N273AY

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 87,212 hrs · 12,303 cycles

AIRCRAFT WAS GROUNDED: 4L EMERGENCY LIGHT BATTERY INOPERABLE. MAINTENANCE REPLACED EMERGENCY BATTERY PACK PER STANDARD PRACTICES.

Part: LINK — LACK OF LUBE (R3 DOOR) · airframe 87,178 hrs · 12,294 cycles

AIRCRAFT WAS GROUNDED: DURING R3 SLIDE CHANGE, R3 DOOR CONSTANTLY SHOWS OPEN, ARMED. FOUND PROX SW 20MJ (TOP DOOR FRAME) ACTUATOR LINKAGE HARD TO MOVE. LUBRICATED LINKAGE, R3 DOOR WARNING OPS CKS OK IAW AMM 52-71-00-710-801-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 86,829 hrs · 12,228 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO DUB ON ACCOUNT OF CREW MEDICAL CHEMICAL SPILL IN THE MAIN CABIN TWO FLIGHT ATTENDANTS LOSS OF CONSCIOUSNESS. EMERGENCY DECLARED. MAINTENANCE REPORTS ACCOMPLISHED SMOKE ODOR FUMES WORK CARD 33L0021001. NO EVIDENCE OR DEFECTS. HAZMAT TEAM TO DEEP CLEAN CABIN. HAZMAT TEAM FOUND NO DEFECTS. MAINTENANCE CANNOT FIND ANY ODOR. A/C OK FOR SERVICE.

Part: FAN — ODOR (GALLEY) · airframe 86,589 hrs · 12,197 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ELECTRICAL ODOR CONCENTRATED AT DOOR 4R, GALLEY LAVATORY DISSIPATED SOMEWHAT AS FLIGHT CONTINUED. F/A + PILOT COULD NOT IDENTIFY SOURCE OF ODOR. MAINTENANCE ACCOMPLISHED JOB CARD 33L00021001 (SMOKE ODOR FUMES INITIAL TROUBLESHOOTING) SUSPECT ODOR COMING FROM AFT GALLEY EXTRACT FAN. REMOVED AND REPLACED EXTRACT FAN IAW AMM 21-23-51. OPS CHECKS OK. INSPECTED AFT GALLEY AND LAVS, NO ODOR NOTED.

Part: TRANSMITTER — LEAKING (WASTE TANK) · airframe 85,254 hrs · 12,025 cycles

AIRCRAFT WAS GROUNDED: F/A'S REPORT STRONG ODOR OF URINE IN AFT CABIN. MAINTENANCE REPLACED FWD WASTE TANK LIQUID LEVEL TRANSMITTER IAW AMM 38-31-11. AREA CLEANED BY CLEANING VENDORS. NO LEAKS NOTED.

Part: FIRE BOTTLE — LOW PRESSURE (LAVATORY) · airframe 83,463 hrs · 11,773 cycles

AIRCRAFT WAS GROUNDED: L54 LAVATORY FIRE BOTTLE LOW. MAINTENANCE REPLACED FIRE BOTTLE PER AMM 26-25-41.

Part: MEGAPHONE — INTERMITTENT (FWD CABIN) · airframe 83,463 hrs · 11,773 cycles

MEGAPHONE IN THE FORWARD CABIN, TRANSMITS INTERMITTENTLY. REPLACED THE MEGAPHONE. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 83,428 hrs · 11,766 cycles

R2 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW 52-10-00.

Part: STRINGER — CRACKED (FRAME 53.5) · airframe 80,190 hrs · 11,358 cycles

CRACK INDICATION ON STRINGER 14L, FR 53.8. REPAIRED THE STRINGER IAW EA 278184.

Part: PROFILE — CRACKED (FRAME 53.5) · airframe 80,190 hrs · 11,358 cycles

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

Part: STRINGER — CRACKED (FRAME 53.5) · airframe 80,126 hrs · 11,349 cycles

STRINGER 15L CRACKED AT FRAME 53.5. REPLACED THE STRINGER IAW SRM 51-72-11, 51-42-11 AND DRAWING F53370020.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,346 hrs · 11,230 cycles

FWD FLIGHT ATTENDANT PANEL (CIDS) EMERGENCY LIGHT SWITCH DOES NOT OPERATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT PANEL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 79,140 hrs · 11,201 cycles

AIRCRAFT WAS NOT GROUNDED. MULTIPLE EMERGENCY LIGHTS INOPERABLE ON LEFT SIDE OF AIRCRAFT IN MIDDLE AND AFT COACH CABIN. CANNON PLUG FOUND TO BE DISCONNECTED, ACCOMPLISHED RECONNECTION PER AMM 33-51-38.

Part: LENS — MISSING (CABIN) · airframe 78,894 hrs · 11,163 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT COVER MISSING L74. REPLACED LENS COVER.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 78,525 hrs · 11,117 cycles

OPS CHECK OF THE EMERGENCY LIGHT SYSTEM FAILED. EPSU SYSTEM TEST SHOWS CLASS 1 EPSU 14WL. REPLACED EPSU.

Part: SLIDE — NO TEST (R2 DOOR) · airframe 78,525 hrs · 11,117 cycles

OPS CHECK OF EMERGENCY LIGHT SYSTEM FAILED. EPSU SYSTEM TEST SHOWS CLASS 1 EPSU 14WL. FOUND R2 SLIDE AT FAULT. REPLACED R2 SLIDE.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 78,427 hrs · 11,105 cycles

AIRCRAFT WAS NOT GROUNDED. 3L DOOR EXIT SIGN FELL OFF. REPLACED EMERGENCY LIGHT LENS COVER.

Part: LIGHT — BROKEN (LAVATORY) · airframe 78,336 hrs · 11,094 cycles

EMERGENCY STAND BY LIGHT IN LAVATORY L34 BROKEN. REPLACED THE EMERGENCY LIGHT. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 77,817 hrs · 11,027 cycles

AIRCRAFT WAS NOT GROUNDED. DURING DAILY CHECK FOUND UPPER FLASHLIGHT AT DOOR 3R BATTERY DEFECTIVE. REPLACED UPPER FLASHLIGHT BATTERY AT DOOR 3R.

Part: FLASHLIGHT — DISCHARGED (CABIN) · airframe 77,000 hrs · 10,927 cycles

FLASHLIGHT AT THE L4 DOOR INBOARD JUMPSEAT IS INOPERATIVE. SECURED FLASHLIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GUARD — BENT (ZONE 800) · airframe 76,001 hrs · 10,798 cycles

AIRCRAFT WAS GROUNDED. DURING REPLACEMENT OF R2 DOOR SLIDE RAFT PER JOB CARD 33L00025001, FOUND RELEASE LEVER GUARD BENT ON GIRT BAR. ACCOMPLISHED GVI, COLD WORKED GIRT BAR LOCK PLATE TO ORIGINAL FLAT CONTOUR AND ACCOMPLISHED HFEC TO LOWER PLATE.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 75,043 hrs · 10,623 cycles

AIRCRAFT WAS NOT GROUNDED. 1R DOOR HANDLE STUCK. MAINTENANCE FOUND AND REMOVED DEBRIS FROM GIRT BAR TRACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 52-10-00.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON FORWARD CARGO DOOR INNER SKIN, FORWARD OF ACTUATOR ATTACHMENT FITTING AT FR 22A BETWEEN BEAM 1 AND 2. REPAIRED INNER SKIN PER EA 263971.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOORBEAM BETWEEN FR 75A AND FR 76 AT Y2462. REPLACED FLOORBEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK BETWEEN FR 37 AND FR 37.1 AT -Y953. REPLACED SEAT TRACK PER SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y1447.8 AND FR 78. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT FR 67 AND Y1959. REPLACED SEAT TRACK PER SRM 51-42-11, SRM 53-00-15 AND SRM 53-41-15 FIG 202.

