N270AY

Part: CROSSBEAM — CRACKED (FRAME 74) · airframe 87,677 hrs · 12,933 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED AFT CABIN WET AREA CROSSBEAM FLANGE AT FR 74 AND YB. REPAIRED THE CROSSBEAM FLANGE IAW SRM 53-00-14-300-002, AND EA 301472.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 87,677 hrs · 12,933 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 73 AND FR 74 AT +YB. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 87,677 hrs · 12,933 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK FR 73 AND +YBI. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 87,677 hrs · 12,933 cycles

AIRCRFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 73 AND FR 74 AT YC1. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 87,039 hrs · 12,830 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SEAT 5A AND 6A INOPERATIVE. MAINTENANCE FOUND WIRE DISCONNECTED AND RECONNECTED PER AMM 33-51-00-710-801-A01.

Part: RADIO — OVERHEATED (NR 3) · airframe 86,202 hrs · 12,724 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS #3 RADIO BECAME VERY HOT-TURNED IT OFF (NO SMELL-TOO HOT TO TOUCH) TURNED INTEGRAL LIGHTING-OFF. MAINTENANCE REMOVED AND REPLACED #3 RADIO IAW AMM 23-12-00. OPS CHECKS NORMAL.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 85,425 hrs · 12,625 cycles

AIRCRAFT WAS GROUNDED: CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK FAILED. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PER AMM 33-51-39.

Part: FIRE — EXTINGUISHED (OVERHEAD BIN) · airframe 85,425 hrs · 12,625 cycles

AIRCRAFT NOT GROUNDED: CREW REPORTED A FIRE IN THE OVERHEAD BIN ABOVE SEATS 14AB. A PAX PUT THE FIRE OUT WITH A BLANKET. FIRE WAS CAUSED BY A VAPING DEVICE IN A PASSENGER BAG IN THE OVERHEAD BIN. NO FIRE EXTINGUISHER USED, CREW DID OPEN THE PBE KIT. CREW PUT THE DEVICE AFTER IN BATTERY CONTAINMENT BAG. DAMAGE TO THE OVERHEAD BIN ABOVE SEATS 14A/B. CREW DID NOT DECLARE AN EMERGENCY. AIRCRAFT WAS NOT OVERWEIGHT. NO INJURIES REPORTED. AIRCRAFT WAS NOT REMOVED FROM SERVICE.

Part: TRANSFER SYS — MALFUNCTIONED (FUEL) · airframe 85,312 hrs · 12,611 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ECAM WARNING FUEL -EXCESS AFT CG CAME ON CLIMB WE TRANSFERRED TV TANK FUEL FORWARD WITH MODE PUSH BOTTON IAW PROCEDURE. ECAM WARNING STOPPED AT 60 LBS FUEL LEFT IN TRIM TANK ECAM CAUTION FUEL T TANKXFR FAULT CAME ON. MAINTENANCE PLACED TRIM PIPE ISO VALVE ON TSI IAW TSM 28-27-00-810-816A. MAINTENANCE IS REPORTING THIS IS A ONE TIME EVENT AND NO 90 DAY HISTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,150 hrs · 12,591 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT EMERGENCY LIGHT AT ROW AT 3L DOOR INOPERATIVE. MAINTENANCE REPLACED LIGHT PER CMM 25-33-55.

Part: PRESSURE SWITCH — STICKING (L3 DOOR SLIDE) · airframe 84,744 hrs · 12,534 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND DOOR 3L CHECK SLIDE PRESSURE ON FAP. MAINTENANCE FOUND THE L3 DOOR PRESSURE SENSOR MICRO SWITCH STICKING. CLEANED SWITCH. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,744 hrs · 12,534 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND EPSU 1L (11WL) BAD DURING OPS CHECK OF EMERGENCY LIGHTING MCDU. REMOVED AND REPLACED EMERGENCY POWER UNIT IAW AMM 33-51-38. OPS CHECKS NORMAL.

Part: DIAPHRAGM — LEAKING (ASSIST BOTTLE) · airframe 84,415 hrs · 12,487 cycles

MAINTENANCE FOUND THE L3 DOOR SLIDE ASSIST BOTTLE HAD LOW PRESSURE, CIDS PANEL WARNING. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE DISCHARGE DIAPHRAGM ON THE ASSIST CYLINDER. CHARGED THE ASSIST CYLINDER. NO LEAKS NOTED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 84,374 hrs · 12,481 cycles

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

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 84,309 hrs · 12,471 cycles

L3 DOOR ASSIST BOTTLE PRESSURE WAS LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-12-14.

Part: VALVE — LEAKING (L3 ASSIST BOTTLE) · airframe 84,271 hrs · 12,466 cycles

THE PILOT REPORTED THE L3 DOOR ASSIST BOTTLE WAS IN YELLOW RANGE. THE AIRCRAFT WAS GROUNDED. FOUND A LEAK AT THE HIGH PRESSURE CHARGING VALVE IAW RD 52-10-00-2. REMOVED AND REPLACED THE CHARGING VALVE AND PACKING IAW AMM 52-10-00. LEAK CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 84,255 hrs · 12,464 cycles

THE L3 DOOR DAMPER BOTTLE PRESSURE WAS LOW. THE AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-10-00-600-802-A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 84,240 hrs · 12,461 cycles

L3 DOOR ASSIST BOTTLE PRESSURE WAS LOW. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-22-00-600-801-A, AND PERFORMED SATISFACTORY OPS CHECK.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 84,221 hrs · 12,457 cycles

CIDS MESSAGE FOR THE L3 DOOR PRESSURE. SERVICED L3 DOOR DAMPER BOTTLE AND EMERGENCY CYLINDER IAW AMM 52-22-00-600-801-A. CHECKED NORMAL. CIDS INDICATION NORMAL.

Part: TOILET — LEAKING (LAVATORY) · airframe 84,080 hrs · 12,436 cycles

ODOR IN THE LAVATORY, FOUND THE TOILET ASSEMBLY LEAKING. REPLACED TOILET ASSEMBLY IAW AMM 38-30-00. PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — NO TEST (R3 DOOR) · airframe 83,339 hrs · 12,311 cycles

R3 DOOR DAMPER, DID NOT PASS A TEST. REPLACED THE DOOR DAMPER IAW AMM 52-22-14-400-801-A.

Part: DAMPER — NO TEST (L3 DOOR) · airframe 83,339 hrs · 12,311 cycles

L3 DOOR DAMPER, DID NOT PASS A TEST. REPLACED THE DOOR DAMPER IAW AMM 52-22-14-400-801-A.

Part: SUPPORT ANGLE — CRACKED (RT NACELLE) · airframe 83,339 hrs · 12,311 cycles

CRACKED SUPPORT ANGLE, UPPER FORWARD, AT THE 12 O,CLOCK POSITION ON THE RT PYLON. REPAIRED THE SUPPORT ANGLE IAW SRM 51-72-11.

Part: PIVOT PIN — WORN (LT MLG) · airframe 83,339 hrs · 12,311 cycles

LEFT MAIN LANDING GEAR BOGIE BEAM PIVOT PIN CHROME PLATING WORN. REPLACED THE PIVOT PIN IAW TC 33T70032002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 83,339 hrs · 12,311 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 222JF BETWEEN FRAMES 14-17 IN FORWARD GALLEY AREA IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 PARA 2 FIGURE 20109.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 83,299 hrs · 12,304 cycles

EPSU BATTERY AT THE R4 DOOR FAILED EMERGENCY EXIT LIGHT CHECK. REPLACED THE BATTERY PACK. OPS TESTED GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 80,110 hrs · 11,907 cycles

R3 DOOR EXIT SIGN FOUND BROKEN. INSTALLED NEW EMERGENCY EXIT SIGN IAW AMM 33-50-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,040 hrs · 11,896 cycles

THE AIRCRAFT WAS NOT GROUNDED. INOPERATIVE EPSU-EMERGENCY POWER SUPPLY UNIT 16WL IN PASSENGER CABIN. (UNIT FAULT). REMOVED AND REPLACED EPSU PER AMM 33-51-38-000-801-A AND 33-51-38-400-801-A AND TEST ARE OK PER AMM 33-51-00-820-801-A.

Part: STRINGER — CRACKED (FRAME 53.8) · airframe 80,037 hrs · 11,895 cycles

A CRACK INDICATION ON STRINGER 14L, FRAME 53.5 + 1 INCH. REPAIRED THE STRINGER IAW EA 278531.

Part: STRINGER — CRACKED (FRAME 53) · airframe 80,037 hrs · 11,895 cycles

A CRACK INDICATION ON STRINGER 15R, FRAMES 53.5 + 2 TO 53.54. REPLACED THE STRINGER IAW SRM 51-72-11, AND DRAWING F53370020.

Part: STRINGER — CRACKED (FRAMES 53.5) · airframe 80,037 hrs · 11,895 cycles

CRACK INDICATION ON STRINGER 15L, FRAMES 53.5 + 2 INCHES TO 53.5A. REPLACED THE STRINGER IAW SRM 51-72-11, AND DRAWING F53370020.

Part: STRINGER — CRACKED (FRAME 53.8) · airframe 80,037 hrs · 11,895 cycles

A CRACK INDICATION ON STRINGER 14R, FRAMES 53.8. REPAIRED THE STRINGER IAW EA 278482.

Part: STRINGER — CRACKED (FRAME 53.8) · airframe 80,037 hrs · 11,895 cycles

CRACK INDICATION ON STRINGER 15L, AT FR 53.8 - 1. REPLACED THE STRINGER IAW SRM IAW 51-72-11, AND DRAWING F53370020.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 79,965 hrs · 11,885 cycles

EXIT SIGN OVER DOOR 3L MISSING. MAINTENANCE SECURED EXIT SIGN AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 79,911 hrs · 11,875 cycles

SEAT 19G EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 78,000 hrs · 11,608 cycles

AIRCRAFT WAS NOT GROUNDED. 3L DOOR EMERGENCY EXIT SIGN FELL OFF. REATTACHED EMERGENCY EXIT LENS COVER AT 3L DOOR.

Part: TRACK — DIRTY (R2 DOOR) · airframe 77,363 hrs · 11,526 cycles

FLIGHT ATTENDANT HAD DIFFICULTY ARMING 2R DOOR. REMOVED DEBRIS FROM DOOR SLIDE TRACK.

