLASHLIGHT AT L2 DOOR WAS FOUND UNSERVICABLE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND STRAP IAW AMM 25-60-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 81,279 hrs · 11,927 cycles

DURING FLIGHT, RECEIVED AN ECAM FOR THE HYD G RSVR LO LVL, HYD G SYS LO PR, GREEN HYD QTY DECREASED TO ZERO. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. IAW TSM 29-11-00-810-801-A, R & R ALL THREE GREEN SYS HYD PUMPS, SYSTEM OPS CHECKED GOOD, OK FOR SERVICE, FOUND A PLUG ON GREEN SYS BRAKE MANIFOLD LEAKING. REPLACED THE O-RING, LEAK CHECKED GOOD.

Part: FITTING — DEFECTIVE (ZONE 800) · airframe 80,630 hrs · 11,843 cycles

AIRCRAFT IN BASE MAINTENANCE. SLIDE FITTING HEATING CONTROL UNITS 3DH, 15DH AND 21DH DIDN'T PASS TEST. REPLACE ESCAPE SLIDE FITTING ASSEMBLY TO 5DH, 17DH, AND 26DH IN PASSENGER CABIN. THIS SDR IS FOR THE 17DH UNIT. (SEE CONTROL #AALA201804109026 AND #AALA201804119025)

Part: FITTING — DEFECTIVE (ZONE 800) · airframe 80,630 hrs · 11,843 cycles

AIRCRAFT IN BASE MAINTENANCE. SLIDE FITTING HEATING CONTROL UNITS 3DH, 15DH AND 21DH DIDN'T PASS TEST. REPLACE ESCAPE SLIDE FITTING ASSEMBLY TO 5DH, 17DH, AND 26DH IN PASSENGER CABIN. THIS SDR IS FOR THE 5DH UNIT. (SEE CONTROL #AALA201804119024 AND #AALA201804119025)

Part: FITTING — DEFECTIVE (ZONE 800) · airframe 80,630 hrs · 11,843 cycles

AIRCRAFT IN BASE MAINTENANCE. SLIDE FITTING HEATING CONTROL UNITS 3DH, 15DH AND 21DH DIDN'T PASS TEST. REPLACE ESCAPE SLIDE FITTING ASSEMBLY TO 5DH, 17DH, AND 26DH IN PASSENGER CABIN. THIS SDR IS FOR THE 26DH UNIT. (SEE CONTROL #AALA201804109026 AND #AALA201804119024)

Part: STRINGER — CRACKED (FRAME 53.5) · airframe 80,627 hrs · 11,842 cycles

A CRACK INDICATION ON STRINGER 15R OF TORSION BOX AT FRAME 53.5. REPLACED THE STRINGER IAW SRM 51-72-11, AND DRAWING F53370020.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,627 hrs · 11,842 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON STRINGER 14 RIGHT OF TORSION BOX BETWEEN FR 53.7A TO FR 53.8 IN PASSENGER CABIN. REPAIRED STRINGER 14 RIGHT PER EA 278902 PART A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,627 hrs · 11,842 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON STRINGER 14 LEFT OF TORSION BOX AT FR 53.8 IN PASSENGER CABIN. REPAIRED STRINGER 14 LEFT PER EA 278900.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,627 hrs · 11,842 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON STRINGER 14 LEFT OF TORSION BOX AT FR 53.5 IN PASSENGER CABIN. REPAIRED STRINGER 14 LEFT PER EA 278900.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 80,627 hrs · 11,842 cycles

OVERHEAD EMERGENCY LIGHT LENS BROKEN AT SEAT, L3 DOOR. REPLACED THE LENS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LEAKING (L3 DOOR ASSIST) · airframe 80,164 hrs · 11,764 cycles

L3 DOOR ASSIST BOTTLE LEAKING. REPLACED THE DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 80,130 hrs · 11,759 cycles

L3 DOOR ASSIST BOTTLE HAD PRESSURE LOW. SERVICED THE ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 80,002 hrs · 11,735 cycles

L3 DOOR ASSIST PRESSURE LOW. SERVICED L3 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 79,872 hrs · 11,715 cycles

L3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE BOTTLE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 79,872 hrs · 11,715 cycles

EMERGENCY LIGHT LENS MISSING AT THE L3 DOOR. INSTALLED A NEW LENS.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 79,649 hrs · 11,681 cycles

L3 DOOR DAMPER CYLINDER LOW. SERVICED L3 DOOR DAMPER CYLINDER IAW AMM 52-10-00-600-802-A.

Part: DECODER — UNSERVICEABLE (L1 DOOR) · airframe 79,443 hrs · 11,650 cycles

AIRCRAFT WAS GROUNDED. 1-L DOOR PRESSURE INDICATION INOP. REPLACED DEU B.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 79,326 hrs · 11,632 cycles

AIRCRAFT WAS NOT GROUNDED. L3 DOOR ASSIST PRESSURE LOW. SERVICED L3 DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 79,007 hrs · 11,589 cycles

L3 DOOR ASSIST BOTTLE PRESSURE IN YELLOW. CHARGED THE DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 78,809 hrs · 11,565 cycles

L3 DOOR ASSIST BOTTLE IN YELLOW BAND. SERVICED THE DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 78,640 hrs · 11,544 cycles

DURING EMERGENCY EQUIPMENT CHECK, FOUND THE L3 DOOR NOT IN GREENBAND. CHARGED THE DOOR DAMPER.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 78,113 hrs · 11,479 cycles

EXIT SIGN OVER THE L3 DOOR KEEPS FALLING OFF. MAINTENANCE REPLACED EXIT SIGN LENS IAW AMM 33-51-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 78,079 hrs · 11,475 cycles

EMERGENCY POWER SUPPLY UNIT BATTERY FAILED AT 16WL. REPLACED BATTERY AT 16WL.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 78,000 hrs · 11,465 cycles

AIRCRAFT WAS NOT GROUNDED. L3 DOOR ASSIST BOTTLE IN YELLOW RANGE. SERVICED DOOR ASSIST BOTTLE.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 77,692 hrs · 11,425 cycles

R4 DOOR WILL NOT ARM. REMOVED DEBRIS FROM FORWARD GIRT ATTACH FITTING AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 77,692 hrs · 11,425 cycles

L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L3 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: WARNING HORN — FALSE ACTIVATION · airframe 77,402 hrs · 11,389 cycles

WHEN THROTTLES WERE ADVANCED FOR TAKE OFF THE AUDIBLE EVACUATION COMMAND SOUNDED. TAKE OFF WAS ABORTED. EVACUATION COMMAND CONTINUED UNTIL SILENCED BY THE FLIGHT CREW. COMMUNICATION BETWEEN FLIGHT CREW AND CABIN CREW DETERMINED THERE WAS NO INTENTIONAL ACTIVATION OF THE COMMAND. SUBSEQUENT TAKE OFF WAS UNEVENTFUL. ON LANDING, MAINTENANCE ACCOMPLISHED A HARD RESET OF THE CIDS PANEL.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 77,271 hrs · 11,372 cycles

L3 DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED THE CYLINDER IAW AMM 52-22-00-600-801A. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 77,177 hrs · 11,356 cycles

L3 DOOR DAMPER CYLINDER PRESSURE IN YELLOW. SERVICED THE CYLINDER BOTTLE.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 76,506 hrs · 11,272 cycles

AIRCRAFT WAS GROUNDED. LEFT HAND EMERGENCY DOOR, DOOR ASSIST ACCUMULATOR LOW PRESSURE. SERVICED LEFT HAND EMERGENCY DOOR ACCUMULATOR.

Part: SIGN — UNSECURE (CABIN) · airframe 76,435 hrs · 11,260 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN 3L FELL OFF. REATTACHED 3L EMERGENCY EXIT LIGHT COVER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,962 hrs · 11,179 cycles

DURING CABIN SWEEP, MAINTENANCE FOUND THE G-3 EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 75,954 hrs · 11,178 cycles

L3 OVERWING DOOR ASSIST BOTTLE SHOWS LOW PSI. SERVICED DOOR ASSIST BOTTLE MM 52-10-00.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 75,761 hrs · 11,141 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY POWER SUPPLY UNIT IN THE L2 POSITION FAULTING. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: DIRECTOR — MALFUNCTIONED (CIDS) · airframe 75,601 hrs · 11,110 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EVACUATION COMMAND WENT OFF UNCOMMANDED. WAS ABLE TO RESET. MAINTENANCE REPLACED CIDS DIRECTOR NR 1 PER AMM 23-73-34. PERFORMED SATISFACTORY EMERGENCY EVACUATION SIGNALING TEST PER 23-73-00.

Part: PROBE — FAULTED (FUEL SYSTEM) · airframe 75,562 hrs · 11,100 cycles

CREW REPORTED POSSIBLE FUEL GAUGE INDICATION PROBLEM. RIGHT INNER FUEL QUANTITY DECREASED AROUND 3000 LBS. DECREASE REFLECTED ON FUEL ON BOARD TOTAL, PLANNED FUEL BURN VERSE ACTUAL WITHIN 1500 LBS. DECLARED A FUEL EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WING TANK PROBE 120QT2 IAW AMM 28-42-15.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 75,233 hrs · 11,563 cycles

RIGHT EMERGENCY EXIT DOOR COCKPIT, CLOSE GREEN/OPEN AMBER INDICATION, INTERMITTENT. CLEANED SENSOR AND TARGET (18WS), CHECKED ADJUSTMENT AND RETIGHTED CONNECTOR PLUG IAW AMM 52-71-12.