Part: FLOOR SUPPORT — CORRODED (BS 75-78) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 75 AND 78 AT Y380. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-80) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 75 AND 80 AT Y450. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOORBEAM AT FRAME 73A BETWEEN Y1993 AND Y2462. REPLACED THE FLOORBEAM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 75) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK AT FRAME 75 AND -Y450. REPLACED THE SEAT TRACK IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: CROSSBEAM — CORRODED (FRAME 78) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON CROSSBEAM AT FRAME 78 AND Y380. REPAIRED THE CROSSBEAM IAW SRM 53-00-14-201 FIG 202.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT ANGLE BETWEEN FRAMES 75A AND 77 AT Y2462. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: CROSSBEAM — CORRODED (FRAME 78) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION FOUND ON CROSSBEAM AT FR 78 AND -Y1447. REPAIRED THE CROSSBEAM IAW SRM 53-00-14-201 FIG 202.

Part: SEAT TRACK — CORRODED (FRAMES 32-36) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK BETWEEN FRAMES 31 TO 37 AT Y1959. REPLACED THE SEAT TRACK IAW SRM 53-00-15 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 32-33) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION FOUND ON SEAT TRACK BETWEEN FRAME 32 AND 33 AT -Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-80) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 75 TO 80 AT -Y450. REPLACED THE FLOOR SUPPORT IAW SRM 51-00-15 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 32-36) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON THE MID CABIN SEAT TRACK BETWEEN FRAMES 32 AND 36 AT Y2462. REPLACED THE SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 32-34) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON FORWARD CABIN SEAT TRACK BETWEEN FRAMES 32 AND 34 AT -Y1959. REPLACED THE SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 39) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK BETWEEEN FRAMES 39 AND 39.2 AT -Y2462. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK AT FRAME 37 AND Y450. REPLACED THE SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 33-35) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION FOUND ON MID CABIN SEAT TRACK AT Y1456 BETWEEN FRAMES 33 AND 35. REPLACED THE SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 51-52) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK BETWEEN FRAMES 51 AND 52 AT Y450. REPLACED THE SEAT TRACK IAW SRM 53-31-15, SRM 51-42-11 AND SRM 51-44-11.

Part: CROSSBEAM — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON CROSSBEAM OUTBOARD SIDE OF SEAT TRACK AT Y450 AND FRAME 37. REPAIRED THE CROSSBEAM IAW SRM 53-00-14 AND SRM 51-42-11.

Part: SHIM — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SHIM BETWEEN FRAMES 73 AND 74 AT Y2462. REPLACED SHIM IAW SRM 53-41-14-001 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 74-80) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON FLOOR SUPPORT AT Y794.3 BETWEEN FRAMES 74 AND 80. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y794.3 AND FRAME 75. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 75 AND 78 AT -Y380. INSTALLED A NEW FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 33-37) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON MID CABIN SEAT TRACK AT Y1552.5 BETWEEN FRAMES 33 AND 37. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 37-39) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK BETWEEN FRAMES 37.4 AND 39 AT -Y450. REPLACED SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 13) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON CABIN FLOOR SUPPORT AT -Y720 AND FRAME 13A . REPLACED FLOOR SUPPORT IAW SRM 53-11-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FITTING — CORRODED (FRAME 16) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON CABIN FLOOR SUPPORT FITTING AT FRAME 16A AND -Y1380. REPLACED FLOOR SUPPORT FITTING IAW SRM 53-11-14, SRM 51-42-11 AND SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FRAMES 71-75) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK AT Y450 BETWEEN FRAMES 71 AND 75. REPLACED THE SEAT TRACK IAW SRM 51-42-11-001, SRM 53-41-14 AND SRM 51-44-11

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON SEAT TRACK BETWEEN FRAMES 37 AND 37.3 AT Y450. REPLACED SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y794.3 AND FRAME 73. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 78-79) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT Y0 BETWEEN FRAMES 78 AND 79. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON FLOOR SUPPORT AT -Y1447.8 AND FRAME 75A. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 74,752 hrs · 10,575 cycles

DELAMINATED MAIN DECK FLOOR PANEL 252BF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-201.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 74,752 hrs · 10,575 cycles

DELAMINATED MAIN DECK FLOOR PANEL 261AF BETWEEN FRAMES 51 - 55 ON LOWER SIDE. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-201.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 74,752 hrs · 10,575 cycles

DELAMINATED MAIN DECK FLOOR PANEL 261CF BETWEEN FRAMES 51 TO 55. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-201.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 74,752 hrs · 10,575 cycles

DELAMINATED MAIN DECK FLOOR PANEL 251AF. REPLACED FLOOR PANEL IAW SRM 53-02-00-201.

Part: FLOOR SUPPORT — CORRODED (FRAMES 77-78) · corrosion level 2 · airframe 74,751 hrs · 10,575 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y1137.1 BETWEEN FR 77 AND 78. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 73,867 hrs · 10,463 cycles

L3 DOOR EMERGENCY POWER SUPPLY (15WL) BATTERY FAILED FUNCTIONAL TEST ACCOMPLISHED PER A CHECK TASK CARD 33C20033002. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 73,860 hrs · 10,462 cycles

R2 DOOR EMERGENCY POWER SUPPLY (12WL) BATTERY FAILED FUNCTIONAL TEST ACCOMPLISHED PER A CHECK TASK CARD 33C20033002. REPLACED BATTERY IAW AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 73,867 hrs · 10,463 cycles

R4 DOOR EMERGENCY POWER SUPPLY (18WL) BATTERY FAILED FUNCTIONAL TEST ACCOMPLISHED PER A CHECK TASK CARD 33C20033002. REPLACED BATTERY IAW AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 73,461 hrs · 10,412 cycles

AIRCRAFT WAS NOT GNDED. 4R DOOR WOULD NOT ARM. REMOVED OBSTRUCTION FROM 4R DOOR GIRT BAR, DOORS ARMS PROPERLY.

Part: LENS — MISSING (EXIT SIGN) · airframe 73,242 hrs · 10,383 cycles

AIRCRAFT WAS NOT GNDED. 3L DOOR EMER EXIT SIGN LENS COVER IS MISSING. R & R EXIT SIGN.