Part: LENS — DETACHED (EMERGENCY SIGN) · airframe 76,703 hrs · 11,435 cycles

EXIT SIGN LENS AT THE R3 DOOR DETACHED. INSTALLED THE EXIT SIGN LENS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 75,939 hrs · 11,322 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT INOPERATIVE, WALL MOUNTED SMALL LIGHTS AT 3L/3R DOORS. MAINTENANCE FOUND CONNECTORS LOOSE AT BOTH DOORS. RECONNECTED THE CONNECTORS. AIRCRAFT WAS GROUNDED.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 75,654 hrs · 11,267 cycles

CIDS 1 EMERGENCY LIGHT POWER SUPPLY UNIT SYSTEM TEST SHOWS FAULT MESSAGE ON BATTERY. REPLACED THE BATTERY IAW AMM 33-51-38.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 75,654 hrs · 11,267 cycles

EXIT SIGN LOCATED ON THE SIDE OF THE L3 DOOR HAS A LOOSE LENS. REPLACED THE LENS IAW AMM 33-51-16.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 75,654 hrs · 11,267 cycles

CIDS 1 EMERGENCY POWER SUPPLY UNIT SYSTEM TEST SHOWS FAULT MESSAGE ON BATTERY. THE POWER SUPPLY UNIT WAS REPLACED IAW AMM 33-51-38.

Part: LIGHT — CRACKED (CABIN) · airframe 75,654 hrs · 11,267 cycles

CRACKED EXIT LIGHT ASSEMBLY AT L2 DOOR. REPLACED EXIT LIGHT ASSEMBLY IAW AMM 33-41-16.

Part: LIGHT — WORN (CABIN) · airframe 75,654 hrs · 11,267 cycles

WORN OUT CABIN EMERGENCY LIGHTING IN FORWARD, MID, AND AFT CABIN ZONE. REPLACED THE EMERGENCY LIGHTS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON CROSSBEAM AT -Y120 AND FR 67. REPAIRED CROSSBEAM SRM 53-41-14-201.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN BARREL NUT FITTING AT -Y1280 AND FR 72. REPLACED FITTING PER SRM 53-41-14 AND SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN BARREL NUT FITTING AT -Y1280 AND FR 73. REPLACED FITTING PER SRM 53-41-14 AND SRM 51-42-11.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SUPPORT ANGLE AT Y1137.1 AFT OF FR 80. REPLACED SUPPORT ANGLE PER SRM 53-41-14 AND SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BARREL NUT FITTING AT Y1280 AND FR 73. REPLACED FITTING PER SRM 53-41-14 AND SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN BARREL NUT FITTING AT Y1280 AND FR72. REPLACED FITTING PER SRM 53-41-14 AND SRM 51-42-11.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SUPPORT ANGLE AT Y1137.1 AFT OF FR 80. REPLACED SUPPORT ANGLE PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT Y1137.1 AND FR 75A. REPLACED AUXILIARY BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT WAS NOT GROUNDED. DAMAGED MID CABIN EMERGENCY LIGHT WIRE 704WL21. REPAIRED WIRE HARNESS PER ESPM 20-53-29.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT CABIN AUXILIARY BEAM AT Y1959 BETWEEN FR71 AND FR72. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM NUT PLATE HOLES AT Y1447.8 AND FR 75A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT Y1137.1 AND FR 75A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT -Y1137.1 AND FR 74. REPAIRED LONGERON BEAM PER SRM 53-41-14.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT Y1447.8 BETWEEN FR 75 AND FR 76. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT Y380 AND FR 78. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT WAS NOT GROUNDED. DAMAGED AFT CABIN EMERGENCY LIGHT WIRE 706WL33. REPAIRED WIRE HARNESS PER ESPM 20-53-29.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT WAS NOT GROUNDED. DAMAGED AFT CABIN EMERGENCY LIGHT WIRE 706WL34. REPAIRED WIRE HARNESS PER ESPM 20-53-29.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT Y1137.1 AND FR 78. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR SILL AT Y2462 AND FR 74. REPLACED DOOR SILL PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT -Y450 AND FR 78. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT -Y1447.8 AND FR 75A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM ATY1959 AND FR 73A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT -794.3 AND FR 75A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT -Y2462 AND FR 73A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT Y450 AND FR 78. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y1650 AND FR 73A. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT Y1959 AND FR 73A. REPLACED BEAM PER SRM 53-41-14 AND SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT -Y380 AND FR 78. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON R4 DOOR MIDDLE FILLER AT -Y2462 AND FR74. REPLACED FILLER PER SRM 53-41-14 AND SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT -Y1137.1 AND FR 78. REPAIRED FLOORBEAM PER SRM 53-00-14.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED FORWARD CABIN EMERGENCY LIGHT WIRE 618WL11. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED MID CABIN SEAT EMERGENCY LIGHT WIRE 702WL31. REPLACED WIRE HARNESS PER AMM 35-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED MID CABIN SEAT EMERGENCY LIGHT WIRE 701WL13. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED AFT CABIN SEAT EMERGENCY LIGHT WIRE 703WL41. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED AFT CABIN SEAT EMERGENCY LIGHT WIRE 701WL48. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED AFT CABIN SEAT EMERGENCY LIGHT WIRE 703WL42. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED CABIN SEAT EMERGENCY LIGHT WIRE 706WL24. REPAIRED WIRE HARNESS PER ESPM 20-53-29.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y2462 AND FR 53. REPLACED SEAT TRACK PER SRM 53-31-15, SRM 51-42-11 AND SRM 51-44-11.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

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

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SUPPORT ANGLE AT -Y2462 AND FR 75A. REPLACED SUPPORT ANGLE PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FILLER AT -Y2465 AND FR 74. REPLACED FILLER PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 35) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON MID CABIN SEAT TRACK AT Y1456 AND FR 35. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: STRUCTURE — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON LONGERON AT -Y794.3 BETWEEN FR 75 AND FR 76. REPLACED LONGERON PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM AT -Y1137.1 AND FR 78. REPAIRED FLOORBEAM PER SRM 53-00-14.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. FORWARD CABIN SEAT EMERGENCY LIGHT 618WL5 WIRE DAMAGED. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 7,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. AFT CABIN EMERGENCY LIGHT 701WL47 WIRE DAMAGED. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. MID CABIN EMERGENCY LIGHT 701WL25 WIRE DAMAGED. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. FORWARD CABIN EMERGENCY LIGHT 618WL6 WIRE DAMAGED. REPLACED WIRE HARNESS PER AMM 33-51-12.

Part: SEAT TRACK — CORRODED (FRAME 34) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON SEAT TRACK AT -Y953 AND FRAME 34. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: SUPPORT ANGLE — CORRODED (FRAME 76) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN, SUPPORT ANGLE AT Y2462 AND FRAME 76, AT NUT PLATE HOLES. REPLACED THE SUPPORT ANGLE IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FRAME 73A) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN AUXILARY BEAM AT -Y1959 AND FRAME 73A. REPLACED THE BEAM IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 33) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON MID CABIN FLOORBEAM AT Y953 AND FRAME 33. REPLACED FLOORBEAM IAW SRM 53-00-14.

Part: DOOR SILL — CORRODED (L4 DOOR) · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN L4 DOOR METAL DOOR SILL. REPLACED DOOR SILL IAW 33C27053005.

Part: DOOR SILL — CORRODED (L2 DOORWAY) · airframe 75,654 hrs · 11,267 cycles

CORROSION ON FORWARD CABIN L2 DOOR METAL DOOR SILL. REPLACED THE DOOR SILL IAW 33C23053005.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON FLOORBEAM AT -Y450 AND FRAME 17. REPLACED FLOORBEAM IAW SRM 53-11-14, SRM 51-42-11, SRM 51-44-11.

Part: DOOR SILL — CORRODED (R4 DOOR) · airframe 75,654 hrs · 11,267 cycles

CORRSION ON AFT CABIN R4 DOOR METAL DOOR SILL. REPLACED THE DOOR SILL IAW 33C27053005.

Part: SEAT TRACK — CORRODED (FRAME 35) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON SEAT TRACK AT Y1552.5 AND FRAME 35. REPLACED SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 AND SRM 51-44-11.

Part: THRESHOLD — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON THRESHOLD ASSEMBLY AT -Y2462 AND FRAME 74. REPLACED THRESHOLD IAW SRM 51-73-11,SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN FLOORBEAM AT Y648, FR 74 AT BARREL NUT HOLES. REPLACED THE FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN FLOORBEAM AT -Y648 AND FRAME 74. REPLACED FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON AFT CABIN FLOORBEAM AT Y2462 AND FRAME 73. REPLACE THE FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AUXILIARY BEAM AT -Y1959 BETWEEN FR 71 AND FR 72. REPLACED BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 75A) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

CORROSION ON FLOORBEAM AT -Y2462 AND FRAME 75A. REPLACED THE FLOORBEAM IAW SRM 53-41-14, SRM 51-21-11, AND SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN SEAT TRACK AT -Y450 AND FR2 19. REPLACED SEAT TRACK PER SRM 53-00-15.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN AUXILIARY BEAM AT -Y1959 AND FR 72. REPLACED BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y2462 AND FR 73A. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MID CABIN FLOOR SUPPORT AT Y0 AND FR 37. REPLACED FLOOR SUPPORT PER SRM 53-21-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT Y1250 BETWEEN FR 73 AND FR 74. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT Y450 AND FR 75. REPLACE SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT Y1250 BETWEEN FR 73 AND FR 74. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN LONGERON AT Y794.3 AND FR73. REPLACED LONGERON PER SRM 53-41-14, SRM 51-42-11, SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT LONGERON AT YO AND FR 73. REPLACED LONGERON PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN FLOOR SUPPORT AT Y230 AND FR14. REPLACED FLOOR SUPPORT PER SRM 53-11-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN SEAT TRACK AT -Y450 AND FR 75. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11 AND SRM 51-44-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND SIDE AFT CABIN LONGERON BEAM AT -Y1447, BETWEEN FR 74 AND FR 77. REPLACED LONGERON BEAM PER SRM 51-74-00, SRM53-41-14, AND SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 75,654 hrs · 11,267 cycles

DELAMINTATION ON CABIN FLOOR PANEL 251EF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 75,654 hrs · 11,267 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR PANEL 271AG. REPLACED THE FLOOR PANEL IAW SRM 53-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y1552.5 BETWEEN FR 32 AND FR 34. REPLACED SEAT TRACK PER SRM 53-00-15,SRM 51-42-11,SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y1959 AND FR 35. REPLACED SEAT TRACK PER SRM 53-00-15, SRM 41-42-11, SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,654 hrs · 11,267 cycles

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

Part: DOOR — OBSTRUCTED (L4) · airframe 75,628 hrs · 11,264 cycles

L4 DOOR SLIDE WILL NOT ARM. MAINTENANCE REMOVED DEBRIS FROM DOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DETACHED (EMERGENCY LIGHTS) · airframe 74,783 hrs · 11,148 cycles

EXIT COVER SIGN CAME OFF AT 3L. REPLACED EXIT LIGHT COVER PER AMM 33-51-16

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,410 hrs · 10,850 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT JUMP SEAT AT 1L , BREAKAWAY FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SIGN — MISSING (CABIN) · airframe 71,939 hrs · 10,760 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN AT DOOR 3R MISSING. INSTALLED EXIT SIGN AT 3R DOOR.