Part: FITTING — CORRODED (FRAME 16A) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON FITTING AT STRINGER 26R AND FRAME 16A. REPLACED THE FITTING IAW SRM 53-11-14, SRM 51-42-11 AND AMM 30-46-00.

Part: LENS — CRACKED (CABIN) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. L4 EXIT LIGHT LENS CRACKED. REPLACED EXIT LIGHT LENS PER AMM 33-51-16.

Part: FITTING — FAULTY (L4 DOOR) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT N BASE MAINTENANCE. AFT OF BULK CARGO, HEATED SLIDE FITTING CONTROL UNIT 21DH, FAILS BITE TEST WITH FAULT FOR L4 DOOR DUE TO FORWARD SLIDE LOCK FITTING (23DH). REPLACED L4 DOOR FORWARD SLIDE LOCK FITTING PER AMM 30-46-11 AND 52-13-31.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 75,377 hrs · 11,066 cycles

DELAMINATION ON FLOOR PANEL BETWEEN FRAMES 74 AND 75. REPAIRED THE FLOOR PANEL IAW EA 265802.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 75,377 hrs · 11,066 cycles

DELAMINATION ON FLOOR PANEL BETWEEN FRAMES 74 AND 75. REPAIRED THE FLOOR PANEL IAW E.A 265801.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 75,377 hrs · 11,066 cycles

CORROSION FOUND ON FLOOR PANEL 271JF METAL COVER PLATE. REPLACED FLOOR PANEL PER EA 265767.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 75,377 hrs · 11,066 cycles

CORROSION ON FLOOR PANEL 272JF METAL COVER PLATE. REPLACED FLOOR PANEL IAW EA 265766.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON AFT CABIN FLOORBEAM AT FRAME 73, BETWEEN -Y1959 AND -Y2462. REPLACED THE FLOORBEAM IAW SRM 53-41-14.

Part: FLOORBEAM — CRACKED (FRAME 74) · airframe 75,377 hrs · 11,066 cycles

CRACK ON FRAME 74 FLOORBEAM AT YB. REPAIRED THE FLOORBEAM IAW SRM 53-00-14-201.

Part: FLOOR SUPPORT — CORRODED (FRAMES 74-82) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION WAS FOUND ON THE AFT CABIN FLOOR SUPPORT AT Y1137.1 BETWEEN FRAMES 74 AND 82. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14-101.

Part: SEAT TRACK — CORRODED (FRAME 13A) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

FOUND CORROSION ON THE SEAT TRACK AT Y953 AND FRAME 13A. REPLACED THE SEAT TRACK IAW SRM 53-11-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SEAT RAIL AT -Y2000 AND FR 72. REPLACE SEAT RAIL PER SRM 53-41-14-101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR, AFT SECTION OF R4 DOOR THRESHOLD, SUPPORT BEAM ASSEMBLY AT FR 75A AND -Y2300. REPLACED FLOOR SUPPORT PER SRM 51-73-11 AND 51-42-11.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 152AF. REPLACED FLOOR PANEL PER SRM 53-0200-201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOORBEAM AT -Y1959 AND FR 72. REPLACED FLOORBEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED/BROKEN FORWARD CARGO COMPARTMENT FLOOR PANEL 131QF. REPAIRED FLOOR PANEL PER SRM 53-02-00-201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK, 10 INCHES FORWARD OF FR72 TO FR75 AT Y450. REPLACED SEAT TRACK PER SRM 53-41-14-101 AND SRM 51-42-11.

Part: CONTROL UNIT — NO TEST (SLIDE FITTING) · airframe 75,377 hrs · 11,066 cycles

FORWARD CARGO RIGHT SIDE, JUST AFT OF CARGO DOOR, HEATED SLIDE FITTING CONTROL UNIT (10DH) FAILS BITE CHECK. REPLACED THE CONTROL UNIT IAW AMM 30-46-34-0401.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN RIGHT HAND SIDE FLOOR TO WALL JOINT, PROFILE AT FR 75.4 AND STRINGER 26R. REPLACED PROFILE PER SRM 51-42-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON JUNCTION FITTING BETWEEN FR 12A AND FR 13. REPLACED JUNCTION FITTING PER SRM 53-11-13 AND ESO 34002.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y1447.8 AND FR 73. REPLACED SEAT TRACK PER SRM 51-74-00, SRM 53-41-15-101 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT BEAM INBOARD OF TRACK -Y450 AND FR 75. REPLACED FLOOR SUPPORT BEAM PER SRM 51-44-11-101 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM 7 INCHES AFT OF FR 73 AND BETWEEN TRACK YA AND YB. REPLACED AUXILIARY BEAM PER SRM 53-41-14 AND 51-42-11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN INTERCOSTAL AT Y0 BETWEEN FR 78 AND FR 79. REPLACED INTERCOSTAL PER SRM 53-41-14-101 AND 51-42-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y2462 AND FR 53.4. REPLACED SEAT TRACK PER SRM 51-74-00, SRM 53-31-15 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT Y1447.8 BETWEEN FR 77 AND FR 80. REPLACED FLOOR SUPPORT PER SRM 53-41-14, 51-41-20 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT Y450 AND FR 75. REPLACED SEAT TRACK PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y2462 AND FR 33. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 51-42-11 AND SRM 53-21-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT -Y450 BETWEEN FR 75 AND FR 82. REPLACED SEAT TRACK PER SRM 53-41-14 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT Y1447.8 BETWEEN FR 73 AND FR 74. REPLACED SEAT TRACK PER SRM 53-00-15 AND SRM 51-42-11

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y953 AND FR 37. REPLACED SEAT TRACK PER SRM 53-00-15-101.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN TRACK ATTACH PLATE AT -Y450 BETWEEN FR 80 AND FR 82. REPLACED PLATE PER SRM 53-41-14 AND 51-42-11

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT CABIN FLOOR AFT OF R4 DOOR FRAME SHEAR-WEB AT STRINGER 26R AND FR 75. REPAIRED SHEAR-WEB PER SRM 53-41-14.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR CROSSBEAM AT FR 75 BETWEEN Y0 AND -Y1137. REPAIRED CROSSBEAM PER SRM 53-00-14-201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y450 AND FR 37. REPLACED SEAT TRACK PER A330 SRM 53-00-15-101.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON THE SEAT TRACK AT FRAME 33 AND Y1959. REPAIRED THE SEAT TRACK IAW SRM 53-00-14, AND SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FRAME 18) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON SEAT TRACK, -Y450 AND FRAME 18. REPLACED THE SEAT TRACK IAW SRM 53-00-15 FIG.103, AND SRM 51-42-11.

Part: PLATE — CORRODED (FRAMES 80-82) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON ATTACH PLATE AT Y450 BETWEEN FRAMES 80 AND 82. REPLACED THE ATTACH PLATE IAW SRM 53-00-15-101.

Part: SEAT TRACK — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON FORWARD CABIN, SEAT TRACK AT -Y450 BETWEEN FRAMES 17 AND 18. REPLACED THE SEAT TRACK IAW SRM 53-11-15-101.

Part: SHIM — CORRODED (FRAME 72) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON AFT CABIN FLOOR FORWARD SECTION OF DOOR THRESHOLD SHIM, -Y2300 AND FRAME 72. REPLACED THE SHIM IAW SRM 51-74-00, AND 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 75A) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON AFT CABIN FLOORBEAM -Y1137 AND FRAME 75A. REPLACED THE FLOORBEAM IAW SRM 51-74-00, SRM 51-73-11, AND SRM 51-42-11.

Part: SHIM — CORRODED (FRAME 73) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON AFT CABIN MID SECTION OF R4 DOOR THRESHOLD, FLOOR ATTACHING ANGLE SHIM, -Y2300 AND FRAME 73. REPLACED THE SHIM IAW SRM 51-74-00, SRM 51-73-11, AND SRM 51-42-11.

Part: SHIM — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT SHIM AT Y1447.8 AND 10 INCHES FORWARD OF FRAME 74. REPLACED THE FLOOR SUPPORT SHIM IAW SRM 53-41-14-101.

Part: SEAT TRACK — CORRODED (FRAMES 33-34) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON SEAT TRACK AT -Y1456 BETWEEN FRAMES 33 AND 34. REPLACED THE SEAT TRACK IAW SRM 53-00-15.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

CORROSION ON FORWARD CABIN FLOORBEAM LANDING ASSEMBLY FITTING AT FRAME 17 BETWEEN -Y953 AND -Y1456. REPLACED THE TEE IAW SRM 53-11-14-101.

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y450 AND FR 73. REPLACED SEAT TRACK PER SRM 51-42-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED PROFILE Z, L= 2.45" W= 2.21 D= .070". REPLACED WITH IDENTICAL PART IAW ARM 51-42-11 AND 51-44-11.