Part: COVER — MISSING (CABIN) · airframe 73,242 hrs · 10,383 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT COVER AT L74 LAVATORY IS MISSING. REPLACED MISSING EMER LIGHT COVER.

Part: LENS — MISSING (CABIN) · airframe 72,512 hrs · 10,252 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT LENS MISSING MID GALLEY R2 DOOR. REPLACED R2 DOOR EMER LIGHT LENS.

Part: WIRE HARNESS — DAMAGED (CABIN)

AIRCRAFT WAS IN BASE MX. SEAT 19 AB EMER LIGHT HARNESS DAMAGED. R & R SEAT 19 AB EMER LIGHT HARNESS IAW FIGURE DWG FG23 & 3044. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-803-A. SYS CHECKED NORMAL.

Part: FITTING — DIRTY (L2 DOOR) · airframe 72,118 hrs · 10,165 cycles

AIRCRAFT WAS NOT GNDED. 2L DOOR WON'T ARM. REMOVED DEBRIS FROM GIRT BAR FLOOR MOUNT. 2L DOOR ARMS NORMALLY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,287 hrs · 9,758 cycles

PILOT FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY IN THE PILOT'S FLASHLIGHT.

Part: GIRT BAR — DAMAGED (L4 DOOR SLIDE) · airframe 68,941 hrs · 9,710 cycles

SLIDE CONTROL UNIT, 21DH, F HEAT G AFT INDICATOR LIGHT DOES NOT ILLUMINATE WHEN TESTED. R & R L4 GIRT BAR FITTING, 25DH.

Part: GIRT BAR — NO TEST (DOOR SLIDE) · airframe 68,941 hrs · 9,710 cycles

SLIDE CONTROL UNIT, 22DH, F HEAT G AFT INDICATOR LIGHT DOES NOT ILLUMINATE WHEN TESTED. R & R SLIDE FITTING, 26DH.

Part: EPSU — INOPERATIVE (CABIN) · airframe 68,821 hrs · 9,686 cycles

1R EMER LIGHT BATTERY FAULT, ESPU. R & R 1R ESPU.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,240 hrs · 9,578 cycles

CO-PILOT EMER FLASHLIGHT BATTERY POWER INOPERATIVE. REPLACED THE CO-PILOT'S EMER FLASHLIGHT BATTERY.

Part: BALLAST — DETERIORATED (CABIN) · airframe 67,894 hrs · 9,519 cycles

EN-ROUTE SMOKE OBSERVED FOR 10 SEC, AFT GALLEY A/C LT MIDWAY IN GALLEY OVER TOP OF LAST REMOVABLE BIN. COULD NOT DUPLICATE THE PROBLEM, HOWEVER, AN AFT WORK LIGHT BALLAST CONDITION WAS FOUND DETERIORATED. THE BALLAST WAS REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,292 hrs · 9,420 cycles

EMERGENCY LIGHT BATTERY R3 16WC FAILED BITE TEST. R & R THE EMER LIGHT BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,527 hrs · 9,316 cycles

EMERGENCY FLASHLIGHT 2L JS IS INOPERATIVE. R & R 2L DOOR EMER FLASHLIGHT BATTERY & STRAP. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 65,353 hrs · 9,165 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK JOB CARD 33C20033002. REPLACED THE EMER POWER SUPPLY UNIT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 65,353 hrs · 9,165 cycles

CABIN EMER LIGHTING BATTERY CHECK. REPLACED THE EMER POWER SUPPLY UNIT.

Part: LENS — MISSING (CABIN) · airframe 64,261 hrs · 9,027 cycles

EMERGENCY LIGHT LENS COVER MISSING AT L54. INSTALLED EMERGENCY LIGHT COVER AT L54 LAVATORY.