Part: BATTERY — FAULTED (CABIN) · airframe 71,874 hrs · 10,742 cycles

AIRCRAFT WAS NOT GNDED. WHILE ACCOMPLISHING EMER LIGHTING BATTERY CAPACITY CHECK, BATTERY AT 2L FAULTED. R & R EPSU BATTERY 2L IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.

Part: BATTERY — FAULTED (CABIN) · airframe 71,874 hrs · 10,742 cycles

AIRCRAFT WAS NOT GNDED. WHILE ACCOMPLISHING EMER LIGHTING BATTERY CAPACITY CHECK, BATTERY AT 1L FAULTED. R & R EPSU BATTERY AT 1L IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 71,627 hrs · 10,688 cycles

AIRCRAFT WAS NOT GNDED. SEAT 11G EMER EXIT PATH LIGHT INOPERATIVE. FOUND WIRE DISCONNECTED, SECURED & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — LOOSE (CABIN) · airframe 71,253 hrs · 10,602 cycles

AIRCRAFT WAS NOT GNDED. LENS COVER FOR EMER EXIT LIGHT AT 25F NEEDS TO BE SECURED. SECURED EMER EXIT LIGHT LENS AT 25F.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 71,166 hrs · 10,588 cycles

AIRCRAFT WAS NOT GNDED. FLASHLIGHT BY 4L JUMP SEAT NEEDS TO BE REPLACED. REPLACED FLASHLIGHT.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 71,154 hrs · 10,583 cycles

AIRCRAFT WAS NOT GNDED. FUEL TRIM TANK PUMP LOW PRESS INDICATION. R & R TRIM TANK TRANSFER PUMP IAW AMM 28-27-48-000-801-A 400-801-A & TRANSFER PUMP PRESS SWITCH IAW AMM 28-27-11-000-801-A 400-801-A. LEAK & OPERATION CHECKED NORMAL. SEE ALSO AALA201512119009.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 71,154 hrs · 10,583 cycles

AIRCRAFT WAS NOT GNDED. FUEL TRIM TANK PUMP LOW PRESS INDICATION. R & R TRIM TANK TRANSFER PUMP IAW AMM 28-27-48-000-801-A 400-801-A & TRANSFER PUMP PRESS SWITCH IAW AMM 28-27-11-000-801-A 400-801-A. LEAK & OPERATIONS CHECKED NORMAL. SEE ALSO AALA201512119010.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 70,948 hrs · 10,547 cycles

R1 DOOR SLIDE SHOWS LOW PSI ON CIDS & SERVICING REPORT SLIDE GAUGE READS WELL WITHIN THE GREEN BAND, SLIDE PACK WERE RE-ARMED THIS SHIFT. REPLACED R1 DOOR SLIDE RAFT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-801-A-01 & 25-62-41.

Part: FITTING — FAULTY (EVAC SLIDE) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, SLIDE FITTING 20DH FAILS OPERATIONAL TEST. REPLACED 20DH SLIDE FITTING IAW AMM 30-46-11-000-801-A & AMM 30-46-11-400-801-A. OPERATIONAL TESTED GOOD IAW AMM 30-46-000-710-801-A. ADJUSTED GIRT BAR FITTING IAW AMM 52-22-00-820-801-A.

Part: FITTING — FAULTY (EVAC SLIDE) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, SLIDE FITTING 19DH FAILS OPERATIONAL TEST. REPLACED 19DH SLIDE FITTING IAW AMM 30-46-11-000-801-A & AMM 30-46-11-400-801-A. OPERATIONS TESTED GOOD IAW AMM 30-46-00-710-801-A. ADJUSTED GIRT BAR FITTING IAW AMM 52-22-00-820-801-A.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, EMER LIGHT HARNESS IN SEAT 4A DAMAGED. REPLACED EMER LIGHT HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-801-A.

Part: WIRE — EXPOSED (CABIN) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, EMER LIGHT HARNESS HAS EXPOSED WIRING. REPLACED EMER LIGHT WIRE HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-801-A.

Part: CONTROL UNIT — FAILED (ZONE 100) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, 21DH CONTROL UNIT SLIDE FITTING HEAT G FAILS OPERATIONAL TEST. REPLACED SLIDE FITTING CONTROL UNIT 21DH & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 30- 46-000-8011-400-801A & 30-46-00-710-801-A.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 70,939 hrs · 10,545 cycles

C1 CHECK, AFT PIT FLOOR PANEL 152HF HAS THREE EACH CRACKS IN UPPER SKIN. REPLACED FLOOR PANEL IAW SRM 51-42-11 & AMM 53-00-00-400-802.

Part: ISOLATION VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 70,582 hrs · 10,499 cycles

FUEL TRIM TANK XFR FAULT ECAM. REPLACED FUEL TRIM PIPE ISOLATION VLV & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-27-53-400-801-A.

Part: BATTERY — FAULTY (CABIN) · airframe 70,483 hrs · 10,487 cycles

RON, NR 1 BATTERY LIGHT ILLUMINATED & NR 2 FAULT LIGHT ILLUMINATED DURING CHECK OF ASPSU BATTERY CHECK ON JC 33C21052004. R & R EMER ASPSU BATTERY NR 2 IAW AMM 52-71-36. SEE ALSO AALA201509309006.

Part: BATTERY — FAULTY (CABIN) · airframe 70,483 hrs · 10,487 cycles

RON, NR 1 BATTERY LIGHT ILLUMINATED & NR 2 FAULT LIGHT ILLUMINATED DURING CHECK OF ASPSU BATTERY CHECK ON JC 33C21052004. R & R EMER ASPSU BATTERY NR 1 IAW AMM 52-71-36. SEE ALSO AALA201509309019.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 70,367 hrs · 10,468 cycles

FLIGHT 720, DURING CRUISE, CREW NOTED NR 2 PACK OUTPUT TEMP HIGH, 40 C AT FL 350. R & R TEMP CONTROL VLV 522HH3 IAW AMM 21-53-53-000-801-A. OPERATIONAL CHECKED GOOD.

Part: ENGINE — LEAKING (NR 2) · airframe 70,138 hrs · 10,435 cycles

FLIGHT 9200 EN-ROUTE, DURING CRUISE, ENG 2 OIL PRESS WENT TO ZERO. ENG 2 WAS SHUT DOWN. THE FLIGHT DECLARED AN EMER & DIVERTED WHERE IT LANDED WITHOUT FURTHER INCIDENT. R & R NR 2 ENG ASSEMBLY IAW JC 33L40071001.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS)

DURING ACCOMPLISHMENT OF A CHECK JC 33C20033002, EMERGENCY BATTERY CAPACITY CHECK FAULTED EPSU 2R 14WL & EPSU 4L 17WL. REPLACED BATTERY PACK AT EPSU 2R 14WL & PSU 4L 17WL IAW AMM 33-51-38-400-802.

Part: LENS — MISSING (CABIN) · airframe 68,772 hrs · 10,250 cycles

EMERGENCY LIGHT PLASTIC COVER IS MISSING FROM BOTTOM OF WALL, AFT LT AHEAD OF GALLEY. REPLACED THE EMER LIGHT LENS COVER.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 68,297 hrs · 10,187 cycles

CUSTOMER CARE CHECK. AFT CABIN FLOOR PANEL 272KF DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-00-00-400-801.

Part: GUIDE — CORRODED (NLG STRUT) · airframe 68,197 hrs · 10,172 cycles

NOSE LANDING GEAR LOWER STRUT LEG, LOWER GUIDE HAS CORROSION. REPLACED NLG LOWER STRUT LEG, LOWER GUIDE IAW AMM 32-21-13.

Part: LENS — MISSING (CABIN) · airframe 67,571 hrs · 10,039 cycles

SEAT EMER LIGHT LENS MISSING AT SEAT 8B, 13G & 28B. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKS OK.

Part: COVER — UNSECURE (CABIN) · airframe 66,582 hrs · 9,848 cycles

DOOR 2L EMER LIGHT COVER FELL OFF DURING LANDING. ADJUSTED EMER LIGHT COVER TABS ON DOOR 2L FOUND TO BE SECURE AT THIS TIME.

Part: COVER — DETACHED (EXIT SIGN) · airframe 66,462 hrs · 9,832 cycles

EXIT 3L SIGN COVER NEEDS TO BE RE ATTACHED. FIXED COVER.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 65,113 hrs · 9,656 cycles

FLASHLIGHT AT 3R DOOR INOPERATIVE, BATTERY LIGHT NOT FLASHING. REPLACED 3R DOOR FLASHLIGHT. OPERATIONAL CHECK IS GOOD.

Part: SIGN — MISSING (CABIN) · airframe 64,538 hrs · 9,582 cycles

4L EXIT SIGN ABOVE DOOR MISSING. REPLACED SIGN.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK, CRACK ON LT NR 1 SLAT TOP SKIN AT 2.2 INCHES PARALLEL TO TE & 6.5 INCHES PARALLEL TO INBD EDGE & 2.8 INCHES FROM NR 1 SLAT OTBD TE. REPAIRED SLAT TOP SKIN IAW EA 505976.