Part: SHIM — CORRODED (FRAMES 74-75) · corrosion level 2 · airframe 75,377 hrs · 11,066 cycles

DOOR SILL SHIM CORRODED. REPLACED THE SHIM IAW SRM 51-41-11.

Part: OVEN — ODOR (GALLEY) · airframe 75,337 hrs · 11,060 cycles

AIRCRAFT WAS NOT GROUNDED. OVEN NR 1 HAS STRONG ELEC SMELL MAYBE A BAD HEATING COIL. MAINTENANCE REPLACED THE NR 1 OVEN PER AMM 25-35-19.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 75,306 hrs · 11,056 cycles

NR 1 OVEN IN AFT GALLEY BECAME UNCONTROLLABLE HOT, PULLED CIRCUIT BREAKER AND HEAT SUBSIDED. MAINTENANCE REPLACED THE OVEN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECKED IAW AMM 25-35-19.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 75,006 hrs · 11,018 cycles

DURING DAILY CHECK FOUND THE L1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: SIGN — DETACHED (CABIN) · airframe 74,958 hrs · 11,012 cycles

EMERGENCY EXIT SIGN FELL OFF AT 3L DOOR. INSTALLED EMERGENCY EXIT SIGN AT THE 3L DOOR.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 73,890 hrs · 10,879 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR SLIDE WILL NOT ARM. MAINTENACE REMOVED GLASS FROM THE GIRT BAR FLOOR TRACK.

Part: SERVER — DEFECTIVE (CABIN) · airframe 73,487 hrs · 10,830 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT CREW REPORTED THAT WHILE DESCENDING THROUGH 200000 FEET, VIDEO SCREENS IN ECONOMY WERE BLINKING ON AND OFF AND F/A`S DETECTED AN ODOR RESEMBLING DIRTY SOCKS. POWER TO VIDEO SYSTEM WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 CONTENT SERVER UNIT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 23-32-00.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 73,338 hrs · 10,810 cycles

AIRCRAFT WAS NOT GNDED. CIDS INDICATES DOOR 3L SLIDE BOTTLE PRESSURE LOW. SERVICED 3L DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 72,882 hrs · 10,755 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR DAMPER REQUIRES CHARGING. SERVICED 3L DOOR DAMPER IAW AMM 52-10-00.

Part: BATTERY — FAULTED (CABIN) · airframe 72,757 hrs · 10,738 cycles

AIRCRAFT WAS NOT GNDED. 4L EMER POWER SUPPLY BATTERY FAULT DURING TEST 17WL. R & R BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BRAKE — DEFECTIVE (ZONE 700) · airframe 72,455 hrs · 10,700 cycles

AIRCRAFT WAS NOT GNDED. AFTER TAKEOFF FOR LT PACK MAX TEMP, WHEEL 1=395, WHEEL 2= 585, WHEEL 5= 300 & WHEEL 6=485. THE BRAKES WERE COOLED, THE GEAR RETRACTED & THE FLIGHT CONTINUED. CREW REQUESTED EMER EQUIPMENT BE STANDING BY UPON ARRIVAL AS A PRECAUTIONARY MEASURE. THE ACFT LANDED SAFELY WITH NO BRAKE OVERHEATING NOTED & TAXIED TO THE GATE WITH NO FURTHER INCIDENTS. REPLACED THE NR 2 BRAKE ASSEMBLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL & LEAK CHECK IAW AMM 32-42-27-0401.

Part: CHANNEL — CONTAMINATED (ENTRY DOOR) · airframe 72,270 hrs · 10,662 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANTS REPORTED SMELLING FUMES IN AFT & MID GALLEY. MX CONFERRED WITH FLIGHT CREW & WAS ADVISED OF A SWEET & THICK ODOR. UPON INSPECTION OF ACFT, FOUND ALL ENTRY DOOR CHANNELS SATURATED WITH DE-ICING FLUID. INITIAL REPORT OF FUMES OCCURRED AT GATE AFTER APPROX 1 HOUR ON GND WITH MAIN ENTRY DOOR & AFT DOORS OPENED. CLEANED GLYCOL FROM ALL DOORS & ACCOMPLISHED JC 33L00021001. TROUBLE SHOT CABIN AIR QUALITY. ENG RUNS & APU IN ALL CONFIGURATIONS WITH PACKS UNCOVERED, NO DEFECTS OR ODOR. OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 72,035 hrs · 10,607 cycles

AIRCRAFT WAS NOT GNDED, L3 DOOR EMER ASSIST CYLINDER PRESS NOT IN THE GREEN ZONE, IT’S IN THE YELLOW ZONE. SERVICED CYLINDER TO GREEN ZONE IAW JC 33L00005002.

Part: UNKNOWN — ODOR (CABIN) · airframe 71,913 hrs · 10,575 cycles

AIRCRAFT WAS GNDED. PASSENGERS AT SEAT 30 G & H REPORTED A SMELL & HAVING A HEADACHE. ACCOMPLISHED JC 33L00021001, NO ODOR NOTED. REPLACED HEPA FILTERS AS A PRECAUTIONARY ACTION. ACFT RETURNED TO SERVICE.

Part: MECHANISM — OBSTRUCTED (L4 DOOR) · airframe 71,889 hrs · 10,572 cycles

AIRCRAFT WAS NOT GNDED. 4L DOOR WILL NOT ARM. REMOVED DEBRIS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE DOOR ARMING MECHANISM.

Part: FITTING — DEFECTIVE (EVAC SLIDE) · airframe 71,817 hrs · 10,557 cycles

AIRCRAFT IN BASE MX. CONTROL NIT 22DH FAILS OPERATIONAL TEST. REPLACED SLIDE FITTING, ACCOMPLISHED ADJUSTMENT & OPERATIONAL CHECK IAW AMM 30-46-11-400-801D, 52-13-00-820-001 & 30-46-00-710-801D.

Part: LENS — BROKEN (EXIT SIGN) · airframe 71,816 hrs · 10,556 cycles

AIRCRAFT IN BASE MX. R3 DOOR OVERHEAD EXIT SIGN LENS IS BROKEN. R3 DOOR OVERHEAD EXIT SIGN LENS REPLACED IAW MM 33-51-16-04-01.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 71,816 hrs · 10,556 cycles

AIRCRAFT IN BASE MX. SEAT 24HG, EMER LIGHT HARNESS DAMAGED. REPLACED EMER LIGHT HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-803-A.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 71,816 hrs · 10,556 cycles

AIRCRAFT IN HEAVY MX. 3A EMER LIGHT HARNESS DAMAGED. REPLACED WIRE HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-803-A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 70,230 hrs · 10,319 cycles

ON WALK THRU FOUND 3L DOOR PRESS LOW. SERVICED L3 DOOR ASSIST BOTTLE IAW AMM 52-22-00-0600-801A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,003 hrs · 10,146 cycles

CABIN EMER LIGHTING BATTERY CAPACITY CHECK FAILED TEST. FAULTED EPSU 1L, 1R, 2L & 3L. REPLACED THE CABIN EMER LIGHT BATTERIES AT 1L, 1R, 2L, & 3L.

Part: DIAPHRAGM — RUPTURED (R4 DOOR) · airframe 68,863 hrs · 10,128 cycles

DURING DAILY CHECK FOUND DOOR R4 ASSIST ACTUATOR EMPTY. REPLACED RUPTURED DIAPHRAGM ON R4 DOOR EMER OPERATION CYLINDER.

Part: OVEN — ODOR (AFT GALLEY) · airframe 68,447 hrs · 10,072 cycles

AFT GALLEY ACFT RT OVEN NR 1 EXCESSIVE SMOKE. CB PULLED AS DIRECTED. R & R AFT GALLEY NR 1 OVEN.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 68,330 hrs · 10,057 cycles

R2 DOOR EMER OPERATION CYLINDER PRESS BELOW GREEN BAND. SERVICED R2 DOOR EMER OPERATIONS CYLINDER.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 68,330 hrs · 10,057 cycles

L3 DOOR EMER OPERATION CYLINDER, PRESS BELOW GREEN BAND. SERVICED L3 DOOR EMER OPERATION CYLINDER.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 68,216 hrs · 10,034 cycles

DOOR 3L REQUIRES ASSIST BOTTLE SERVICING. SERVICED 3L DOOR ASSIST BOTTLE.

Part: HOOK — BROKEN (CABIN) · airframe 67,901 hrs · 9,973 cycles

SEATS 26G & H O2 MASKS DROPPED ON TAKEOFF. FOUND HOOK BROKEN AT 17H-G & 36 A-B. REPLACED LATCH HOOKS & REPACKED MASKS AT SEATS 26 G & H.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 67,729 hrs · 9,930 cycles

DEU-1 15WL & 18WL FAIL EPSU SYS TEST. R & R EPSU ON 15WL & 18WL, R & R EPSU BATTERIES ON 15WL & 18WL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 67,729 hrs · 9,930 cycles

DEU-1 15WL FAIL EPSU SYS TEST. R & R EPSU ON 15WL, R & R EPSU BATTERIES ON 15WL.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 67,610 hrs · 9,906 cycles

3L DOOR ASSIST BOTTLE LOW. SERVICED THE 3L DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 67,276 hrs · 9,839 cycles

DOOR ASSIST BOTTLE PRESS IN YELLOW, NO ECAM MSG DOOR 3L. SERVICED DOOR ASSIST AS REQUIRED

Part: COVER — MISSING (EXIT SIGN) · airframe 67,202 hrs · 9,827 cycles

DOOR 3R EXIT SIGN COVER MISSING. RELOCATED & REPOSITIONED EMER EXIT LIGHT ASSEMBLY AT 3R.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 67,173 hrs · 9,822 cycles

CHECK DOOR PRESS 3L SHOWN ON FWD ATTENDANT PANEL. CHARGED CYLINDER AT DOOR 3L.