Part: PIN — CORRODED (LT MLG) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK CORROSION ON LT LANDING GEAR BOGIE PIVOT PIN AT RIB 5. REPLACED IAW A330 MM 32-11-14-400-801A & EO 32O9U046.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK, CRACK ON FLOOR PANEL 151AF BETWEEN FRAME 53.5 TO FRAME 53.7, Y 470. REPLACED FLOOR PANEL 151AF IAW SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 151HF BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 140 TO Y 805. REPLACED FLOOR PANEL 151HF IAW SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK, CRACK ON FLOOR PANEL 151VF AT FRAME 57.1, Y 1140. REPLACED FLOOR PANEL 151VF IAW SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 162EF BETWEEN FRAME 69 TO FRAME 72 & BETWEEN Y 0 TO -Y 900. REPLACED FLOOR PANEL 162EF IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 151EF BETWEEN FRAME 54 TO FRAME 57.1 & BETWEEN Y 140 TO Y 805. REPLACED FLOOR PANEL 151EF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251GG BETWEEN FRAME 47 TO FRAME 52 & BETWEEN Y 450 TO -Y 450. REPLACED FLOOR PANEL 251GG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2CHECK DELAMINATION ON FLOOR PANEL 252XF BETWEEN FRAME 40 TO FRAME 42.2 & BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 252XF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251GF BETWEEN FRAME 37.4 TO FRAME 39 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251GF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251QF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 251QF IAW A330 SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252HG BETWEEN FRAME 47 TO FRAME 50 & BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 252HG IAW A330 SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252MF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 252MF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252SF BETWEEN FRAME 39.2 TO FRAME 40 & BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 252SF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252RG BETWEEN FRAME 52 TO FRAME 53.2 & BETWEEN -Y 1456 TO -Y 1959. REPLACED FLOOR PANEL 252RG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251AG BETWEEN FRAME 40 TO FRAME 42 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 251AG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251HG BETWEEN FRAME 47 TO FRAME 51 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251HG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251RG BETWEEN FRAME 51 TO FRAME 53.2 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 251RG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251PF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 251PF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251SG BETWEEN FRAME 52 TO FRAME 53.2 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 251SG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262UG BETWEEN FRAME 65 TO FRAME 69 & BETWEEN -Y 1959 TO -Y 2462. REPLACED FLOOR PANEL 262UG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 252CF BETWEEN FRAME 37 TO FRAME 37.4 & BETWEEN -Y 953 TO -Y 1456. REPLACED FLOOR PANEL 252CF IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251BG BETWEEN FRAME 45 TO FRAME 47 & BETWEEN Y 450 TO -Y 450. REPLACED FLOOR PANEL 251BG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261QG BETWEEN FRAME 62 TO FRAME 65 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 261QG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251QG BETWEEN FRAME 52 TO FRAME 53.2 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 251QG IAW SRM 53-02-00, PARA 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262WF BETWEEN FRAME 57.1 TO FRAME 58 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 262WF IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232CH BETWEEN FRAME 55 TO FRAME 57.1 BETWEEN -Y953 TO -Y1959. REPLACED FLOOR PANEL 232CH IAW A330 SRM 53-02-00, PARA 5I, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261ZG BETWEEN FRAME 69 TO FRAME 71 BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 261ZG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261WF BETWEEN FRAME 57.1 TO FRAME 58 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261WF IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262YG BETWEEN FRAME 69 TO FRAME 71 BETWEEN -Y953 TO -Y1959. REPLACED FLOOR PANEL 262YG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261CH BETWEEN FRAME 55 TO FRAME 57.1 BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261CH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261RF BETWEEN FRAME 55 TO FRAME 57.1 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261RF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261LG BETWEEN FRAME 62 TO FRAME 65 BETWEEN Y 450 TO -Y 450. REPLACED FLOOR PANEL 261LG IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262JH BETWEEN FRAME 53.7 TO FRAME 53.9 BETWEEN -Y 1456 TO -Y 1959. REPLACED FLOOR PANEL 262JH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261UG BETWEEN FRAME 65 TO FRAME 69 BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 261UG IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261TG BETWEEN FRAME 65 TO FRAME 69 BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261TG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261MG BETWEEN FRAME 62 TO FRAME 65 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261MG IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261LF BETWEEN FRAME 53.9 TO FRAME 55 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261LF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261HF BETWEEN FRAME 53.7 TO FRAME 53.9 BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261HF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262XG BETWEEN FRAME 69 TO FRAME 71 BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 262XG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262TG BETWEEN FRAME 65 TO FRAME 69 BETWEEN -Y953 TO -Y1959. REPLACED FLOOR PANEL 262TG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261JF BETWEEN FRAME 53.7 TO FRAME 53.9 BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 261JF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262FH BETWEEN FRAME 62 TO FRAME 65 BETWEEN -Y953 TO -Y1959. REPLACED FLOOR PANEL 262FH IAW A330 SRM 53-02-02, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261KH BETWEEN FRAME 53.7 TO FRAME 53.9 BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 261KH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261BG BETWEEN FRAME 58 TO FRAME 60 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 261BG IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262LF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 262LF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261FH BETWEEN FRAME 62 TO FRAME 65 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261FH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261QF BETWEEN FRAME 55 TO FRAME 57.1 & BETWEEN -Y 450 TO Y 450. REPLACED FLOOR PANEL 261QF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262DH BETWEEN FRAME 58 TO FRAME 60 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 262DH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261VF BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261VF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262MF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 262MF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261MF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 261MF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262EH BETWEEN FRAME 60 TO FRAME 62 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 262EH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261XG BETWEEN FRAME 69 TO FRAME 71 & BETWEEN Y 953 TO Y 450. REPLACED FLOOR PANEL 261XG IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262ZF BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 2462 TO Y 1959. REPLACED FLOOR PANEL 262ZF IAW SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261LH BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 1959 TO Y 953. REPLACED FLOOR PANEL 261LH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261YG BETWEEN FRAME 69 TO FRAME 71 & BETWEEN Y 1959 TO Y 953. REPLACED FLOOR PANEL 261YG IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262JF BETWEEN FRAME 53.7 TO FRAME 53.9 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 262JF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261EH BETWEEN FRAME 60 TO FRAME 62 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261EH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261JH BETWEEN FRAME 53.7 TO FRAME 53.9 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 261JH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262LH BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 1959 TO Y 953. REPLACED FLOOR PANEL 262LH IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262SG BETWEEN FR 65 TO FR 67 & BETWEEN -Y 450 TO -Y 953. REPLACED FLOOR PANEL 262SG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 262NF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 262NF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261NF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 261NF IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 261FG BETWEEN FRAME 60 TO FRAME 62 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261FG IAW SRM 53-02-00 FIG 211 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232HF BETWEEN FRAME 19 TO FRAME 22 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 232HF IAW SRM 53-02-00, PARA 5L, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231HF BETWEEN FRAME 19 TO FRAME 22 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 231HF IAW SRM 53-02-00, PARA 5L, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231LF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 231LF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232MF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 232MF IAW SRM 53-02-00, PARA 5L, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231PF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 2462 TO Y 1959. REPLACED FLOOR PANEL 231PF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232XF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 232XF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232LF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 232LF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231MF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 231MF IAW SRM 53-02-00, PARA 5L, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231FF BETWEEN FRAME 19 TO FRAME 22 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 231FF IAW SRM 53-02-00, PARA 5L, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231YF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 1959 TO Y 1456. REPLACED FLOOR PANEL 231YF IAW SRM 53-02-00, PARA 5L FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 231VF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 231VF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,993 hrs · 8,982 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 232ZF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 232ZF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 63,463 hrs · 8,904 cycles

EMERGENCY LIGHTS AT 2L DOOR, 2L OVERHEAD, SEATS 3, 5, 6, 8, 19, 24 & 13. FOUND CONNECTOR DISCONNECTED AT BATTERY PACK OVER 2L DOOR. RECONNECTED CONNECTOR, OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,218 hrs · 8,869 cycles

DURING CABIN CREW CHECK, FOUND L1 DOOR JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN FLASHLIGHT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,171 hrs · 8,863 cycles

RT SIDE AISLE AT R3 DOOR AFT FACING EMERGENCY EXIT LIGHT LENS BROKEN, UNABLE TO SECURE IN FIXTURE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT COVER. CHECKED OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,377 hrs · 8,759 cycles

F/A EMERGENCY FLASHLIGHT INOPERATIVE, L-1 DOOR FORWARD OTBD. MX R & R THE FLASHLIGHT BATTERY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 61,948 hrs · 8,703 cycles

WHILE PERFORMING OPS CHECK, EMERGENCY LIGHTS FAULT OCCURED, MX R & R BATTERY. EPSU BITE TEST CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,067 hrs · 8,315 cycles

OPERATIONAL CHECK EMERGENCY LIGHTS VIA MCDU REPORTS FAULT: ATA 335100 EXIT SIGNS/ EPSU 1L (11WL). MAINTENANCE REMOVED AND REPLACED EPSU 1L (11WL) BATTERY AND OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,067 hrs · 8,315 cycles

OPERATIONAL CHECK EMERGENCY LIGHTS VIA MCDU. REPORTS FAULT: ATA 335100 BAT/ EPSU 4R (18WL). MAINTENANCE REMOVED AND REPLACED EPSU 4R (18WL) BATTERY AND OPS CHECKED GOOD.

Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 59,067 hrs · 8,315 cycles

OPS CHECK EMERGENCY LIGHTS VIA MCDU REPORTS FAULT: ATA 335100 EXIT SIGNS/ EPSU 3R (16WL). MAINTENANCE RESET EPSU 3R (16WL) BATTERY AND OPS CHECKED GOOD.

Part: SIGN — MISSING (CABIN) · airframe 57,749 hrs · 8,137 cycles

RIGHT LAV L74 RED EXIT SIGN MISSING. MAINTENANCE REPLACED SIGN AT LAV L74.

Part: OVEN — FAULTY (GALLEY) · airframe 57,686 hrs · 8,129 cycles

FLIGHT ATTENDANT REPORTED BURNING SMELL COMING FROM OVEN 2 POSITION 4-3. IT WAS A PLASTIC SMELL AND CONFIRMED IT WAS NOT COMING FROM INSIDE THE OVEN BUT MAYBE BEHIND IT. ALL C/B'S WERE PULLED AND THE ODOR STOPPED. MAINTENANCE REMOVED AND REPLACED OVEN NR 2 POS 4-3.