Part: RIB — CRACKED (LE SLAT) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK, CRACK ON LT NR 1 SLAT OTBD END RIB AT 2.2 INCHES PARALLEL TO TE & 6.5 INCHES PARALLEL TO INBD EDGE & 2.8 INCHES FROM NR 1 SLAT OTBD TE. REPAIRED NR 1 SLAT OTBD END RIB IAW EA 505976.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

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

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252KG BETWEEN FRAME 50 TO FRAME 51 & BETWEEN -Y 1456 TO -Y 953. REPLACED FLOOR PANEL 252KG IAW SRM 53-02-00, PAR 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 252JG BETWEEN FRAME 47 TO FRAME 50 & BETWEEN -Y 1456 TO -Y 953. REPLACED FLOOR PANEL 252JG IAW SRM 53-02-00, PAR 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251MF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN Y 953 TO Y 450. REPLACED FLOOR PANEL 251MF IAW SRM 53-02-00, PAR 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 261YG BETWEEN FRAME 69 TO FRAME 71 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261YG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 261ZG BETWEEN FRAME 69 TO FRAME 71 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 261ZG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 261TG BETWEEN FRAME 65 TO FRAME 69 & BETWEEN Y953 TO Y1959. REPLACED FLOOR PANEL 261TG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 232DG BETWEEN FRAME 26.4 TO FRAME 31 & BETWEEN Y 948 TO -Y 1124. REPLACED FLOOR PANEL 232DG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 251CG BETWEEN FRAME 42 TO FRAME 47 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251CG IAW SRM 53-02-00, PAR 5I, FIG 211 & MM 53-00-00.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 261UG BETWEEN FRAME 65 TO FRAME 69 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 261UG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 231CG BETWEEN FRAME 26.4 TO FRAME 30 & BETWEEN Y 678 TO Y 984. REPLACED FLOOR PANEL 231CG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 63,853 hrs · 9,486 cycles

C2 CHECK PEELED PLIES ON FLOOR PANEL 231BG BETWEEN FRAME 26.4 TO FRAME 31 & BETWEEN Y450 TO Y690. REPLACED FLOOR PANEL 231BG IAW SRM 53-02-00, PAR 5I, FIG 211.

Part: MONITOR — MALFUNCTIONED (CABIN) · airframe 62,855 hrs · 9,340 cycles

PASSENGER REPORTED SMELLING SMOKE FROM VIDEO AT 15G. INSPECTED SEAT CABLES FOR DAMAGE SEAT 15G, NO FAULTS FOUND. REPLACED 15G VIDEO MONITOR, SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,687 hrs · 9,318 cycles

R3 EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE LAMPS, OPS CHECKED GOOD.

Part: MONITOR — UNKNOWN (ZONE 200) · airframe 62,386 hrs · 9,277 cycles

PASSENGER REPORTED PUFF OF SMOKE FROM TOP OF THE VIDEO SCREEN AT SEAT 23C. VIDEO SCREEN SEEMS TO OPERATE NORMALLY. MAINTENANCE REPLACED MONITOR AT 23C.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 61,425 hrs · 9,157 cycles

R3 DOOR OVERHEAD EXIT LIGHT FELL OFF DURING TAKEOFF. MX REPOSITIONED AND SECURED EXIT LIGHT COVER.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 61,354 hrs · 9,147 cycles

EMERGENCY EXIT SIGN CAME OFF AT L3 DOOR. MX INSTALLED EMERGENCY EXIT SIGN, OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,235 hrs · 9,131 cycles

EXIT LIGHT LENS OVER 3L DOOR MISSING. MX REPLACED LENS.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 61,027 hrs · 9,104 cycles

EXIT SIGN COVER FELL OFF ON TAKEOFF. MX REINSTALLED COVER. OK FOR SERVICE

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 61,027 hrs · 9,104 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2G INOPERATIVE. REPLACED TERMINAL LUG.

Part: GUIDE — OUT OF POSITION (R1 DOOR) · airframe 60,849 hrs · 9,082 cycles

ACFT 1R DOOR EXTREMELY DIFFICULT TO DISARM. MX INSTALLED DOOR LINKAGE GUIDE IN CORRECT POSITION. OPS CHECKS GOOD, DOOR OPERATES , FUNCTIONS NORMALLY.

Part: SLIDER — LACK OF LUBE (R1 DOOR) · airframe 60,719 hrs · 9,066 cycles

SLIDE DISARM LEVER AT 1R HANGS UP AT AN INTERMEDIATE POSTION WHEN DISARMING DOOR. MX CHECKED FUNCTIONAL OPS OF GIRT BAR. CHECK IS GOOD. LUBED GIRT BAR & SLIDERS.

Part: SIGN — DETACHED (CABIN) · airframe 59,451 hrs · 8,898 cycles

FORWARD ENTRY EXIT SIGN FELL DOWN. MAINTENANCE INSTALLED FWD EXIT SIGN.

Part: COVER — DETACHED (EXIT SIGN) · airframe 59,436 hrs · 8,896 cycles

THE 3R EXIT SIGN COVER DETACHED. MAINTENANCE REPLACED 3R EXIT SIGN COVER.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 59,337 hrs · 8,883 cycles

FRA - OVERHEAD EXIT SIGN AT R-3 DOOR COVER FELL OFF (LOOSE BEST FIT). RE-SECURED EXIT SIGN COVER AT DOOR 3R.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,836 hrs · 8,811 cycles

ESPSU BATTERY 2L FAILED ESPSU BATTERY CAP TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES FOR 2L AND BATTERY SUPPLY UNIT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,836 hrs · 8,811 cycles

1L EPSU BATTERY FAILED BATTERY CAP TEST. MAINTENANCE REMOVED AND REPLACED 1L EPSU BATTERY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,836 hrs · 8,811 cycles

ESPSU BATTERY 3R FAILED BATTERY CAP TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES FOR 3R AND BATTERY SUPPLY UNITS.

Part: SIGN — UNSECURE (CABIN) · airframe 57,974 hrs · 8,692 cycles

CEILING EXIT SIGN AT 3L FELL OFF NEEDS TO BE SECURED. MAINTENANCE RE-SECURED EXIT SIGN AT 3L OPERATIONAL CHECK IS OKAY.

Part: LENS — MISSING (CABIN) · airframe 56,806 hrs · 8,540 cycles

CLT - 3L DOOR EXIT LIGHT COVER MISSING. REPLACED LENS COVER, CHECKS OK.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - DOOR ASSIST BOTTLE FOR R1 DOOR NEEDS TO BE SERVICED. SERVICED R1 DOOR ASSIST BOTTLE IAW A330 AMM 52-1000-600-802-A, NO LEAKS NOTED.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - DOOR ASSIST BOTTLES FOR R3 DOOR NEEDS TO BE SERVICED. SERVICED R3 DOOR ASSIST BOTTLE IAW A330 AMM 52-1000-600-801-A, NO LEAKS NOTED.

Part: ANGLE — DAMAGED (RT WING) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 A/C'S AT RIB 1 / FR 42, OUTER ANGLES REMOVED & RE-INSTALLED / REPLACED AS REQUIRED. REPLACED OUTER ANGLE ON RIGHT SIDE AT FR42, RIB 1 IAW EA 103839A.

Part: SPAR — CRACKED (RT WING) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - CRACK ON RIGHT CENTER SPAR WEB AT FR42, WING RIB 1. REPAIRED RIGHT CENTER SPAR WEB AT FR42, WING RIB 1 IAW EA 134659.

Part: ANGLE — DAMAGED (LT WING) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 A/C'S AT RIB 1 / FR 42, OUTER ANGLES REMOVED & RE-INSTALLED / REPLACED AS REQUIRED. REPLACED OUTER ANGLE ON LEFT SIDE AT FR42, RIB 1 IAW EA 103839A.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 55,602 hrs · 8,383 cycles

C11 CHECK - MOISTURE INGESSION ON UPPER SURFACE OF LEFT ELEVATOR AT ELEVATOR RIBS 2, 3, 6, 7, 8, 9 & 10 BETWEEN 2.3 TO 4.2 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A330 SRM 55-21-11 & EO 5511UO56.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 55,602 hrs · 8,383 cycles

C11 CHECK - MOISTURE INGESSION ON UPPER SURFACE OF RIGHT ELEVATOR AT ELEVATOR RIBS 2, 6, 7, 10 & 11 BETWEEN 3.5 TO 4 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW EO 5511UO56.

Part: SUPPORT — CRACKED (BELLY FAIRING) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - CRACK ON BELLY FAIRING SUPPORT AT FR 53.2, OUTBOARD OF S35L. REPAIRED BELLY FAIRING SUPPORT IAW SRM 53-35-14, FIG 202.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON BELLY FAIRING SUPPORT BETWEEN FR40 TO FR44, -Y430. REPLACED BELLY FAIRING SUPPORT BETWEEN FR40 TO FR44, -Y430 IAW A330 SRM 51-72-11 & 51-42-11.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,602 hrs · 8,383 cycles

C1 CHECK - CRACK ON BELLY FAIRING SUPPORT AT FR53.2, OUTBOARD OF S35L. REPAIRED BELLY FAIRING SUPPORT AT FR53.2, OUTBOARD OF S35L IAW A330 SRM 53-35-14, FIG. 202.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 54,872 hrs · 8,291 cycles

ON TAKEOFF, OVERHEAD CEILING LIGHT ROW 23 LEFT FELL OFF . MAINTENANCE REPLACED "EXIT" LIGHT COVER & TESTED OKAY.

Part: COVER — BROKEN (EXIT SIGN) · airframe 53,291 hrs · 8,089 cycles

OVERHEAD EXIT SIGN - COVER BROKEN AT 3L. REPLACED OVERHEAD EXIT SIGN COVER 3L.

Part: COVER — MISSING (CABIN) · airframe 52,374 hrs · 7,974 cycles

PHL - EMERGENCY EXIT LIGHT COVER, ON THE WALL ADJACENT SEAT 23C, IS MISSING. MAINTENANCE REPLACED LIGHT COVER.

Part: COVER — UNSECURE (CABIN) · airframe 52,192 hrs · 7,950 cycles

FRA - MID GALLEY AIRCRAFT RIGHT COVER LOWER LIGHT FELL OFF. MAINTENANCE RESECURED THE MID GALLEY RIGHT FORWARD COVER. OKAY FOR SERVICE.

Part: COVER — OUT OF POSITION (EXIT SIGN) · airframe 51,689 hrs · 7,885 cycles

EXIT SIGN COVER 3L FELL OFF. MAINTENANCE RE-ATTACHED EXIT SIGN AT 3L, OK FOR CONTINUED SERVICE.