Part: FITTING — FAILED (L1 DOOR) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK L2 DOOR FWD ESCAPE SLIDE FITTING ASSEMBLY FAILED 04 OPERATIONS TEST. REPLACED L1 DOOR ESCAPE SLIDE GIRT BAR FITTING IAW AMM 30-46-11-PB401. GIRT BAR FITTING ADJUSTMENT GOOD IAW AMM 52-11-00-820-801-A. OPERATIONS TESTED GOOD IAW AMM 30-46-00-710-801-A.

Part: TERMINAL — LOOSE (CABIN)

C2 CHECK EMER LIGHTS ON SEATS 24G & H INOPERATIVE. FOUND TERMINAL OF EMER LIGHT AT SEAT 24G & H LOOSE. SECURED TERMINALS & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: TERMINAL — DISCONNECTED (CABIN)

C2 CHECK EMER LIGHTS INOPERATIVE ON SEATS. TROUBLE SHOT & FOUND TERMINAL DISCONNECTED. CONNECTED TERMINAL & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-801-401. SYS CHECKED NORMAL.

Part: WIRE HARNESS — DAMAGED (CABIN)

C2 CHECK EMER ESCAPE LIGHTING WIRE IS DAMAGED AT SEAT 4A. R & R WIRE HARNESS AT SEAT 4A. OPERATIONS CHECKED IAW AMM 33-51-12-400-814. SYS CHECKED NORMAL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 151EF BETWEEN FRAME 54 TO 57 & BETWEEN Y140 TO Y800. REPLACED IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 151NF BETWEEN FRAME 58 TO 60 & BETWEEN Y140 TO Y800. REPLACED FLOOR PANEL 151NF IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 132AG BETWEEN FRAME 37 TO 37.4 & BETWEEN -Y140 TO -Y800. REPLACED IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 132MF BETWEEN FRAME 25 TO 26.3 & BETWEEN -Y800 TO -Y1473. REPLACED IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 131LF BETWEEN FRAME 25 TO 26.3 & BETWEEN Y140 TO Y800. REPLACED FLOOR PANEL 131LF IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 9,806 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 132LF BETWEEN FRAME 25 TO 26.3 & BETWEEN -Y140 TO -Y800. REPLACED IAW SRM 53-02-00-201 PARA 5I FIG 211.

Part: BATTERY PACK — FAILED (CABIN) · airframe 66,835 hrs · 9,774 cycles

4L EMER BATTERY PACK FAILED DURING EPSU BATTERY CAP TEST, SELF-TEST OF BATTERY ILLUMINATED BATTERY LED. REMOVED 4L BATTERY PACK & INSTALLED SERVICEABLE BATTERY PACK. OPERATIONAL CHECK OF BATTERY SELF-TEST GOOD AT THIS TIME.

Part: COVER — DETACHED (CABIN) · airframe 64,880 hrs · 9,518 cycles

3L EXIT LIGHT COVER DETACHED. SECURED 3L EXIT LIGHT COVER, NOW OPERATES NORMAL.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 64,764 hrs · 9,504 cycles

CLT 4R DOOR EMERGENCY ASSIST BOTTLE PRESS IS LOW. SERVICED 4R DOOR BOTTLE.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 64,727 hrs · 9,498 cycles

DURING DAILY CHECK FOUND DOOR DAMPER 3 LT IN RED BAND. ADJUSTED DOOR DAMPER PRESS.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 64,499 hrs · 9,469 cycles

DOOR 2R ASSIST BOTTLE PRESS FOUND IN YELLOW BAND. SERVICED 2R ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 64,467 hrs · 9,465 cycles

3L DOOR BOTTLE ASSIST PRESS LOW. SERVICED 3L DOOR BOTTLE ASSIST.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 64,337 hrs · 9,449 cycles

CHECK DOOR PRESS MSG FOR 3L ON FLIGHT ATTENDANT PANEL. SERVICED 3L DOOR EMERGENCY OPERATION CYLINDER TO REQUIRED PRESS.

Part: SIGN — BROKEN (CABIN) · airframe 64,034 hrs · 9,404 cycles

CLT ROW 25 ACFT RT EXIT SIGN BROKEN. MX REPLACED LIGHT ASSEMBLY, CHECKED GOOD.

Part: ACTUATOR — INOPERATIVE (CABIN) · airframe 63,010 hrs · 9,253 cycles

CLT MULTIPLE OXYGEN MASKS FAILED DROP TEST. MAINTENANCE REPLACED ACTUATORS IN MULTIPLE CABIN LOCATIONS.

Part: COVER — WORN (EMERGENCY LIGHT) · airframe 62,915 hrs · 9,240 cycles

R3 DOOR EMERGENCY EXIT LIGHT COVER WORN. MAINTENANCE REPLACED EMERGENCY LIGHT COVER.

Part: ACTUATOR — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK O/H PANELS 23EF, 23GH, 24CD, 25AB, 25EF, 25GH, 26AB, 26EF FAILED DROP TEST. MAINTENANCE REPACKED O/H PANEL'S, REPLACED SOLENOID AT 25AB, 25EF, 26AB.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK OVERHEAD PANELS 17GH, 18AB, 18GH, 19EF, 19GH, 20AB, 20CD, 20GH FAILED DROP TEST. MAINTENANCE REPACKED O/H PANELS, REPLACED SOLENOID AT 17GH AND 18AB.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK OVERHEAD PANELS 14CD, 14GH, 15EF, 16AB, 16EF, 16GH, 17AB, 17CD FAILED DROP TEST. MAINTENANCE REPACKED OVERHEAD PANELS, REPLACED SOLENOID AT 16AB, 16EF, 16GH, 17AB, 17GH, 18AB.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

O2 MASK O/H PANELS 30GH, 31AB, 31EF, 31GH, 32EF, 32GH, 33AB, 34AB FAILED DROP TEST. MAINTENANCE RESTOWED PANELS AND REPLACED SOLENOIDS WHERE REQUIRED.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK OVERHEAD PANELS 11CD, 11EF, 11HG, 12AB, 12CD, 12EF, 12GH, 13AB FAILED DROP TEST. MAINTENANCE REPACKED OVERHEAD PANELS, REPLACED SOLENOID AT 11HG.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK O/H PANELS 34CD, 34EF, 35CD, 35EF, 36AB, 36EF, 36GH, 37AB FAILED DROP TEST. MAINTENANCE RESTOWED PANELS AND REPLACED SOLENOIDS AS REQUIRED.

Part: SOLENOID — FAILED (OXYGEN MASK) · airframe 62,726 hrs · 9,216 cycles

OXYGEN MASK O/H PANELS 37F, 38AB, 38CD, 39AB, 39CD, 39F, 40F, 40GH FAILED DROP TEST. MAINTENANCE RESTOWED AND REPLACED SOLENOIDS AS REQUIRED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 62,348 hrs · 9,164 cycles

LAV L33, EMERGENCY LIGHT COVER MISSING. MX REPLACED EMERGENCY LIGHT LENS AT L-33.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 61,872 hrs · 9,104 cycles

CIDS PANEL CAUTION LIGHT - LOW PRESSURE. MX SERVICED L3 DOOR ASSIST BOTTLE TO PROPER PRESSURE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 60,668 hrs · 8,949 cycles

FAP SHOWS L3 DOOR LOW PRESSURE. MX SERVICED DOOR L3 ASSIST BOTTLE.

Part: CYLINDER — LOW (L3 DOOR) · airframe 60,336 hrs · 8,902 cycles

THE 3L DOOR EMERGENCY OPERATION CYLINDER PRESSURE IS LOW. MAINTENANCE ACCOMPLISHED CHARGING OF 3L DOOR EMERGENY OPERATIONS CYLINDER PRESSURE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 59,832 hrs · 8,836 cycles

THE 3L DOOR CHECK DOOR PRESSURE LIGHT. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 59,832 hrs · 8,836 cycles

DURING DAILY CHECK FOUND DOOR 3L EMERGENCY ASSIST BOTTLE LOW. MAINTENANCE RE-INFLATED DOOR TO NOMINAL PRESSURE, GREEN BAND, NO FURTHER MESSAGE ON FAP AND CMS.

Part: VIDEO MONITOR — FAULTY (CABIN) · airframe 59,787 hrs · 8,830 cycles

PAX SEAT 16C VIDEO SCREEN EMITTING ELECTRICAL SMELL. MAINTENANCE REMOVED &REPLACED SEAT MONITOR AT SEAT 16C.