Part: DOOR LATCH — OUT OF POSITION (EMERGENCY EXIT) · airframe 57,386 hrs · 8,091 cycles

THE 3R EMERGENCY EXIT SHOWS OPEN ON ECAM, THE DOOR IS CLOSED AND ARMED. MAINTENANCE FOUND UPPER LATCH OUT OF POSITION, REPOSITIONED LATCH 3R DOOR CHECKS GOOD.

Part: COVER — MISSING (EXIT SIGN) · airframe 57,351 hrs · 8,087 cycles

EXIT SIGN ABOVE 26E COVER CAME OFF (3R DOOR). MAINTENANCE INSTALLED NEW EXIT SIGN COVER, NOW OKAY.

Part: COVER — MISSING (CABIN) · airframe 57,191 hrs · 8,066 cycles

EMERGENCY LIGHT COVER AT SEAT 25D MISSING. MAINTENANCE LOCATED LIGHT COVER AND RE-FITTED AT SEAT 25D.

Part: BRACKET — BROKEN (EXIT SIGN) · airframe 56,499 hrs · 7,977 cycles

THE 2L OVERHEAD EMERGENCY EXIT SIGN BRACKET BROKEN. MAINTENANCE REPLACED CEILING EMERGENCY EXIT LIGHT FRAME AT L2 DOOR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - DELAMINATION ON FLOOR PANEL 131NF BETWEEN FR26.3 TO FR30 & BETWEEN Y140 TO Y805. REPLACED FLOOR PANEL 131NF IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - DELAMINATION ON FLOOR PANEL 252DF BETWEEN FR37 TO FR37.4 & BETWEEN -Y1456 TO -Y1959. REPLACED FLOOR PANEL 252DF IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - DELAMINATION ON FLOOR PANEL 251ZF BETWEEN FR40 TO FR42 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 251ZF IAW A330 SRM 53-02-00 FIG 211.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 8 APPROX 3 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR SKIN UPPER SURFACE EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR SKIN UPPER SURFACE BETWEEN ELEVATOR RIB 9 & RIB 10 APPROX 4.875 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR SKIN UPPER SURFACE EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR UPPER SKIN AT ER10 APPROX 9 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 9 APPROX 4.0625 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR SKIN UPPER SURFACE EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,851 hrs · 7,765 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 2 APPROX 4.25 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE EO 5511U056.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 54,403 hrs · 7,707 cycles

SCHEDULED PARTS CHANGE FOR P/N 33-2561-9-0009S/N 1676 SLIDE, RAFT L1/R1&L4/R4 POSITION L1 LEFT 1 NHA POSITION L1 LEFT 1. MAINTENANCE REPL'D L1 DOOR EVAC SLIDE PER J/C 33L20025001. SLIDE WOULD NOT DEPLOY. CONNECTOR FOR LIGHTS STAYED CONNECTED TO AC AND SLIDE, DID NOT INFLATE MANUALLY EITHER.

Part: SLIDE RAFT — PUNCTURED (L4 DOOR)

PHL - JOB CARD 33L20025001 DUE - L4 SLIDE/RAFT OPERATIONAL CHECK. MAINTENANCE JOB CARD 33L20025001 ACCOMPLISHED ON L4 SLIDE/RAFT. OPERATIONAL CHECK FAILED DUE TO PUNCTURE IN SLIDE/RAFT ASSY.

Part: OVEN — OVERHEATED (GALLEY) · airframe 53,129 hrs · 7,536 cycles

FLIGHT 743, BCN-PHL - THE MID GALLEY OVEN NR 2 4-3 OVERHEATED AND BEGAN SMOKING GALLEY POWER WAS TURNED OFF. MAINTENANCE REMOVED AND REPLACED MID GALLEY NR 2 OVEN PER REF 25-30-00 OPERATIONAL CHECK IS SATISFACTORY.

Part: LENS — MISSING (CABNI) · airframe 52,909 hrs · 7,507 cycles

FCO - SEAT 11G EMERGENCY LIGHT LENS MISSING. MAINTENANCE 11G EMERGENCY LIGHT LENS REPLACED LIGHT OPERATIONAL NORMAL. M,E 26-3351-3-0019. P/N 25-1435-3. AMM 33-51-12.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 52,799 hrs · 7,494 cycles

PHL - EMERGENCY ESCAPE PATH LIGHT, DISPLACED FROM SEAT AT 11G. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT 11G. CHECKS GOOD, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,725 hrs · 7,485 cycles

PHL - DURING CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK BATTERY AT R-3 DOOR FAILED. REMOVED AND REPLACED BATTERY, OPERATIONAL CHECK IS GOOD IAW 33-51-00.

Part: COVER — MISSING (CABIN) · airframe 52,410 hrs · 7,445 cycles

CLT - EMERGENCY LIGHT COVER MISSING ON WALL OF AIRCRAFT RIGHT BY LAVATORY 74. MAINTENANCE REPLACED MISSING EMERGENCY LIGHT COVER AT RT LAV 74, OK FOR SERVICE.

Part: DOOR — STUCK (L4)

MAD - PRIOR TO DEPARTURE, CREW UNABLE TO CLOSE DL4. DL4 FOUND STUCK, PREVENTING EITHER OPENING/CLOSING. RELEASED DL4 FROM FORWARD MID ROLLER. INSPECTED DOOR AND FRAME AND FOUND NO DAMAGE AND GOOD CONDITION. CYCLED DL4 DOOR SEVERAL TIMES AND OPERATION NORMAL.

Part: ROLLER — DEFECTIVE (L4 DOOR)

PHL - L4 DOOR HARD TO CLOSE (APPEAR A ROLLER MID WAY UP THE DOOR IS NOT WORKING PROPERLY). ACCOMPLISHED ADJUSTMENT AND TEST ON L4 DOOR. DOOR OPERATES NORMALLY. OK FOR SERVICE.

Part: SLIDE RAFT — DEFECTIVE (L2 DOOR)

PHL - L2 SLIDE PRESSURE INDICATED ON THE FLIGHT ATTENDANT PANEL. FOUND A BAD SLIDE DISARMING MECHANISM WHERE THE SLIDE SAFETY PIN IS INSERTED. THE "C" CLIP WAS MISSING AND A SPRING WAS COMING OUT OF THE END. MAINTENANCE REMOVED AND REPLACED THE L2 SLIDE.

Part: WIRE — BROKEN (CABIN)

LGW - SEAT ROW 19AB EMERGENCY LIGHT UNIT ADRIFT FROM SEAT AND WIRE BROKEN. MAINTENANCE REMADE WIRE CONNECTION, AND REFITTED THE EMERGENCY LIGHT ASSEMBLY.

Part: FASTENER — LOOSE (CENTER WING) · airframe 50,745 hrs · 7,230 cycles

PHL - 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 102857A & 102881A.

Part: EPSU — FAULTY (CABIN) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - EEL - EMERGENCY POWER SUPPLY UNIT (EPSU) 11W ON L-1 DOOR AREA SHOWS BATTERY FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 11W ON L-1 DOOR AREA IAW B737 AMM 33-51-38-000-802.