Part: LENS — MISSING (CABIN)

CLT - EXIT SIGN COVER L3 MISSING. REPLACED EMERGENCY EXIT LIGHT LENS 3H.

Part: WIRE — BROKEN (CABIN)

CLT - THE EMERGENCY LIGHT AT ROW 22G/H IS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE IN-SEAT CONNECTOR.

Part: FASTENER — LOOSE (CENTER WING) · airframe 50,515 hrs · 7,728 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 102861A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

FRA - THE CREW REQUESTED THAT THE L3 DOOR ASSIST BOTTLE PRESSURE BE CHECKED. MAINTENANCE SERVICED THE L3 DOOR ASSIST BOTTLE.

Part: MEGAPHONE — UNSERVICEABLE (CABIN)

LGW - THE FORWARD MEGAPHONE WAS FOUND UNSERVICEABLE. THE FORWARD MEGAPHONE WAS REPLACED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

LGW - THE L3 DOOR ASSIST BOTTLE SHOWS LOW PRESSURE ON SERVICE REPORT. THE L3 DOOR BOTTLE WAS SERVICED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - FLASHLIGHTS AT L1 AFT SEAT, BOTH SEATS AT R4, AND ONE SEAT AT L4 OUTBOARD HAVE DEAD BATTERIES. MAINTENANCE REPLACED FLASHLIGHT MOUNTS AND BATTERIES AT FLIGHT ATTENDANT SEATS L1 AFT, BOTH R4 AFT, AND L4 OUTBOARD.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS EPSU TEST FAULTS BATT AT R1, R4, AND L4. MAINTENANCE REPLACED THE EPSU BATTERIES.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGERON AT FR73 + 20 INCHES, Y650. REPLACED LONGERON AT FR73 + 20 INCHES, Y650 IAW SRM 51-72-11.

Part: O-RING — LEAKING (HYD SYSTEM)

FLT 9465 - MAINTENANCE TEST FLT FROM CWF TO CWF. DURING CLIMB, FROM APPROXIMATELY 4,000 TO 8,000 FEET, THE COCKPIT FILLED WITH FUMES. THE CREW DONNED THE OXYGEN MASKS, PERFORMED QRH TASKS TO SHUT OFF THE PACKS, AND DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO FIELD CWF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED PACKS ONE AND TWO, APU, AC, FWD AIR DIST & BULK BAYS. NO DEFECTS NOTED. INSPECTED THE HYDRAULIC FLUID SEPARATORS. REMOVED AND REPLACED THE NR 2 PRECOOLER & REPLACED THE BLUE BOWL MANIFOLD O-RINGS. SERVICED THE GREEN SYSTEM RESERVOIR. PERFORMED LEAK AND OPERATIONAL CHECKS. NO FAULTS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM UPPER CHORD AT FR75, S26L, Y450. REPAIRED FLOORBEAM UPPER CHORD AT FR75, S26L, Y450 IAW SRM 53-41-14.

Part: SLIDE — UNLACED (L3 DOOR) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - EES - L-3 DOOR SLIDE DISCOVERED UNLACED WHILE PERFORMING A PROXIMITY CHECK. REPLACED L-3 DOOR SLIDE IAW A330 AMM 25-62-42-860-050 & 25-62-42-400-801.

Part: SLIDE — UNLACED (R3 DOOR) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - EES - R-3 DOOR SLIDE WAS DISCOVERED UNLACED DURING PROXIMITY CHECK. REPLACED R-3 DOOR SLIDE & PERFORMED TEST IAW A330 SRM 25-62-42-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR SUPPORT BETWEEN FR11 TO FR14, -Y701. REPLACED FLOOR SUPPORT BETWEEN FR11 TO FR14, -Y701 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR74 + 8 INCHES, Y450. REPLACED SEAT TRACK AT FR74 + 8 INCHES, Y450 IAW A330 SRM 51-44-11. SUP - AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING. THE CORROSION LEVEL FIELD WAS UPDATED TO REFLECT THIS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