Part: VIDEO MONITOR — SMOKE (SEAT 41C) · airframe 59,748 hrs · 8,824 cycles

FLT 705 ENROUTE. PASSENGER OBSERVED VIDEO SCREEN SMOKING AT SEAT 41C. REPLACED THE SEAT VIDEO MONITOR.

Part: VIDEO MONITOR — SMOKE (CABIN) · airframe 59,702 hrs · 8,818 cycles

PAX STATED HE OBSERVED SMOKE BRIEFLY COME OUT OF SCREEN AT 15F. SMOKE ODOR BRIEFLY NOTICED BY CREW. CREW CONTINUED TO WORK. REPLACED VIDEO MONITOR AT 15F. OP'S CHECK OK.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,566 hrs · 8,799 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON BELLY FAIRING SUPPORT FRAME AT FR44, -Y57. REPAIRED BELLY FAIRING SUPPORT FRAME AT FR44, -Y57 IAW A330 SRM 53-35-14, 51-21-11 & 51-23-12.

Part: SHAFT — CONTAMINATED (EMERGENCY EXIT) · airframe 59,566 hrs · 8,799 cycles

C1 CHECK - EMERGENCY EXIT DOOR 3R FAILED OPERATIONAL CHECK OF THE INTERLOCK MECHANISM. INSPECTED EMERGENCY EXIT DOOR 3R & FOUND LOWERING SHAFT STICKING DUE TO EXCESSIVE CIC. DISASSEMBLED CLEANED LUBRICATED & REASSEMBLED IAW A330 AMM 52-22-21. PERFORMED OPERATIONAL CHECK OF THE INTERLOCK MECHANISM. OPS CHECK GOOD.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,566 hrs · 8,799 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON BELLY FAIRING SUPPORT FRAME AT FR44, -Y37. REPAIRED BELLY FAIRING SUPPORT FRAME AT FR44, -Y37 IAW A330 SRM 51-73-00, 53-35-14, 51-21-11 & 51-23-12.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 59,343 hrs · 8,767 cycles

ON CIDS PANEL CHECK DOOR PRESSURE 3L. MAINTENANCE SERVICED DOOR 3L EMERGENCY OPERATIONAL CYLINDER. OKAY FOR SERVICE. MESSAGE ON CIDS PANEL EXTINGUISHED.

Part: CONTROL HANDLE — DEFECTIVE (R2 DOOR) · airframe 59,223 hrs · 8,750 cycles

R2 DOOR WILL NOT CLOSE FROM OUTSIDE, BUT OPEN FUNCTION OPERATIONAL. IN SIDE OPERATION NORMAL. MAINTENANCE CLEANED DEBRIS FROM DOOR MECHANISM. DOOR OPERATES NORMALLY. REPLACED R2 EXTERNAL CONTROL HANDLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 58,978 hrs · 8,719 cycles

CLT - 3L DOOR BOTTLE PRESSURE READS LOW. MAINTENANCE SERVICED 3L DOOR BOTTLE PRESSURE TO PROPER LEVEL.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 58,932 hrs · 8,713 cycles

THE 3L DOOR PRESSURE LOW. MAINTENANCE SERVICED 3L DOOR CYLINDER.

Part: SIGN — DETACHED (CABIN) · airframe 58,166 hrs · 8,605 cycles

EXIT SIGN OVER 2-L DOOR FELL DOWN. MAINTENANCE REFITTED EXIT SIGN AT DOOR 2L.

Part: COVER — MISSING (CABIN) · airframe 57,400 hrs · 8,507 cycles

GALLEY A/C LEFT - EMERGENCY LIGHT ON WALL MISSING COVER. MAINTENANCE REPLACED MISSING LENS COVER. OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 57,400 hrs · 8,507 cycles

AFT 4L DOOR EMERGENCY LIGHT COVER MISSING. MAINTENANCE INSTALLED MISSING COVER. OK FOR SERVICE.

Part: HINGE — BROKEN (L2 DOOR) · airframe 57,400 hrs · 8,507 cycles

MID PAX 2L DOOR DIFFICULT ONLY TO CLOSE FROM OUTSIDE. MAINTENANCE FOUND TRIM HINGE IN DOOR, REMOVED, DOOR OPERATES OK.

Part: COVER — DETACHED (CABIN) · airframe 57,325 hrs · 8,497 cycles

A/C MID CABIN EXIT LIGHT COVER WILL NOT STAY ATTACHED. MAINTENANCE REPLACED LIGHT COVER FOR MID CABIN EXIT LIGHT, CHECKS OK.

Part: LENS — MISSING (CABIN) · airframe 57,258 hrs · 8,489 cycles

LHR - EMERGENCY LEFT COVER A/C LEFT NEXT TO LAV 73 COVER IS MISSING. REPLACED AFT LEFT EMERGENCY LIGHT LENS (NEXT TO LAV 73). OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,219 hrs · 8,483 cycles

PHL - F/A JUMPSEAT 1L FLASHLIGHT DEAD, NOT CHARGING. REPLACED BATTERY AND BREAKAWAY STRAP. OPS GOOD.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 55,523 hrs · 8,265 cycles

A 5.5 INCH LONG CRACK IN CROSSBEAM AT FR63 BETWEEN -Y1318 TO -Y2540. REPAIRED CROSSBEAM AT FR63 BETWEEN -Y1318 TO -Y2540 IAW EA 134646.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,523 hrs · 8,265 cycles

DOOR L3 WALL MOUNTED EXIT LENS NOT INSTALLED. INSTALLED NEW DOOR L3 WALL MOUNTED EXIT LENS LIGHT IAW AMM 33-51-13-400-801A.

Part: BEAM — CRACKED (ZONE 100) · airframe 55,523 hrs · 8,265 cycles

A 5.5 INCH LONG CRACK IN AFT CARGO DOOR ACTUATOR BEAM ASSEMBLY BETWEEN FR62 TO FR63, -Y1727. REPLACED AFT CARGO DOOR ACTUATOR BEAM ASSEMBLY IAW EA 134646 & SRM 51-42-11.

Part: PLACARD — DEFECTIVE (CABIN) · airframe 55,481 hrs · 8,259 cycles

3L DOOR EMERGENCY EXIT PLACARD ON CEILING KEEPS FALLING OFF. MAINTENANCE REFITTED DOOR 3L EMERGENCY EXIT LENS SATISFACTORY.

Part: COVER — MISSING (CABIN) · airframe 55,450 hrs · 8,255 cycles

MID GALLEY NEAR COMPARTMENT 3-18 EMERGENCY EXIT LIGHT COVER IS MISSING. MAINTENANCE REPLACED LENS COVER AT COMPARTMENT 3-18 MID GALLEY.

Part: SLIDE — MALFUNCTIONED (R2 DOOR) · airframe 55,289 hrs · 8,234 cycles

R2 DOOR WOULD NOT SHOW PROPERLY ARMED. CHUTE DEPLOYED BY MAINTENANCE. PRIOR TO 2R SLIDE BEING BLOWN, CAPTAIN REPORTED THE SLIDE WOULD NOT ARM. IT WAS SHOWING ARMED IN THE COCKPIT AND NOT ARMED ON FLIGHT ATTENDANT PANEL. MAINTENANCE REPLACED THE R2 DOOR SLIDE ASSEMBLY AND THE DIAPHRAGM AND SHEAR PIN ON THE DOOR EMERGENCY CYLINDER. ALL DOOR INDICATIONS NORMAL ON ECAM AND FLIGHT ATTENDANT PANEL.

Part: LENS — MISSING (CABIN) · airframe 54,189 hrs · 8,091 cycles

PHL - EMERGENCY PATHWAY LIGHTING LENS COVERS MISSING AT ROW 11B AND 16G. MAINTENANCE REPLACED MISSING LENS AT ROW 11 AND 16.

Part: ANGLE — DAMAGED (LT WING) · airframe 54,063 hrs · 8,073 cycles

WHILE PERFORMING THE CENTER WING BOX DRY BAY PERMANENT REPAIR ASSOCIATED WITH PREVIOUSLY SUBMITTED SDR USAA2011111500009, IT WAS NOTED THAT FASTENER HOLES 1 AND 2 ON LEFT HAND RIB 1 ANGLE WERE ELONGATED. THESE ELONGATED HOLES WERE REPAIRED PER EA 103502.

Part: ANGLE — DAMAGED (RT WING) · airframe 54,063 hrs · 8,073 cycles

WHILE PERFORMING THE CENTER WING BOX DRY BAY PERMANENT REPAIR ASSOCIATED WITH PREVIOUSLY SUBMITTED SDR USAA2011111500009, IT WAS NOTED THAT FASTENER HOLES 1 AND 2 ON RIGHT RIB 1ANGLE WERE ELONGATED. THESE ELONGATED HOLES WERE REPAIRED PER EA 103502.

Part: SEALANT — DAMAGED (FUEL TANK) · airframe 54,061 hrs · 8,072 cycles

FUEL LEAK - FUEL LEAKING FROM CENTER BOX DRY BAY DRAIN. LOCATED FUEL LEAK SOUCE IN DRY BAY AT CENTER SPAR FR42 AT RIB 1 LEFT LOWER CORNER ON FORWARD SIDE & NR 8 FASTENER, & ON AFT SIDE OF LEFT SEAM OPPISITE OF NR 8 FASTENER. PERFORMED TEMP REPAIR IAW SRM 51-76-12, LEAK CHECK SATISFACTORY.