Part: RIB — CRACKED (RT WING)

BFM - S2 - MAJOR REPAIR - CRACK ON RIGHT WING RIB 6 AFT FUEL PIPE APPERTURE CUTOUT AFT UPPER ATTACHMENT HOLE. REPAIRED IAW EA 134359.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON L4 DOOR CUTOUT LOWER SILL AT FR 74 - FR 75. REPLACED L4 DOOR CUTOUT LOWER SILL AT FR 74 - FR 75 IAW A330 SRM 51-74-00.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON R4 DOOR CUTOUT LOWER SILL AT FR 73 - FR 74, -Y2462. REPLACED R4 DOOR CUTOUT LOWER SILL AT FR 73 - FR 74, -Y2462 IAW A330 SRM 51-74-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR PANEL 271KF. REPLACED FLOOR PANEL 271KF IAW A330 SRM 51-75-12.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 53,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR PANEL 222GF. REPLACED FLOOR PANEL 222GF IAW A330 SRM 51-75-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR72 TO FR73, -Y1959. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR72 TO FR73, -Y1959 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN FLOOR PANEL 221GF UPPER SURFACE. REPLACED CABIN FLOOR PANEL 221GF UPPER SURFACE IAW TRM 330-5302-11-0330.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM FORWARD OF FR13A, Y1959. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR12A TO FR18, Y1959 IAW A330 SRM 53-11-14 & 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S4 CHECK - LEVEL 2 CORROSION ON BEAM AT FR 73, -Y1147. REPLACED BEAM AT FR 73, -Y1147 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC & INTERGRANULAR CORROSION ON CABIN FLOOR LONGITUDINAL BEAM (SEAT TRACK) AFT OF FR73, Y2462. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM AFT OF FR73, Y2462 IAW A330 SRM 53-41-14 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR64 AND FR65, BL -Y2462. REPLACED SEAT TRACK BETWEEN FR64 AND FR65, BL -Y2462 IAW A330 SRM 51-42-11, 53-00-15, 51-74-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR75 TO FR80, -Y450. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR75 TO FR80, -Y450.1 IAW A330 SRM 53-41-14 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR57.2 TO FR57.3, BL -Y1959. REPLACED SEAT TRACK BETWEEN FR57.2 TO FR57.3, BL -Y1959 IAW A330 SRM 53-00-15 FIG 101, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR57.3, BL Y2462. REPLACED SEAT TRACK AT FR57.3, BL Y2462 IAW A330 SRM 53-00-15, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR 73, +Y1478. REPLACED SEAT TRACK AT FR 73, +Y1478 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR73, -Y2462. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR73, -Y2462 IAW A330 SRM 53-41-14 & 51-72-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR61 TO FR62, BL Y450. REPLACED SEAT TRACK BETWEEN FR61 TO FR62, BL Y450 IAW A330 SRM 51-42-11, 51-72-00, 53-00-15 FIG 101 & 204.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,315 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 55- FR 57.3, -Y450. REPLACED SEAT TRACK AT FR 55- FR 57.3, -Y450 IAW A330 SRM 53-10-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR58 TO FR68, BL -Y450. REPLACED SEAT TRACK BETWEEN FR58 TO FR68, BL -Y450 IAW A330 SRM 51-42-11, 51-74-00, 51-44-11, 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR53.8 TO FR53.9, BL Y1456. REPLACED SEAT TRACK BETWEEN FR53.8 TO FR53.9, BL Y1456 IAW A330 SRM 53-31-15 FIG 201, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR58 TO FR60, BL -Y1959. REPLACED SEAT TRACK BETWEEN FR58 TO FR60, BL -Y1959 IAW A330 SRM 53-00-15 FIG 102, 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGITUDINAL BEAM BETWEEN FR74 TO FR78, Y1137.1. REPLACED LONGITUDINAL BEAM FROM FR74 TO FR80, Y1137.1 IAW A330 SRM 53-41-14 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 62-FR63, +Y2462. REPLACED SEAT TRACK AT FR 62-FR63, +Y2462 IAW A330 SRM 53-00-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR71 TO FR75, BL Y450. REPLACED SEAT TRACK BETWEEN FR71 TO FR75, BL Y450 IAW A330 SRM 53-00-15 FIG 101, 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 71-FR72, -Y450. REPLACED SEAT TRACK AT FR 71-FR72, -Y450.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR53.4 T0 FR53.6, BL Y1552.5. REPLACED SEAT TRACK BETWEEN FR53.4 T0 FR53.6, BL Y1552.5 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR74 TO FR76, Y=0. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR74 TO FR76, Y=0 IAW A330 SRM 53-41-14 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR73, -Y794. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR73, -Y794 IAW A330 SRM 53-41-14, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR52 TO FR53, BL Y450. REPLACED SEAT TRACK BETWEEN FR52 TO FR53, BL Y450 IAW A330 SRM 51-42-11, 51-72-11, 53-31-15 FIG 101.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGITUDINAL BEAM AT FR78, Y=0. REPLACED LONGITUDINAL BEAM FROM FR77 TO FR78, Y=0 IAW A330 SRM 53-41-14 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR74 TO FR76, -Y794.3. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR74 TO FR80, Y1137.1 IAW A330 SRM 53-41-14 & 51-72-11.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON LEFT AC PACK OUTLET DOOR SURROUND FRAME AT FR 44-FR45. REPAIRED LEFT AC PACK OUTLET DOOR SURROUND FRAME AT FR 44-FR45 IAW A330 SRM 51-74-00 AND SRM 53-35-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR80, -Y794.3. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR80, -Y794.3 IAW A330 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR LONGITUDINAL BEAM (SEAT TRACK) AT FR78, -Y1447.8. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR78, -Y1447.8 IAW A330 SRM 53-41-14, 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR75 TO FR76, Y1447.8. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR75 TO FR76, Y1447.8 IAW A330 SRM 53-41-14 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR30, BL Y450. REPLACED SEAT TRACK AT FR30, BL Y450 IAW A330 SRM 53-00-15 FIG 102 AND 204, 53-21-15 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR75 TO FR76, -Y1447.8. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR75 TO FR76, -Y1447.8 IAW A330 SRM 53-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,305 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN LONGITUDINAL FLOORBEAM AT FR16A, -Y1456. REPLACED LONGITUDINAL FLOORBEAM AT FR16A, -Y1456 IAW A330 SRM 51-42-11, 51-72-11 & 53-11-14.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON ATTACH ANGLE SUPPORT AT FR76, -Y1447.8. REPLACED ATTACH ANGLE SUPPORT AT FR76 -Y1447.8 IAW A330 SRM 53-41-14, 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR75, Y450. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR75, Y450 IAW A330 SRM 51-42-11, 51-72-11, 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR74 TO FR76, -Y11371. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR74 TO FR76, -Y11371 IAW A330 SRM 53-41-14, 51-42-11 & 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN LONGITUDINAL FLOORBEAM AT FR73, Y794.3. REPLACED LONGITUDINAL FLOORBEAM AT FR73, Y794.3 IAW A330 SRM 51-72-11 & 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR54 TO FR55, -Y450. REPLACED SEAT TRACK BETWEEN FR54 TO FR55, -Y450 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y1447. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y1447 IAW A330 SRM 53-00-15, 51-42-11 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - FLOOR PANEL 271QF IS DELAMINATED & HAS CORROSION ON INSERTS BETWEEN FR78 TO FR80 & BETWEEN Y450 TO Y1447. REPAIRED CABIN FLOOR PANEL 271QF IAW A330 SRM 53-42-12 & 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR72 TO FR73, -Y450. REPLACED SEAT TRACK BETWEEN FR72 TO FR73, -Y450 IAW A330 SRM 51-72-11 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - FLOOR PANEL 271NF IS DELAMINATED & HAS CORROSION ON INSERTS BETWEEN FR76 TO FR78 & BETWEEN Y450 TO Y1447. REPAIRED CABIN FLOOR PANEL 271NF IAW A330 SRM 53-42-12 & 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, -Y1137. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y1137 IAW A330 SRM 53-00-15, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.6, Y1959. REPLACED SEAT TRACK BETWEEN FR53.4 TO FR53.6, Y1959 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR53.9 TO FR54, -Y450. REPLACED SEAT TRACK BETWEEN FR53.9 TO FR54, -Y450 IAW A330 SRM 53-31-15.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CABIN FLOOR PANEL 272QF IS DELAMINATED BETWEEN FR78 TO FR80 & BETWEEN -Y450 TO -Y1447. REPAIRED CABIN FLOOR PANEL 272QF IAW A330 SRM 53-42-12 & 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR57.4 TO FR58, Y1959. REPLACED SEAT TRACK BETWEEN FR57.4 TO FR58, Y1959 IAW A330 SRM A330 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN LONGITUDINAL FLOORBEAM AT FR78, -Y1447.8. REPLACED LONGITUDINAL FLOORBEAM AT FR78, -Y1447.8 IAW A330 SRM 53-41-14 & 51-42-11.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON GALLEY MOUNT SUPPORT BEAM AT FR16A, BL -Y1938. REPLACED GALLEY MOUNT SUPPORT BEAM AT FR16A, BL -Y1938 IAW A330 SRM 53-11-14, 51-42-11, 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR53.3 T0 FR53.6, BL Y2055.5. REPLACED SEAT TRACK BETWEEN FR53.3 T0 FR53.6, BL Y2055.5 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR55 TO FR56, -Y1959. REPLACED SEAT TRACK BETWEEN FR55 TO FR56, -Y1959 IAW A330 SRM 53-00-15 & 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CABIN SEAT TRACK AT FR17, Y450. REPLACED CABIN SEAT TRACK AT FR17, Y450 IAW A330 SRM 51-73-00, 53-11-15, 51-74-00, 51-42-11 & 51-44-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR57.1, Y450. REPLACED SEAT TRACK AT FR57.1, Y450 IAW A330 SRM 53-00-15, 51-70-00, 51-42-11 & 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR73, -Y953. REPLACED LONGITUDINAL FLOORBEAM AT FR73, -Y953 IAW A330 SRM 51-42-11, 51-21-11 & 53-41-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR31 TO FR36, -Y450. REPLACED SEAT TRACK BETWEEN FR31 TO FR36, -Y450 IAW A330 SRM 53-00-15, 51-74-11, 51-44-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, -Y1447. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y1447 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR73, Y1670. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR73, Y1670 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR35 TO FR36, Y1516.5. REPLACED SEAT TRACK BETWEEN FR35 TO FR36, Y1516.5 IAW A330 SRM 53-00-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR31 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR31 TO FR37, Y450 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR16A, -Y1959. REPLACED LONGITUDINAL FLOORBEAM AT FR16A, -Y1959 IAW A330 SRM 51-74-03, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR46, -Y450. REPLACED SEAT TRACK AT FR46, -Y450 IAW A330 SRM 53-31-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR33, Y=0. REPLACED LONGITUDINAL FLOORBEAM AT FR33, Y=0 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR75 TO FR78, -Y400. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, -Y400 IAW A330 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN Y1910 TO Y2462.6. REPLACED CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN Y1910 TO Y2462.6 IAW A330 SRM 51-42-11 & 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y1137. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y1137 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN -Y1910 TO -Y2462.5. REPLACED CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN -Y1910 TO -Y2462.5 IAW A330 SRM 51-42-11 & 53-41-14.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - CRACK ON SUPPORT BETWEEN FR26 TO FR25, S25L. REPLACED SUPPORT BETWEEN FR26 TO FR25, S25L IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR16A, -Y953. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR16A, -Y953 IAW A330 SRM 53-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR78, -Y1137.1. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR78, -Y1137.1 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,365 hrs · 7,171 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y400. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y400 IAW A330 SRM 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAN - ON DAILY CHECK, THE FLASHLIGHT AT THE OUTBOARD JUMP SEAT, DOOR R4, WAS INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FLASHLIGHT BATTERY WAS DISCHARGED AT FORWARD FACE OF DOOR L1 FLIGHT ATTENDANT SEAT. REPLACED BATTERY OF FLASHLIGHT AT FORWARD FACE OF DOOR L1 FLIGHT ATTENDANT SEAT.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS FAILED THE OPS CHECK VIA MCDU. REMOVED AND REPLACED THE BATTERIES FROM EPSU AT DOOR L3.