MAJOR REPAIR -S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK AT FR 29 + 12 - FR 30+3, S26, -Y450, WL =0. REPLACED SEAT TRACK AT FR 29 + 12 - FR 30+3, S26, -Y450, WL =0 IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR SUPPORT AT FR71, S26R, -Y793. REPLACED FLOOR SUPPORT AT FR71, S26R, -Y793 IAW SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR PANEL 272JF COVER PLATE BETWEEN FR74 TO FR76 & BETWEEN -Y1145 TO -Y1450. REPLACED FLOOR PANEL 272JF COVER PLATE BETWEEN FR74 TO FR76 & BETWEEN -Y1145 TO -Y1450 IAW EA 140238.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR74 + 8 INCHES, S26L, Y450. REPLACED SEAT TRACK AT FR74 + 8 INCHES, S26L, Y450 IAW SRM 51-44-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 222KF BETWEEN FR14 TO FR17 & BETWEEN -Y1959 TO -Y2462. REPLACED FLOOR PANEL 222KF BETWEEN FR14 TO FR17 & BETWEEN -Y1959 TO -Y2462 IAW EA 140238.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,985 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 221KF BETWEEN FR14 TO FR17 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 221KF BETWEEN FR14 TO FR17 & BETWEEN Y1959 TO Y2462 IAW EA 140238. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 271KF BETWEEN FR73 TO FR75 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 271KF BETWEEN FR73 TO FR75 & BETWEEN Y1959 TO Y2462 IAW EA 140238. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 271JF BETWEEN FR74 TO FR75 & BETWEEN Y1456 TO Y1959. REPLACED PANEL 271JF BETWEEN FR74 TO FR75 & BETWEEN Y1456 TO Y1959 IAW EA 140238. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - LEVEL 2 CORROSION ON FLOOR PANEL 272KF. REPLACED FLOOR PANEL 272KF IAW EA 140238.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - FLOOR PANEL 241TF INSERTS CORRODED BETWEEN FR33 TO FR34 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 241TF IAW EA 140238.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251NF BETWEEN FR39 TO FR40.1 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 251NF BETWEEN FR39 TO FR40.1 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR35 + 8 INCHES, -Y450. REPLACED SEAT TRACK AT FR35 + 8 INCHES, -Y450 IAW SRM 53-00-05 & 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271HF BETWEEN FR73 TO FR75 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 271HF BETWEEN FR73 TO FR75 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251DG BETWEEN FR42 TO FR47 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 251DG BETWEEN FR42 TO FR47 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 18 - FR 19, -Y953, Z=0. REPLACED SEAT TRACK AT FR 18 - FR 19, -Y953, Z=0 IAW A330 SRM 53-00-15. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232BG BETWEEN FR26.4 TO FR31 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 232BG BETWEEN FR26.4 TO FR31 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252HF BETWEEN FR37.4 TO FR39 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL NR 252HF BETWEEN FR37.4 TO FR39 & BETWEEN -Y953 TO -Y1456 IAW MCGILL IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 50 + 10, S26R, -Y450. REPLACED SEAT TRACK AT FR 50 + 10 S26R, -Y450 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 242GF BETWEEN FR33 TO FR37 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 242GF BETWEEN FR33 TO FR37 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 211EF BETWEEN FR7 TO FR11A & BETWEEN Y490 TO -Y490. REPAIRED FLOOR PANEL 211EF BETWEEN FR7 TO FR11A & BETWEEN Y490 TO -Y490 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251WG BETWEEN FR53.2 TO FR53.4 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 251WG BETWEEN FR53.2 TO FR53.4 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON NR 2 PYLON INBOARD RIB 8A. REPLACED WEB ON NR 2 PYLON INBOARD RIB 8A IAW A330 SRM 51-42-11 & PMS 01-04-21.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231KF BETWEEN FR22 TO FR25 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 231KF BETWEEN FR22 TO FR25 & BETWEEN Y450 TO -Y450 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252KG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252KG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 242LF BETWEEN FR33 TO FR37 & BETWEEN -Y2462 TO SILL. REPAIRED FLOOR PANEL 323PF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON NR 2 PYLON OUTBOARD RIB 8A. REPAIRED WEB ON NR 2 PYLON OUTBOARD RIB 8A IAW A330 SRM 51-42-11 & PMS 01-04-21.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251LG BETWEEN FR47 TO FR51 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251LG BETWEEN FR47 TO FR51 & BETWEEN Y1456 TO Y1959 IAW MCGILL IRM 9701 REV G.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - NR 6315634, CORROSION ON BEAM AT FR 75 + 20, S26R, -Y1950. REPLACED BEAM AT FR 75 + 20, S26R, -Y1950 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 49, S26L, +Y450. REPLACED SEAT TRACK AT FR 49, S26L, +Y450 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 49 + 12, S26L, +Y450. REPLACED SEAT TRACK AT FR 49 + 12, S26L, +Y450 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR53 + 10 INCHES, Y450. REPLACED SEAT TRACK AT FR53 + 10 INCHES, Y450 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33, S25L, +Y450, Z=0. REPLACED SEAT TRACK AT FR 33, S25L, +Y450, Z=0 IAW A330SRM 53-00-15, 51-74-00 & 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 47 + 8, S26L, +Y450. REPLACED SEAT TRACK AT FR 47 + 8, S26L, +Y450 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR45, -Y450, S26R. REPLACED SEAT TRACK AT FFR45, -Y450, S26R IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: BEAM — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM AT FR73, -Y793. REPLACED LONGERON BEAM AT FR73, -Y793 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 52, S26L, +Y450. REPLACED SEAT TRACK AT FR 52, S26L, +Y450 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33 + 6, -Y1536, Z= 0. REPLACED SEAT TRACK AT FR 33 + 6, -Y1536, Z= 0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON AT FR 30, S26, Y=0, Z=0. REPLACED LONGERON AT FR 30, S26, Y=0, Z=0 IAW A330 DRAWING F53275651. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON CROSS BEAM AT FR75, S26R, -Y450. REPAIRED CROSS BEAM AT FR75, S26R, -Y450 IAW A330 SRM 53-41-14 & 53-00-14.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - NR 6309482 - DELAMINATION ON FLOOR PANEL 232EG BETWEEN FR26.4 TO FR31 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 232EG BETWEEN FR26.4 TO FR31 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 38 + 19.5, S26L, +Y450. REPLACED SEAT TRACK AT FR 38 + 19.5, S26L, +Y450 IAW A330 SRM 51-42-11 & 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - NR 6317427 - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR14 TO FR16 & BETWEEN Y953 TO -Y953. REPAIRED FLOOR PANEL 221EF BETWEEN FR14 TO FR16 & BETWEEN Y953 TO -Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33 - FR 34, -Y953, S26R. REPLACED SEAT TRACK AT FR 33 - FR 34, -Y953, S26R IAW A330 SRM 51-44-11 & 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33, S26L, +Y953. REPLACED SEAT TRACK AT FR 33, S26L, +Y953 IAW A330 SRM 51-72-11 & 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: BEAM — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM 1 INCH FORWARD OF FR78, S35R, Y=0. REPLACED LONGERON BEAM AT FR78, S35R, Y=0 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM AT FR75 + 11 INCHES, S35R, -Y387. REPLACED LONGERON BEAM AT FR75 + 11 INCHES, S35R, -Y387 IAW A330 SRM 51-72-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR14 TO FR18, S26R, -Y953. REPLACED SEAT TRACK BETWEEN FR14 TO FR18, S26R, -Y953 IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251QG BETWEEN FR51 TO FR53.2 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 251QG BETWEEN FR51 TO FR53.2 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR14 TO FR18, S26R, -Y450. REPLACED SEAT TRACK BETWEEN FR12A TO FR18, S26R, -Y450 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - 3 AREAS OF LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR 47 - FR 53.2, +Y953, Z = 0. REPLACED SEAT TRACK BETWEEN FR 47 - FR 53.2, +Y953, Z = 0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 47 +7, S26R, -Y450. REPLACED SEAT TRACK AT FR 47 +7, S26R, -Y450 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 43 + 7, S26L, +Y450. REPLACED SEAT TRACK AT FR 43 + 7, S26L, +Y450 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR67 + 9 INCHES,Y450. REPLACED SEAT TRACK BETWEEN FR58 + 10 INCHES TO FR67 + 10 INCHES, Y450 IAW A330 SRM 51-42-11 AND 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 49, S26R, -Y450. REPLACED SEAT TRACK AT FR 49, S26R, -Y450 IAW A330SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 14, S26R, -Y1456, Z=0. REPLACED SEAT TRACK AT FR 14, S26R, -Y1456, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261CH BETWEEN FR55 TO FR57.1 & BETWEEN Y953 TO Y1959. REPAIRED FLOOR PANEL 261CH BETWEEN FR55 TO FR57.1 & BETWEEN Y953 TO Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR65 TO FR66, Y450. REPLACED SEAT TRACK BETWEEN FR65 TO FR66, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR74, Y1250. REPLACED SEAT TRACK AT FR74, Y1250 IAW A330 SRM 51-74-00, 51-42-11 & 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR64 + 5 INCHES, Y450. REPLACED SEAT TRACK AT FR64 + 5 INCHES, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR65 + 19 INCHES, Y450. REPLACED SEAT TRACK AT FR65 + 19 INCHES, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGERON BEAM AT FR73 + 8 INCHES, S25L, Y1231. REPLACED LONGERON BEAM AT FR73 + 8 INCHES, S25L, Y1231 IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CROSS BEAM AT FR78, S35L, Y387. REPAIRED CROSSBEAM AT FR78, S35L, Y387 IAW SRM 53-00-14.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 242DF BETWEEN FR31 TO FR33 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 242DF BETWEEN FR31 TO FR33 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 71PF BETWEEN FR78 TO FR80 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 271PF BETWEEN FR78 TO FR80 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR75, Y=0. REPAIRED FLOORBEAM AT FR75, Y=0 IAW SRM 53-00-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR68 + 3 INCHES, S23R, -Y450. REPLACED SEAT TRACK AT FR68 + 3 INCHES, S23R, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 272HF BETWEEN FR73 TO FR75 + 6 INCHES & BETWEEN -Y793 TO -1143. REPLACED FLOOR PANEL 272HF BETWEEN FR73 TO FR75 + 6 INCHES & BETWEEN -Y793 TO -1143 IAW MCGILL IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR38 + 3.5 INCHES, -Y450. REPLACED SEAT TRACK AT FR38 + 3.5 INCHES, -Y450 IAW A330 SRM 53-31-15, 51-42-11 & 51-75-2. DEFECTIVE AREA WAS EXPANDED TO INCLUDE FR 38 + 18 & FR 39.1 + 7.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261GF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 261GF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261GG BETWEEN FR60 TO FR62 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 261GG BETWEEN FR60 TO FR62 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261NF BETWEEN FR53.9 TO FR55 & BETWEEN Y1457 TO Y1959. REPAIRED FLOOR PANEL 261NF BETWEEN FR53.9 TO FR55 & BETWEEN Y1457 TO Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR38 + 3.5 INCHES, -Y450. REPLACED SEAT TRACK AT FR38 + 3.5 INCHES, -Y450 IAW A330 SRM 53-31-15, 51-42-11 & 51-75-2. DEFECTIVE AREA WAS EXPANDED TO INCLUDE FR 38 + 18 & FR 39.1 + 7.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR58 TO FR60 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 261BG BETWEEN FR58 TO FR60 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: SPAR — DELAMINATED (HORIZ STAB) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON RIGHT HORIZONTAL STABILIZER FRONT SPAR AT LEADING EDGE RIB 4. REPAIRED RIGHT HORIZONTAL STABILIZER FRONT SPAR AT LEADING EDGE RIB 4 IAW EA 140257A.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON BEAM AT FR 73 + 8, S26L, +Y1450. REPLACED BEAM AT FR 73 + 8, S26L, +Y1450 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261JH BETWEEN FR53.7 TO FR53.9 & BETWEEN Y1557 TO Y1959. REPAIRED FLOOR PANEL 261JH BETWEEN FR53.7 TO FR53.9 & BETWEEN Y1557 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261LF BETWEEN FR53.9 TO FR55 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 261LF BETWEEN FR53.9 TO FR55 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON BEAM AT FR 73 + 8, S35, +Y1600. REPLACED LONGERON BEAM AT FR 73 + 8, S35, +Y1600 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262GG BETWEEN FR60 TO FR62 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 262GG BETWEEN FR60 TO FR62 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261WF BETWEEN FR57.1 TO FR58 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 261WF BETWEEN FR57.1 TO FR58 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262PF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y2059 TO Y2407. REPAIRED FLOOR PANEL 262PF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y2059 TO Y2407 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR71 +6 INCHES TO FR75, S35R, -Y457. REPLACED SEAT TRACK BETWEEN FR71 +6 INCHES TO FR75, S35R, -Y457 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262JF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y953 TO Y1457. REPAIRED FLOOR PANEL 262JF BETWEEN FR53.7 TO FR53.9 & BETWEEN Y953 TO Y1457 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262JH BETWEEN FR53.7 TO FR53.9 & BETWEEN -Y11557 TO Y1959. REPAIRED FLOOR PANEL 262JH BETWEEN FR53.7 TO FR53.9 & BETWEEN -Y11557 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261FH BETWEEN FR62 TO FR65 & BETWEEN Y953 TO Y1959. REPAIRED FLOOR PANEL 261FH BETWEEN FR62 TO FR65 & BETWEEN Y953 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261LH BETWEEN FR57.1 TO FR58 & BETWEEN Y953 TO Y1959. REPAIRED FLOOR PANEL 261LH BETWEEN FR57.1 TO FR58 & BETWEEN Y953 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262H BETWEEN FR57.1 TO FR58 & BETWEEN -Y953 TO -Y1959. REPAIRED FLOOR PANEL 262LH BETWEEN FR57.1 TO FR58 & BETWEEN -Y953 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262CF BETWEEN FR53.4 TO FR53.9 & BETWEEN Y1457 TO Y1557. REPAIRED FLOOR PANEL 262CF BETWEEN FR53.4 TO FR53.9 & BETWEEN Y1457 TO Y1557 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251CF BETWEEN FR42 TO FR47 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251CF BETWEEN FR42 TO FR47 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON Z-PROFILE AT FR80, -Y450. REPLACED Z-PROFILE AT FR80, -Y450 IAW SRM 51-72-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON AT FR 74 - FR 80 + 8, +Y1137, Z= 0. REPLACED LONGERON AT FR 74 - FR 80 + 8, +Y1137, Z= 0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252QG BETWEEN FR51 TO FR53.2 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252QG BETWEEN FR51 TO FR53.2 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 132MF BETWEEN FR25 TO FR26.3 & BETWEEN Y867 TO Y1414. REPAIRED FLOOR PANEL 132MF BETWEEN FR25 TO FR26.3 & BETWEEN Y867 TO Y1414 IAW A330 SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON BEAM AT FR 75 + 3, S35L, Y793. REPLACED LONGERON BEAM AT FR 75 + 3", S35L, Y793 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252LG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252LG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR18 + 14 INCHES TO FR19 + 11 INCHES, S26R, -Y450. REPAIRED SEAT TRACK BETWEEN FR18 + 14 INCHES TO FR19 + 11 INCHES, S26R, -Y450 IAW A330 SRM 53-00-15.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252QG BETWEEN FR51 TO FR53.2 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252QG BETWEEN FR51 TO FR53.2 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR57.3 + 12 INCHES TO 58 + 8 INCHES, -Y2462. REPAIRED SEAT TRACK BETWEEN FR57.3 + 12 INCHES TO 58 + 8 INCHES, -Y2462 IAW A330 SRM 53-00-15.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 252WG BETWEEN FR53.2 TO FR53.4 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252WG BETWEEN FR53.2 TO FR53.4 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR39.2 + 6 INCHES, Y450. REPLACED SEAT TRACK AT FR39.2 + 6 INCHES, Y450 IAW A330 SRM 53-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252YF BETWEEN FR40 TO FR42 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252YF BETWEEN FR40 TO FR42 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251ZF BETWEEN FR40 TO FR42 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251ZF BETWEEN FR40 TO FR42 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON AFT CARGO FLOOR PANEL 151LF BETWEEN FR57.4 TO FR58 & BETWEEN -Y867 TO -Y1414. REPAIRED AFT CARGO FLOOR PANEL 151LF BETWEEN FR57.4 TO FR58 & BETWEEN -Y867 TO -Y1414 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231UF BETWEEN FR25 TO FR26.1 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 231UF BETWEEN FR25 TO FR26.1 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231WF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 231WF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 151KF BETWEEN FR57.3 TO FR57.4 & BETWEEN -Y867 TO -Y1414. REPAIRED FLOOR PANEL 151KF BETWEEN FR57.3 TO FR57.4 & BETWEEN -Y867 TO -Y1414 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON BEAM AT FR 75 + 1, S26, Y=0, Z= 0. REPLACED LONGERON BEAM AT FR 75 + 1, S26, Y=0, Z= 0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251SF BETWEEN FR39.2 TO FR40 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 251SF BETWEEN FR39.2 TO FR40 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251FG BETWEEN FR42 TO FR47 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 251FG BETWEEN FR42 TO FR47 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252BF BETWEEN FR37 TO FR37.4 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 252BF BETWEEN FR37 TO FR37.4 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252KF BETWEEN FR37.4 TO FR39 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 252KF BETWEEN FR37.4 TO FR39 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 11, S26, Y=0. REPLACED SEAT TRACK AT FR 11, S26, Y=0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 211DF BETWEEN FR4 TO FR7 & BETWEEN Y533 TO Y952. REPAIRED FLOOR PANEL 211DF BETWEEN FR4 TO FR7 & BETWEEN Y533 TO Y952 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - CRACK ON CARGO FLOOR PANEL 151VH BETWEEN FR57.2 TO FR57.3 & BETWEEN Y867 TO Y1414. REPAIRED FLOOR PANEL 151VH BETWEEN FR57.2 TO FR57.3 & BETWEEN Y867 TO Y1414 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 39.1 + 11.5, +Y450, Z=0. REPLACED SEAT TRACK AT FR 39.1 + 11.5, +Y450, Z=0. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 212HF BETWEEN FR7 TO FR10 & BETWEEN -Y350 TO -Y1290. REPAIRED FLOOR PANEL 212HF BETWEEN FR7 TO FR10 & BETWEEN -Y350 TO -Y1290 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 39.2 + 3, +Y450, Z=0. REPLACED SEAT TRACK AT FR 39.2 + 3, +Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 212BF BETWEEN FR1 TO FR5, -Y450. REPAIRED FLOOR PANEL 212BF BETWEEN FR1 TO FR5, -Y450 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 38 + 3, +Y450, Z=0. REPLACED SEAT TRACK AT FR 38 + 3, +Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 211GF AT FR9, Y900. REPAIRED FLOOR PANEL 211GF AT FR9, Y900 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 39 + 15, +Y450, Z=0. REPLACED SEAT TRACK AT FR 39 + 15, +Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON BEAM AT FR 74 - FR 76, -Y1143. REPLACED BEAM AT FR 74 - FR 76, -Y1143 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - NR 6317140 - DELAMINATION ON FLOOR PANEL 251TF BETWEEN FR39.2 TO FR40 & BETWEEN Y953 TO 1456. REPAIRED FLOOR PANEL 251TF BETWEEN FR39.2 TO FR40 & BETWEEN Y953 TO 1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 46, -Y450, Z=0. REPLACED SEAT TRACK AT FR 46, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251AG BETWEEN FR40 TO FR42 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 251AG BETWEEN FR40 TO FR42 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 252TF BETWEEN FR39.2 TO FR40 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252TF BETWEEN FR39.2 TO FR40 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251TF BETWEEN FR53.2 TO FR53.4 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251TF BETWEEN FR53.2 TO FR53.4 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251BG BETWEEN FR42 TO FR47 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251BG BETWEEN FR42 TO FR47 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 44 + 6, -Y450, Z=0. REPLACED SEAT TRACK AT FR 44 + 6, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252RG BETWEEN FR51 TO FR53.2 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252RG BETWEEN FR51 TO FR53.2 & BETWEEN -Y1456 TO -Y1959 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251SG BETWEEN FR51 TO FR53.2 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 251SG BETWEEN FR51 TO FR53.2 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251XF BETWEEN FR40 TO FR42 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 251XF BETWEEN FR40 TO FR42 & BETWEEN Y450 TO Y953 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251KF BETWEEN FR37.4 TO FR39 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 251KF BETWEEN FR37.4 TO FR39 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 252UF BETWEEN FR39.2 TO FR40 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252UF BETWEEN FR39.2 TO FR40 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 252GF BETWEEN FR37.4 TO FR39 & BETWEEN-Y450 TO -Y953. REPAIRED FLOOR PANEL 252GF BETWEEN FR37.4 TO FR39 & BETWEEN-Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 252MF BETWEEN FR39 TO FR39.2 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 252MF BETWEEN FR39 TO FR39.2 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251GF BETWEEN FR37.4 TO FR39 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 251GF BETWEEN FR37.4 TO FR39 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR43 + 6, -Y450, Z=0. REPLACED SEAT TRACK AT FR43 + 6, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR44, -Y450, Z=0. REPLACED SEAT TRACK AT FR44, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252AG BETWEEN FR40 TO FR42 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 252AG BETWEEN FR40 TO FR42 & BETWEEN -Y1959 TO -Y2462 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBOND ON FLOOR PANEL 251MF BETWEEN FR39 TO FR39.2 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 251MF BETWEEN FR39 TO FR39.2 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 42 + 12, -Y450, Z=0. REPLACED SEAT TRACK AT FR 42 + 12, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252HF BETWEEN FR37.4 TO FR39 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252HF BETWEEN FR37.4 TO FR39 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251WF BETWEEN FR40 TO FR42 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251WF BETWEEN FR40 TO FR42 & BETWEEN Y450 TO -Y450 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DEBONDED ON FLOOR PANEL 251JF BETWEEN FR37.4 TO FR39 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251JF BETWEEN FR37.4 TO FR39 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 251LF BETWEEN FR39 TO FR39..2 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251LF BETWEEN FR39 TO FR39.2 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 252CG BETWEEN FR42 TO FR47 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 252CG BETWEEN FR42 TO FR47 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - LEVEL 2 CORROSION EXFOLIATION CORROSION ON SEAT TRACK AT FR 39.2 + 3, S26, -Y450. REPLACED SEAT TRACK AT FR 39.2 + 3, S26, -Y450.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252HF BETWEEN FR47 TO FR51 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 252HF BETWEEN FR47 TO FR51 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252QF BETWEEN FR39 TO FR39.2 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 252QF BETWEEN FR39 TO FR39.2 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR53, Y450. REPLACED SEAT TRACK AT FR53, Y450 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - LEVEL 2 CORROSION ON SEAT TRACK AT FR 48 + 15, -Y953, Z=0. REPLACED SEAT TRACK AT FR 48 + 15, -Y953, Z=0 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252LG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 252LG BETWEEN FR47 TO FR51 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251UF BETWEEN FR39.2 TO FR40 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251UF BETWEEN FR39.2 TO FR40 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251RG BETWEEN FR51 TO FR53.2 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251RG BETWEEN FR51 TO FR53.2 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252ZF BETWEEN FR40 TO FR42 & BETWEEN -Y1467 TO -Y1959. REPAIRED FLOOR PANEL 252ZF BETWEEN FR40 TO FR42 & BETWEEN -Y1467 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252XF BETWEEN FR40 TO FR42 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 252XF BETWEEN FR40 TO FR42 & BETWEEN -Y450 TO -Y953 IAW MCGILL IMR 9701 REV 'G'.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251NG BETWEEN FR51 TO FR53.2 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251NG BETWEEN FR51 TO FR53.2 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252DG BETWEEN FR42 TO FR47 & BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 252DG BETWEEN FR42 TO FR47 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 49, -Y953, S26R, Z=0. REPLACED SEAT TRACK AT FR 49, -Y953, S26R, Z=0. IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 45, -Y450, Z=0. REPLACED SEAT TRACK AT FR 45, -Y450, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON FALSE TRACK AT FR 17, S26R, -Y1456, Z=0. REPLACED FALSE TRACK AT FR 17, S26R, -Y1456, Z=0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON RIGHT PROFILE BETWEEN FR75 + 20 INCHES TO FR76, -Y3250. REPLACED RIGHT PROFILE BETWEEN FR75 + 20 INCHES TO FR76, -Y3250 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - CORROSION ON SEAT TRACK AT FR 37.2 +3 AND FR 37.3, -Y1959, Z=0. REPLACED SEAT TRACK BETWEEN FR 37.2 +3 AND FR 37.3, -Y1959, Z=0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 37.1 + 6, -Y1959, Z=0. REPLACED SEAT TRACK AT FR 37.1 + 6", -Y1959, Z=0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 33, S26R, -Y1456, Z=0. REPAIRED SEAT TRACK AT FR 33, S26R, -Y1456, Z=0 IAW A330 53-00-15. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251AF BETWEEN FR37 TO FR37.4 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251AF BETWEEN FR37 TO FR37.4 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - FLOOR PANEL 242UF IS DELAMINATED & HAS 26 CORRODED INSERTS BETWEEN FR33 TO FR35 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 242UF IAW EA 140238.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 241BF BETWEEN FR30 TO FR33 & BETWEEN Y450 TO Y953. REPAIRED FLOOR PANEL 241BF BETWEEN FR30 TO FR33 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR STRAP AT FR80 & BETWEEN -Y450 TO Y450. REPLACED FLOOR STRAP AT FR80 & BETWEEN -Y450 TO Y450 IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251AF BETWEEN FR37 TO FR37.4 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251AF BETWEEN FR37 TO FR37.4 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 37.2, S26R, -Y953, Z=0. REPLACED SEAT TRACK AT FR 37.2, S26R, -Y953, Z=0 IAW A330 SRM 51-44-11 & 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 251EF BETWEEN FR37 TO FR37.4 & BETWEEN Y1959 TO -Y2462. REPAIRED FLOOR PANEL 251EF BETWEEN FR37 TO FR37.4 & BETWEEN Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 2231XF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y953 TO Y1459. REPAIRED FLOOR PANEL 2231XF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y953 TO Y1459 IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT AT FR78 + 1 INCH, Y=0. REPLACED FLOOR SUPPORT AT FR78 + 1 INCH, Y=0 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 222JF AT FR15, -Y550. REPAIRED FLOOR PANEL 222JF AT FR15, -Y550 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - 11 AREAS OF CORROSION ON SEAT TRACK BETWEEN FR 56 + 1 AND FR 58, +Y450, Z=0. REPLACED SEAT TRACK BETWEEN FR 56 + 1 AND FR 58, +Y450, Z=0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - CORROSION ON SEAT TRACK AT FR 53.8 + 15, +Y1552.5, Z=0. REPLACED SEAT TRACK AT FR 53.8 + 15, +Y1552.5, Z=0 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 232ZF AT STA 1817, -Y2462. REPAIRED COMPOSITE DAMAGE ON FLOOR PANEL 232ZF AT STA 1817, -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 232YF AT STA 1817, -Y1456. REPAIRED COMPOSITE DAMAGE ON FLOOR PANEL 232YF AT STA 1817, -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231YF AT FR26.2, Y1959. REPAIRED ON FLOOR PANEL 231YF AT FR26.2, Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - 9 AREAS OF CORROSION ON SEAT TRACK BETWEEN FR 61 + 9 AND FR 66 + 11 +Y953, Z=0. REPLACED SEAT TRACK BETWEEN FR 61 + 9 AND FR 66 + 11, +Y953, Z=0 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 232RF AT STA 1711, -Y450. REPAIRED COMPOSITE DAMAGE ON FLOOR PANEL 232RF AT STA 1711, -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 241FF BETWEEN FR33 TO FR37 & BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL 241FF BETWEEN FR33 TO FR37 & BETWEEN Y450 TO -Y450 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231AG BETWEEN FR26.4 TO FR31 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 231AG BETWEEN FR26.4 TO FR31 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 252SF BETWEEN FR39.2 TO FR40 & BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 252SF BETWEEN FR39.2 TO FR40 & BETWEEN -Y450 TO -Y953 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDED ON FLOOR PANEL 251FF BETWEEN FR37.4 TO FR39 & BETWEEN Y450 TO -Y450. REPAIRED FLOOR PANEL 251FF BETWEEN FR37.4 TO FR39 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 232WF AT STA 1817, -Y450. REPAIRED COMPOSITE DAMAGE ON FLOOR PANEL 232WF AT STA 1817, -Y450 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR70 + 11 INCHES, -Y1959. REPAIRED SEAT TRACK AT FR70 + 11 INCHES, -Y1959 IAW A320 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR63 TO FR61, -Y1959. REPAIRED SEAT TRACK BETWEEN FR63 TO FR61, -Y1959 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR67, S26R, -Y450. REPLACED SEAT TRACK AT FR67, S26R, -Y450 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262ZF BETWEEN FR57.1 TO FR58 & BETWEEN -Y1959 TO -Y2462. REPAIRED FLOOR PANEL 262ZF BETWEEN FR57.1 TO FR58 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - CORROSION ON SEAT TRACK AT FR 54 + 11, +Y450, Z= 0. REPLACED SEAT TRACK AT FR 54 + 11, +Y450, Z= 0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR62 + 16 INCHES, Y450. REPLACED SEAT TRACK AT FR62 + 16 INCHES, Y450 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK / RAIL AT FR 14 - FR 18, S26L, +Y450. REPLACED SEAT TRACK / RAIL AT FR 14 - FR 18, S26L, +Y450 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR58 TO FR60 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 262BG BETWEEN FR58 TO FR60 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON RAIL AT FR 52, S26R, -Y450. REPLACED RAIL AT FR 52, S26R, -Y450 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231MF AT FR24, Y953. REPAIRED FLOOR PANEL 231MF AT FR24, Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 231VF AT STA 1817, Y450. REPAIRED COMPOSITE DAMAGE ON FLOOR PANEL 231VF AT STA 1817, Y450 IAW A330 SRM 53-41-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 252FG BETWEEN FR44 TO FR47 & BETWEEN -Y2462 TO -Y1959. REPLACED FLOOR PANEL 252FG BETWEEN FR44 TO FR47 & BETWEEN -Y2462 TO -Y1959 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231TF BETWEEN FR25 TO FR26.1 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 231TF BETWEEN FR25 TO FR26.1 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 262WF BETWEEN FR57.1 TO FR58 & BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 262WF BETWEEN FR57.1 TO FR58 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231HF BETWEEN FR19 TO FR22 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 231HF BETWEEN FR19 TO FR22 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261ZF BETWEEN FR57.1 TO FR58 & BETWEEN Y1959 TO Y2467. REPAIRED FLOOR PANEL 261ZF BETWEEN FR57.1 TO FR58 & BETWEEN Y1959 TO Y2467 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR18 TO FR19, Y450. REPLACED SEAT TRACK BETWEEN FR18 TO FR22, Y450 IAW SRM 51-42-11 & 53-00-15 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 CHECK - 5 AREAS OF CORROSION ON SEAT TRACK BETWEEN FR 54 AND FR 59, -Y450, Z=0. REPLACED SEAT TRACK BETWEEN FR 54 AND FR 59, -Y450, Z=0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR67, S26R, -Y450. REPLACED SEAT TRACK AT FR67, S26R, -Y450 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231PF BETWEEN FR22 TO FR25 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 231PF BETWEEN FR22 TO FR25 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR55 TO FR57.1 & BETWEEN Y950 TO -Y950. REPAIRED FLOOR PANEL 261QF BETWEEN FR55 TO FR57.1 & BETWEEN Y950 TO -Y950 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 226NF BETWEEN FR56.9 TO FR55 & BETWEEN -Y1467 TO -Y1959. REPAIRED FLOOR PANEL 226NF BETWEEN FR56.9 TO FR55 & BETWEEN -Y1467 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 231NF BETWEEN FR22 TO FR25 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 231NF BETWEEN FR22 TO FR25 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR54 + 12.5, -Y450. REPLACED SEAT TRACK AT FR54 + 12.5, -Y450 IAW A330 SRM 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON LONGERON AT FR 75, -Y1450, S26R. REPLACED LONGERON AT FR 75, -Y1450, S26R IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON PROFILE AT FR 75 + 22, S26L, +Y1970, Z=0. REPLACED PROFILE AT FR 75 + 22, S26L, +Y1970, Z=0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 272QF BETWEEN FR78 TO FR80 & BETWEEN -Y457 TO -Y2462. REPAIRED FLOOR PANEL 272QF BETWEEN FR78 TO FR80 & BETWEEN -Y457 TO -Y2462 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR73 + 12 INCHES, -Y1231. REPLACED SEAT TRACK AT FR73 + 12 INCHES, -Y1231 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT LONGERON AT FR75 + 10 INCHES, S26L, Y1447. REPLACED FLOOR SUPPORT LONGERON AT FR75 + 10 INCHES, S26L, Y1447 IAW A330 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM AT FR75, -Y387. REPAIRED LONGERON BEAM AT FR75, -Y387 IAW A330 SRM 53-00-14.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CLT - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271AG BETWEEN FR71 TO FR73 & BETWEEN Y1959 TO Y2462. REPAIRED FLOOR PANEL 271AG BETWEEN FR71 TO FR73 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00 & MCGILL IRM 9701 REV G.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON BEAM AT FR 75 + 20 - FR 76, S26L, +Y1840, Z=0. REPLACED BEAM AT FR 75 + 20 - FR 76, S26L, +Y1840, Z=0 IAW A330 SRM 51-42-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271MF BETWEEN FR75 TO FR78 & BETWEEN -Y387 TO Y387. REPLACED FLOOR PANEL 271MF BETWEEN FR75 TO FR78 & BETWEEN -Y387 TO Y387 IAW MCGILL IRM 9701 REV G.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON CROSS BEAM AT FR 73, S26R, -Y793, Z=0. REPLACED CROSS BEAM AT FR 73, S26R, -Y793, Z=0 IAW A330 SRM 53-00-14. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR73 + 20 INCHES, -Y647. REPLACED FLOORBEAM AT FR73 + 20 INCHES, -Y647 IAW SRM 51-42-11 & DRAWING F53478254.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON L-4 DOOR SILL WEB AT FR73 + 13 INCHES, Y2000, S26L. REPAIRED L-4 DOOR SILL WEB AT FR73 + 13 INCHES, Y2000, S26L IAW EA 140254.