Part: OVEN — FAULTY (GALLEY) · airframe 53,710 hrs · 8,026 cycles

MAN - BURNING SMELL COMING FROM OVEN NR 2, MID-GALLEY. OVEN WAS TURNED OFF AND F/A WAS INSTRUCTED TO PULL C/B. MAINTENANCE REMOVED AND REPLACED MID GALLEY OVEN IAW AMM 25-35-19-401, OPS CHECKS GOOD THIS CLEARS MEL # 25-22-03C.

Part: COVER — MISSING (CABIN) · airframe 52,830 hrs · 7,908 cycles

FRA - SEAT 6G EMERGENCY LIGHT COVER MISSING. MAINTENANCE REPLACED 6G EMERGENCY LIGHT COVER, OPERATIONAL CHECK IS OK.

Part: LENS — BROKEN (CABIN) · airframe 52,734 hrs · 7,896 cycles

CLT - 19B EXIT LIGHT BROKEN. MAINTENANCE REPLACED BROKEN LENS.

Part: COVER — LOOSE (EXIT SIGN)

LGW EXIT SIGN COVER NEAR ROW 21 FALLS OFF. MAINTENANCE REFITTED EXIT SIGN AT 3L. OPS OK.

Part: SWITCH — FAULTY (CABIN)

CLT - WITH EMERGENCY LIGHT SWITCH IN ARM, THE EMERGENCY EXIT LIGHTS ILLUMINATED WHEN ELECTRICAL POWER SOURCE IS CHANGED, REQUIRING CYCLING OF EMERGENCY EXIT LIGHT SWITCH. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT TOGGLE SWITCH.

Part: EPSU — FAULTY (CABIN)

MAD - FLT 741 EN ROUTE MAD TO PHL. THE EMERGENCY LIGHTS STAYED ON WHEN ARMED. THE FLIGHT RETURNED TO GATE WITHOUT FURTHER INCIDENT. EPSU 3R REPLACED.

Part: RIB — CRACKED (RT WING) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CRACK ON RIGHT WING RIB 6 AT AFT FUEL LINE CUTOUT. REPAIRED RIGHT WING RIB 6 AT AFT FUEL LINE CUTOUT IAW EA 1344158, EO 5706U238 AND DRAWING R572-57026.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 GALVANIC CORROSION STRINGER SHEAR TIE AT FR39.1 BETWEEN S50R TO S51R. REPLACED STRINGER SHEAR TIE AT FR39.1 BETWEEN S50R TO S51R IAW EA 134480.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 WIDESPREAD GALVANIC CORROSION ON STRINGER FITTING AT FR40 BETWEEN S43 TO FR45. REPAIRED STRINGER FITTING AT FR40 BETWEEN S43 TO FR45 IAW A330 SRM EA 134414.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 GALVANIC CORROSION ON STRINGER SHEAR TIE AT FR39.2 BETWEEN S50R TO S51R. REPLACED STRINGER SHEAR TIE AT FR39.2 BETWEEN S50R TO S51R IAW EA 134478.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CRACKS ON ANGLE CHORD AT FR 42, RIB 1 ON LEFT AND RIGHT SIDES. REPAIRED ANGLE CHORD AT FR 42, RIB 1 ON LEFT AND RIGHT SIDES IAW EA 134477.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 EXFOLIATION CORROSION ON BULK CARGO FLOOR SUPPORT AT FR67, -Y563. REPLACED BULK CARGO FLOOR SUPPORT AT FR67, -Y563 IAW A330 SRM 53-41-14, 51-74-00 & 51-42-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 GALVANIC CORROSION ON KEEL BEAM FORWARD CONTINUITY FITTING FORWARD OF FR40, -Y819. REPLACED KEEL BEAM FORWARD CONTINUITY FITTING FORWARD OF FR40, -Y819 IAW A330 SRM 51-42-11, SRM 51-44-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

LEVEL 2 GALVANIC CORROSION ON STRINGER FITTING 10 INCHES FORWARD OF FR40, S50R. REPLACED STRINGER AT FR40, S50R IAW A330 SRM 53-00-14, SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

CORRODED STRINGER END FITTING FORWARD OF FR40, S46R. REPLACED STRINGER END FITTING FORWARD OF FR40, S46R IAW A330 SRM 53-31-13 & 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

CORRODED ON STRINGER END FITTING AT FR40, S49R. REPLACED STRINGER END FITTING AT FR40, S49R IAW A330 SRM 53-31-00 FIG 101, 51-42-11 & 51-74-00.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

A 0.600" LONG CRACK ON FORWARD CARGO DOOR BEAM NR 1 AT FR22A NEAR ACTUATOR FITTING. REPAIRED FORWARD CARGO DOOR BEAM NR 1 AT FR22A NEAR ACTUATOR FITTING IAW EA 134458.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 51,816 hrs · 7,768 cycles

CORROSION, D=6.0", W=.5", D=.04 ON SEAT TRACK BETWEEN FR53.6 TO FR53.7, Y1552.5. REPLACED SEAT TRACK BETWEEN FR53.6 TO FR53.7, Y1552.5 IAW SRM 51-42-11 & SRM 53-00-15.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR 16, Y1456. REPLACED LONGITUDINAL BEAM AT FR 16, Y1456 IAW A330 SRM 53-11-14, SRM 51-72-11, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR 32 TO FR 37, -Y953. REPLACED SEAT TRACK BETWEEN FR 32 TO FR 37, -Y953 IAW A330 SRM 53-00-15, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM -S2 CHECK - CORROSION ON SEAT TRACK AT FR 18, -Y450. REPLACED SEAT TRACK AT FR 18, -Y450 IAW A330 SRM 53-00-15 FIGURE 101, 51-44-11, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR 16A, -Y1456. REPLACED SEAT TRACK AT FR 16A, -Y1456 IAW A330 SRM 53-11-15 FIG 101, 51-42-11, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM -S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR 14B, -Y450. REPLACED SEAT TRACK AT FR 14B, -Y450 IAW A330 SRM 53-11-15 FIG 101, 51-42-11, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK AT FR 57.3 - FR 58, +Y450. REPLACED SEAT TRACK AT FR 57.3 - FR 58, +Y450 IAW SRM 53-00-15, SRM 51-27-11, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK AT FR 59 - FR62, Y450. REPLACED SEAT TRACK AT FR 59 - FR62, Y450 IAW A330 SRM 53-00-15, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK AT FR 37 - FR 38, Y450. REPLACED SEAT TRACK AT FR 37 - FR 38, Y450 IAW A330 SRM 53-00-15 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33 - FR 36, -Y2462. REPLACED SEAT TRACK AT FR 33 - FR 36, -Y2462 IAW A330 SRM 53-21-15 SRM 51-42-11 SRM 51-44-11 SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK AT FR 32 - FR 35, -Y1959. REPLACED SEAT TRACK AT FR 32 - FR 35, -Y1959 IAW A330 SRM 53-00-15 FIG 102, 51-44-11 & SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK RAIL AT FR 53.5 - FR53.6, +Y2462. REPLACED SEAT TRACK RAIL AT FR 53.5 - FR53.6, +Y2462 IAW A330 SRM 53-31-15 FIG 101, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK RAIL, AT FR 54, -Y1959. REPLACED SEAT TRACK RAIL, AT FR 54, -Y195 IAW A330 SRM 53-00-15 FIG 101 51-44-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON SEAT TRACK / RAIL AT FR 53.4 - FR 53.5, -Y450. REPLACED SEAT TRACK / RAIL AT FR 53.4 - FR 53.5, -Y450 IAW SRM 53-31-15 FIG 101, SRM 53-31-15 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN 12 INCHES FORWARD OF FR33 TO 2 INCHES AFT OF FR33, Y1456. REPLACED SEAT TRACK BETWEEN 12 INCHES FORWARD OF FR33 TO 2 INCHES AFT OF FR33, Y1456 IAW A330 SRM 53-00-15, 51-42-11, 51-42-14 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK RAIL BETWEEN FR32 TO FR33, Y953. REPLACED SEAT TRACK RAIL BETWEEN FR32 TO FR33, Y953 IAW A330 SRM 53-00-15, 51-42-11 & 51-72-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON CROSS BEAM AT FR 75A, +794.3 TO +Y1137.1. REPLACED CROSS BEAM AT FR 75A, +794.3 TO +Y1137.1 IAW A330 SRM 51-42-11, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR31 TO FR32, -Y953. REPLACED SEAT TRACK BETWEEN FR31 TO FR32, -Y953 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 33, +Y450 TO -Y450. REPAIRED FLOORBEAM AT FR 33, +Y450 TO -Y450 IAW EA 134433.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR 16A, -Y1959. REPLACED LONGITUDINAL BEAM AT FR 16A, -Y1959 IAW A330 SRM 53-11-14, SRM 51-73-00, SRM 51-42-11, SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y2055.3. REPLACED SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y2055.3 IAW A330 SRM 53-31-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, Y450 IAW A330 SRM 51-72-11, 51-42-11 & 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR53.3 TO FR53.5, Y1959. REPLACED SEAT TRACK BETWEEN FR53.3 TO FR53.5, Y1959 IAW A330 SRM 53-31-15, 51-73-00, 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR 73, Y1137.1. REPLACED FLOOR SUPPORT BEAM AT FR 73, Y1137.1 IAW A330 SRM 53-00-15, SRM 51-42-11, SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR 71, Y=0. REPLACED LONGITUDINAL BEAM AT FR 71, Y=0 IAW A330 SRM 53-41-14, SRM 51-42-11, SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK 8.5 INCHES FORWARD FROM FR59, Y1959. REPLACED SEAT TRACK 8.5 INCHES FORWARD FROM FR59, Y1959 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR73, Y1447.8. REPLACED FLOOR SUPPORT BEAM AT FR73, Y1447.8 IAW A330 SRM 53-00-15, SRM 51-74-00, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK AT FR48, -Y450. REPLACED SEAT TRACK AT FR48, -Y450 IAW A330 SRM 51-42-11, 53-31-15 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR 14 - FR 17, -Y953. REPLACED SEAT TRACK AT FR 14 - FR 17, -Y953 IAW A330 SRM 53-11-15, 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON LONGERON BEAM AT FR 73A, -Y1447.8. REPLACED LONGERON BEAM AT FR 73A, -Y1447.8 IAW A330 SRM 51-74-00, 51-72-11, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR32 TO FR37, -Y450. REPLACED SEAT TRACK BETWEEN FR32 TO FR37, -Y450 IAW A330 SRM 51-42-11, 53-00-15 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK AT FR73, Y1137.1. REPLACED SEAT TRACK AT FR73, Y1137.1 IAW A330 SRM 51-42-11, 53-41-14 & 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR LONGITUDINAL BEAM AT FR 71, Y794.3. REPLACED FLOOR LONGITUDINAL BEAM AT FR 71, Y794.3 IAW A330 SRM 53-41-14,SRM 51-74-00, SRM 51-42-11, SRM 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR 33, Y= 0. REPLACED FLOOR SUPPORT AT FR 33, Y= 0 IAW A330 SRM 53-00-15 FIG 101 & 51-74-00,51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR33 TO FR35, -Y1456. REPLACED SEAT TRACK BETWEEN FR33 TO FR35, -Y1456 IAW A330 SRM 53-00-15, 51-42-11, 51-75-12 & 51-74-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR LONGITUDINAL BEAM AT FR 13A, -Y721.6. REPLACED FLOOR LONGITUDINAL BEAM AT FR 13A, -Y721.6 IAW A330 SRM, 53-11-14,SRM 51-42-11, SRM 51-44-11 SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR 13B, -Y953. REPLACED SEAT TRACK AT FR 13B, -Y953 IAW A330 SRM 53-11-15