Part: FUSE — FAULTY (POWER SUPPLY)

THE EMERGENCY LIGHTS FAILED THE OPS CHECK VIA MCDU. REMOVED AND REPLACED EPSU (15WL). REMOVED AND RE-SOLDERED WEAK CONNECTIONS UNDERNEATH CONVERTER U12, RE-INSTALLED U12, REPLACED LISTED PART(S) (FUSE 4A 250 TR5T19372-4A, MPN 779-435-73). UNIT ASSEMBLED, CLEANED AND PASSED FUNCTIONAL TEST.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS FAILED THE OPS CHECK VIA MCDU. REMOVED AND REPLACED THE BATTERIES AT DOOR L4.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS FAILED THE OPS CHECK VIA MCDU. REMOVED AND REPLACED THE BATTERIES FROM EPSU AT DOOR R4.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS FAILED THE OPS CHECK VIA MCDU. REMOVED AND REPLACED THE BATTERIES FROM THE EPSU AT DOOR R2.

Part: LINKAGE — OUT OF POSITION (ENTRY DOOR)

FCO - THE NUMBER FOUR, LEFT MAIN ENTRY DOOR WAS FOUND JAMMED AT AIRCRAFT DEPARTURE. FOUND THE FORWARD GUIDE ROLLER / (INNER HANDLE INTERLOCK) ON OPPOSITE SIDE OF DOOR FIXED BRACKET. INNER DOOR HANDLE LINKAGE DISCONNECTED TO RELEASE DOOR. LINKAGE RECONNECTED AND DOOR OPEN, CLOSE, AUTO MANUAL CHECKS OUT NUMEROUS TIMES WITH CORRECT FUNCTION.