Part: FASTENER — LOOSE (CENTER WING) · airframe 51,816 hrs · 7,768 cycles

CLT - TRACES OF FUEL HAVE BEEN FOUND IN THE CENTER WING DRY BAY OF A330-300 AIRCRAFT AT RIB 1. AS A RESULT OF THIS AN INSPECTION WAS PERFORMED ON THIS AIRCRAFT & FASTENERS WERE FOUND LOOSE & LEAKING AT FR42 LEFT & RIGHT SIDE AT RIB 1. BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102839B &102875A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR70 TO FR71, Y450. REPLACED SEAT TRACK BETWEEN FR70 TO FR71, Y450 IAW A330 SRM IAW A330 SRM 53-00-15, 51-42-11, 51-27-11 & 51-74-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR32 TO FR34, -Y1522.5. REPLACED SEAT TRACK BETWEEN FR32 TO FR34, -Y1522.5 IAW A330 SRM 53-00-15, 51-42-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR 73, +Y1137.1 TO +Y1447.8. REPLACED FLOOR SUPPORT AT FR 73, +Y1137.1 TO +Y1447.8 IAW A330 SRM 53-41-14 FIG 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR18 TO FR19, Y1456. REPLACED SEAT TRACK BETWEEN FR18 TO FR19, Y1456 IAW A330 SRM 53-00-15, 51-42-11, 51-72-11 & 51-74-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR53.7 TO FR53.9, -Y1552. REPAIRED SEAT TRACK BETWEEN FR53.7 TO FR53.9, -Y1552 IAW A330 SRM 53-31-15, 51-74-00 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK AT FR30, -Y953. REPLACED SEAT TRACK IAW A330 SRM 53-00-15.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK LONGERON ADAPTER BETWEEN FR73 TO FR74, -Y794.3. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y794.3 IAW A330 SRM 53-41-15, 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK AT FR66, Y450. REPLACED SEAT TRACK AT FR66, Y450 IAW A330 SRM 53-00-15, 51-44-12 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR30 TO FR37, Y1959. REPLACED SEAT TRACK BETWEEN FR30 TO FR37, Y1959 IAW A330 SRM 53-00-15, 51-72-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK BETWEEN FR53.5 TO FR53.6, Y450. REPLACED SEAT TRACK BETWEEN FR53.5 TO FR53.6, Y450 IAW A330 SRM 53-00-15, 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON CROSS BEAM AT FR37A, +Y1137.1 TO -Y794.3. REPLACED CROSS BEAM AT FR37A, +Y1137.1 TO -Y794.3 IAW A330 SRM 53-41-14, 5174-00 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 35 - FR 37, Y=0. REPLACED FLOOR SUPPORT AT FR 35 - FR 37, Y=0 IAW A330 SRM 53-00-15 FIG 101 SHT 2, SRM 51-44-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 73A - FR 74, +Y1147.4. REPLACED FLOOR SUPPORT AT FR 73A - FR 74, +Y1147.4 IAW A330 SRM 53-41-14 FIG 101 SHT 2, SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON CROSS BEAM AT FR 73A - 3", +Y1447.8 TO -Y 1137.1. REPLACED CROSS BEAM AT FR 73A - 3", +Y1447.8 TO -Y 1137.1 IAW A330 SRM 53-41-14, SRM 51-42-11, SRM 51-44-11, SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 72, -Y794.3. REPLACED FLOOR SUPPORT AT FR 72, -Y794.3 IAW A330 SRM 53-41-14 FIG 103, SRM 51-42-11, SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 - CORROSION ON SEAT TRACK AT FR30, Y450. REPAIRED SEAT TRACK AT FR30, Y450 IAW A330 SRM 53-00-15 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR 73 - FR 75, -Y794.3. REPLACED FLOOR SUPPORT BEAM AT FR 73 - FR 75, -Y794.3 IAW A330 SRM 51-42-11 AND 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,816 hrs · 7,768 cycles

BFM - S2 CHECK - CORROSION ON FLOOR SUPPORT PROFILE AT FR 82, -Y450. REPLACED FLOOR SUPPORT PROFILE AT FR 82, -Y450 IAW A330 SRM 51-42-11, SRM 53-41-14-101.

Part: BATTERY — FAILED (CABIN)

PHL - THE R3 AND L4 EPSU BATTERIES FAILED EPSU CAPACITY TEST. REPLACED EPSU BATTERIES AT R3 AND L4 ENTRY DOORS.

Part: FUSE — FAILED (POWER SUPPLY)

THE EMERGENCY POWER SUPPLY UNIT (EPSU) AT L2 ENTRY SHOWS "UNIT FAULT" WHEN TESTED. REPLACED L2 EPSU. RE-SOLDERED WEAK CONNECTIONS UNDER CONVERTER U12. REPLACED PARTS (FUSE 4A 250 TR5T19372-4A, MPN 779-435-73), UNIT ASSEMBLED, CLEANED AND PASSED FUNCTIONAL TEST.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

LGW - THE EMERGENCY TORCH AT DOOR L3 DOES NOT FLASH. TORCH BATTERY REPLACED.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EPSU AT DOOR R1 FAILS JOBCARD BAT CAP TEST. REPLACED BATTERY AT EPSU DOOR R1.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EPSU AT DOOR L2 FAILS JOBCARD BAT CAP TEST. REPLACED BATTERY AT EPSU DOOR L2.

Part: LINKAGE — OBSTRUCTED (L2 DOOR)

PHL - ACCOMPLISH L2 SLIDE/RAFT OPERATIONAL CHECK. ESCAPE SLIDE/RAFT OPERATIONAL CHECK ACCOMPLISHED - SLIDE FAILED. REMOVED AND REPLACED L2 SLIDE/RAFT ASSEMBLY. REMOVED AND REPLACED L2 DOOR ASSIST BOTTLE. THE SLIDE DID NOT RELEASE FROM PACK, KEPT DOOR FROM OPENING. FURTHER INVESTIGATION REVEALED THAT THE SHIPPING NUT HAD BEEN LEFT ON THE DOOR ASSIST LINKAGE SPRING ROD ASSEMBLY.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,890 hrs · 6,967 cycles

CABIN FLOOR PANEL NR 148FL DAMAGED BETWEEN FR 73 TO FR 75, REPAIRED CABIN FLOOR PANEL NR 148FL IAW SRM 53-02-00.

Part: WIRE — BROKEN (CABIN) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - EEL - SEVERAL IN SEAT EMERGENCY LIGHTS ARE INOPERATIVE. REPAIRED BROKEN WIRES AT 5GH, 6GH, 13AB, 31GH, 38GH IAW AIRBUS ESPM 20-40-00 AND 20-53-29.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BEAM FLOOR SUPPORT BETWEEN FR74 & FR80/82, -Y794.3. REPLACED LONGERON BEAM FLOOR SUPPORT BETWEEN FR74 & FR80/82, -Y794.3 IAW A330 SRM 51-42-11, 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR74 & FR80/82, Y1137.1. REPLACED FLOOR SUPPORT BETWEEN FR74 & FR80/82, Y1137.1 IAW A330 SRM 51-42-11 & 51-27-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BEAM LONGERON BETWEEN FR72 & FR76, BL 0. REPLACED FLOOR SUPPORT BEAM LONGERON BETWEEN FR72 & FR76, BL 0 IAW A330 SRM 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR75 & FR78, Y450. REPLACED FLOOR SUPPORT BETWEEN FR75 & FR78, Y450 IAW A330 SRM 53-41-14 & 51-42-12.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BEAM BETWEEN FR77 & FR78, BL 0. REPLACED LONGERON BEAM BETWEEN FR77 & FR78, BL 0 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1- MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR74 TO FR75, Y450. REPLACED SEAT TRACK BETWEEN FR74 TO FR75, Y450 IAW A330 SRM 51-00-15 & 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BEAM BETWEEN FR78 & FR79, BL 0. REPLACED LONGERON BEAM BETWEEN FR78 & FR79, BL 0 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR75 & FR76, -YA THRU -Y1447.8. REPLACED FLOOR SUPPORT BETWEEN FR75 & FR76, -YA THRU -Y1447.8 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR74 & FR75, Y450. REPLACED SEAT TRACK BETWEEN FR74 & FR75, Y450 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT BETWEEN FR72 & FR80/82, Y794.3. REPLACED CABIN FLOOR SUPPORT BETWEEN FR72 & FR80/82, Y794.3 IAW A330 SRM 51-74-00 & 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BEAM BETWEEN FR74 & FR77.5, -Y1447.8. REPLACED LONGERON BEAM BETWEEN FR74 & FR77.5, -Y1447.8 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR75 & FR80, Y450. REPLACED LONGERONS BETWEEN FR75 & FR80, Y450 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR75 & FR80, -Y450. REPLACED LONGERONS BETWEEN FR75 & FR80, -Y450 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR77 & FR80/82, Y1447.8. REPLACED LONGERON BETWEEN FR77 & FR80/82, Y1447.8 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 & FR74, YC1. REPLACED SEAT TRACK BETWEEN FR73 & FR74, YC1 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR77 & FR80/82, -Y1447.8. REPLACED LONGERON BETWEEN FR77 & FR80/82, -Y1447.8 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 & FR74, -YC1. REPLACED SEAT TRACK BETWEEN FR73 & FR74, -YC1 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR74 & FR80/82, -Y1137.1. REPLACED LONGERON BETWEEN FR74 & FR80/82, -Y1137.1 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,890 hrs · 6,967 cycles

BFM - C1 - MAJOR REPAIR - CORROSION ON LONGERON BETWEEN FR72 & FR74, Y794.3. REPLACED LONGERON BETWEEN FR72 & FR74, Y794.3 IAW A330 SRM 51-42-11, 51-44-11, 51-40-00.

Part: BATTERY — DISCHARGED (CABIN)

MAN - EMERGENCY TORCH INDICATOR LIGHT DIM AT LEFT FORWARD ATTENDANT'S POSITION. REPLACED BATTERY.

Part: SLIDE — FAULTY (R2 DOOR)

PHL - OPS CHECK OF EMERGENCY LIGHTS VEA MCDU FAILED ATA 256241 ESCAPE SLIDE LT SW/EPSU 2R14WL. REPLACED R2 DOOR SLIDE.

Part: SLIDE — FAILED (L3 DOOR)

PHL - OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA MCDU FAILED ATA 25 62 41 ESCAPE SLIDE LT SW/ EPSU 3L 13WL. REMOVED AND REPLACED L3 EMERGENCY EXIT SLIDE RAFT.

Part: BOTTLE — LOW PRESSURE (R1 DOOR)

PHL - THE R1 DOOR ASSIST BOTTLE WAS IN YELLOW BAND FOR PSI. SERVICED THE R1 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L4 DOOR)

PHL - THE L4 DOOR ASSIST BOTTLE WAS IN YELLOW BAND FOR PSI. SERVICED THE R1 DOOR ASSIST BOTTLE.

Part: ATTACH BOLT — SHEARED (R4 DOOR)

PHL - THE R4 DOOR DAMPER ATTACH BOLT SHEARED. INSTALLED NEW ATTACH BOLT.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

PHL - THE L3 DOOR ASSIST BOTTLE WAS IN YELLOW BAND FOR PSI. SERVICED THE R1 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

PHL - THE L1 DOOR ASSIST BOTTLE WAS IN YELLOW BAND FOR PSI. SERVICED THE R1 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

CLT - THE L3 DOOR EMERGENCY ASSIST BOTTLE READS LOW. MAINTENANCE SERVICED THE L3 DOOR EMERGENCY ASSIST BOTTLE.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EPSU SYSTEM TEST INDICATED FAULT "BAT/EPSU 1L" (11WL). MAINTENANCE REPLACED THE POWER SUPPLY BATTERY AT DOOR L1. OPERATIONALLY CHECKS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAN - THE R-4 DOOR FLASHLIGHT BELOW THE FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES TO THE FLASHLIGHT. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON FLOOR SUPPORT, BS 5759/FR 75, +Y350 TO +Y450. REPAIRED FLOOR SUPPORT, BS 5759/FR 75, +-Y350 TO +Y450 IAW USAIRWAYS EA 134009.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON FLOOR SUPPORT, BS 5759/FR 75, -Y350 TO -Y450. REPAIRED FLOOR SUPPORT, BS 5759/FR 75, -Y350 TO -Y450 IAW USAIRWAYS EA 134009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5367 / FR 73, -Y450. REPLACED CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5367 / FR 73, -Y450 IAW A330 SRM 51-42-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5759 / FR 75, +Y450. REPAIRED CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5759 / FR 75, +Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4842 / FR 58, +Y1959. REPAIRED CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4842 / FR 58, +Y1959 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4895 / FR 59 - BS 5160 / FR 64, +Y450. REPAIRED CABIN SEAT TRACK, BS 4895 / FR 59 - BS 5160 / FR 64, +Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4682 / FR 57.2, -Y450. REPAIRED CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4682 / FR 57.2, -Y450 IAW A330 SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,527 hrs · 5,985 cycles

BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON CABIN SEAT TRACK, BS 4258 / FR 53.7 - BS 4417 / FR 54, -Y450. REPAIRED CABIN SEAT TRACK, BS 4258 / FR 53.7 - BS 4417 / FR 54, -Y450 IAW A330 SRM 53-31-15.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FRA - THE LEFT AFT INBOARD FLIGHT ATTENDANT SEAT FLASHLIGHT LOCATED UNDERNEATH THE SEAT DOES NOT WORK. MAINTENANCE REPLACED THE BATTERY OF THE LEFT AFT INBOARD FLIGHT ATTENDANT SEAT FLASHLIGHT. OPERATIONALLY CHECKS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAN - THE EMERGENCY FLASHLIGHT AT D1L (OUTBOARD SEAT) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT BATTERY. OPERATIONALLY CHECKS OK.

Part: TERMINAL BLOCK — FAILED (WINDOW HEAT)

PHL CLT-LGW FLT NR 704, CREW REPORTED L1 WINDOW NOT HEATING, FLIGHT DIVERTED TO PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TERMINAL BLOCK 301VT. OPS CHECKS OK.

Part: EPSU — FAULTED (EMERGENCY LIGHTS)

PHL - THE DOOR R3 EMERGENCY POWER SUPPLY UNIT (EPSU), FIN 16WL, FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED EPSU, FIN 16WL, ABOVE DOOR R3. OPERATIONALLY CHECKS OK.

Part: ADIRU — FAILED (NR 1)

PHL FLT 754 PHL-CDG EN ROUTE CREW THE NUMBER 1 ADIRU BECAME INOP. DUE TO PROCEDURAL ISSUES FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED NUMBER 1 ADIRU.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 35,586 hrs · 5,582 cycles

MAINTENANCE FOUND THE 3R EMERGENCY LIGHT POWER SUPPLY FAULTED. REPLACED POWER SUPPLY.

Part: FIRE DETECTOR — FAILED (NR 2 ENGINE) · airframe 30,847 hrs · 4,925 cycles

FLIGHT 26, PHL-CDG: AFTER TAKEOFF, THE WARNING LIGHT ON THE NUMBER TWO ENGINE FIRE HANDLE ILLUMINATED. NO OTHER ASSOCIATED WARNINGS. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE NUMBER TWO FIRE DETECTION UNIT. NO FURTHER FAULTS.