Part: COMPRESSOR — OVERHEATED (CABIN SEAT)

SEAT 5A/B ELECTRICAL WIRE (SMOKE) ODOR. FOUND LUMBAR COMPRESSOR OVERHEATED. REMOVED COMPRESSOR ASSEMBLY FROM SEAT. REPLACED SEAT LUMBAR ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

MAD - FOUND CAPTAIN'S FLASHLIGHT LED NOT FLASHING. REMOVED AND REPLACED CAPTAIN'S FLASHLIGHT BATTERY PACK.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EES - NEED TO SERVICE DOOR L-2 ASSIST BOTTLE. SERVICED L-2 DOOR ASSIST BOTTLE IAW A330 AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EES - NEED TO SERVICE DOOR R-1 ASSIST BOTTLE. SERVICED R-1 DOOR ASSIST BOTTLE IAW A330 AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EES - NEED TO SERVICE DOOR R-2 ASSIST BOTTLE. SERVICED R-2 DOOR ASSIST BOTTLE IAW A330 AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EES - NEED TO SERVICE DOOR L-1 ASSIST BOTTLE. SERVICED L-1 DOOR ASSIST BOTTLE IAW A330 AMM 52-10-00.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EEL - CABIN IN SEAT EMERGENCY LIGHT ON SEAT 1GH, & 2AB INOP. REPAIRED CABIN IN SEAT EMERGENCY LIGHT ON SEAT 1GH, & 2AB IAW A330 ESPM 20-43-10.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 44,600 hrs · 6,402 cycles

BFM - C1 - EEL - CABIN IN SEAT EMERGENCY LIGHT ON SEAT 9GH, 22GH, 28GH & 33GH INOP. REPAIRED HARNESS CABLE & ELECTRIC ITEM IAW ESPM 20-53-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,600 hrs · 6,402 cycles

BFM - C-1 - MAJOR REPAIR - CORROSION ON T-CHORD FRAME AT FR44 BETWEEN RBL 50 TO LBL 50. REPLACED T-CHORD FRAME AT FR44 BETWEEN RBL 50 TO LBL 50 IAW A330 SRM 53-35-14, 51-44-11, 51-42-11.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE BATTERY FOR THE EPSU 1R FAILED CAPACITY TEST. MAINTENANCE REPLACED 1R ESPU BATTERY.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MAD - THE R2 DOOR FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT ASSEMBLY.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FCO - THE DOOR L3 FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: BATTERY — DISCHARGED (MEGAPHONE)

PHL - THE FORWARD MEGAPHONE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES OF THE FORWARD MEGAPHONE.

Part: TRIM PANEL — LOOSE (L1 DOOR)

MAN - THE L1 DOOR COULD NOT BE OPENED. MAINTENANCE FOUND THE L1 DOOR TRIM MOLDING LOOSE AND JAMMING THE ROLLER ARM TO THE WRONG SIDE OF THE DOOR APERTURE. THE STRIKER PLATE ROLLER WAS REPOSITIONED, AND THE DOOR TRIM MOLDING WAS REMOVED. THE DOOR WAS OPERATIONALLY CHECKED OK.

Part: OUTFLOW VALVE — DEFECTIVE (CABIN PRESSURE)

CDG FLT 755 EN ROUTE CDG TO PHL. AT FL 343, RECEIVED CABIN PRESSURE ADVISORY LIGHT. THE CABIN PRESSURE PAGE ON ECAM DISPLAYED. THE VENT EXTRACT VALVE INDICATED AMBER AND OPEN. THE CABIN PRESSURE REACHED 10,500 FEET. THE FLIGHT CREW PERFORMED A RAPID DESCENT TO 10,000 FEET AND REGAINED CONTROL OF CABIN PRESSURE. THE FLIGHT RETURNED TO FIELD CDG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE OVERBOARD EXTRACT VALVE ON MEL. MAINTENANCE LATER REPLACED THE OVERBOARD EXTRACT VALVE. OPERATIONALLY CHECKS OK.

Part: DOOR — OBSTRUCTED (L4)

SJU - DOOR 4L WOULD NOT OPEN. MAINTENANCE REMOVED OBSTRUCTION FROM TOP FORWARD DOOR FRAME. OPERATIONALLY CHECKS OK.

Part: DIAPHRAGM — LEAKING (L4 DOOR) · airframe 37,218 hrs · 5,408 cycles

BFM - EES - C2 CHECK - THE L4 DOOR ASSIST BOTTLE CANNOT BE SERVICED. REPLACED THE L4 DOOR DAMPER DIAPHRAGM AND SERVICED DAMPER IAW A330 AMM 52-10-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,218 hrs · 5,408 cycles

BFM - MAJOR REPAIR -C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5266 / FR 66, +Y953. REPAIRED CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5266 / FR 66, +Y953 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,218 hrs · 5,408 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5054 / FR 62 - BS 5584 / FR 72, +Y2462. REPAIRED CABIN SEAT TRACK, BS 5054 / FR 62 - BS 5584 / FR 72, +Y2462 IAW A330 SRM 53-00-15.

Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM)

PHL FRA-PHL FLT 701 - CREW REPORTED ON DESCENT ECAM MESSAGE STATING "HYD SYS G LEAKING". PRESSURE WAS REPORTED AT 2950 LBS, NO QUANTITY EVER GIVEN. NO EQUIPMENT WAS CALLED FOR LANDING. AFTER LANDING WHILE ON TAXIING TO THE GATE, THE AIRCRAFT HAD A COMPLETE HYDRAULIC FAILURE. THE AIRCRAFT WAS THEN TOWED FROM TAXIWAY TO GATE. MAINTENANCE FOUND LEFT ENGINE GREEN HYD PUMP PRESS LINE LEAKING. REMOVED AND REPLACED GREEN PUMP LINE.

Part: PUMP — FAILED (HHYDRAULIC SYS) · airframe 32,897 hrs · 4,807 cycles

FLIGHT 1071, PHL-SJU: DURING CRUISE, THE GREEN SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE GREEN SYSTEM HYDRAULIC PUMPS AND FILTERS.

Part: ADIRU — FAILED (NR 1) · airframe 32,518 hrs · 4,753 cycles

FLIGHT 1592, CLT-FRA: CREW RECEIVED ADIRU 1 FAULT. DIVERTED TO PHL. MAINTENANCE REPLACED ADIRU 1. NO FURTHER FAULTS.

Part: ELECTRONIC UNIT — ODOR (CABIN) · airframe 30,384 hrs · 4,451 cycles

FLIGHT 914, ODOR IN CABIN AROUND ROWS 12-15 LT. CREW SUSPECTED LT PACK OR ENTERTAINMENT SYSTEM. BOTH THE LT PACK AND ENTERTAINMENT SYSTEMS WERE SHUTDOWN, AND ODOR DISSIPATED. FLIGHT CONTINUED WITH NO FURTHER DIFFICULTIES. MAINTENANCE FOUND THE ROW 13CD SEU AT FAULT, AND USED THE BOX FROM ROW 35AB FOR ROW 13CD. NO FURTHER FAULTS.