Part: SILL — CORRODED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CORROSION ON L4 DOOR SILL AT FR73 + 13 INCHES & BETWEEN Y2100 TO Y2300. REPLACED L4 DOOR SILL AT FR73 + 13 INCHES & BETWEEN Y2100 TO Y2300 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271QF BETWEEN FR78 TO FR80 & BETWEEN Y457 TO Y2462. REPAIRED FLOOR PANEL 271QF BETWEEN FR78 TO FR80 & BETWEEN Y457 TO Y2462 IAW A330 SRM 53-02-00.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON STRINGER AT FR79 + 12 INCHES, S26R. REPAIRED STRINGER AT FR79 + 12 INCHES, S26R IAW A330 SRM 53-00-13.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON AFT CABIN Z-PROFILE AT FR79 + 12 INCHES, S26L. REPLACED AFT CABIN Z-PROFILE AT FR79 + 12 INCHES, S26L IAW A330 SRM 51-42-11.

Part: ATTACH FITTING — BROKEN (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - BROKEN FLOOR SUPPORT ATTACH CLIP AT FR80, -Y1450. REPLACED FLOOR SUPPORT ATTACH CLIP AT FR80, -Y1450 IAW A330 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 79 + 18, +Y457, Z=0. REPLACED FLOOR SUPPORT AT FR 79 + 18, +Y457, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SUPPORT — CORRODED (ZONE 100 - FUSEL) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT AT FR78, S25L, Y387. REPLACED CABIN FLOOR SUPPORT AT FR78, S25L, Y387 IAW SRM 51-42-11.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 49,958 hrs · 7,650 cycles

CWF - S2 - MAJOR REPAIR - CRACK ON Y-CHORD AT FR79 + 12 INCHES, S26L. REPAIRED Y-CHORD AT FR79 + 12 INCHES, S26L IAW A330 SRM 53-00-13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,958 hrs · 7,650 cycles

CWF - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 78 + 8, S26R, -Y457, Z=0. REPLACED FLOOR SUPPORT AT FR 78 + 8, S26R, -Y457, Z=0 IAW A330 SRM 51-72-11. AFTER FURTHER REVIEW BY THE ENGINEERING DEPARTMENT IT WAS DETERMINED THAT THIS EVENT WAS CPCP RELATED AND CLASSIFIED AS A LEVEL 2 FINDING.

Part: SLIDE RAFT — OUT OF POSITION (R1 DOOR)

FCO - CREW REPORTED AS: "ON NR 1 RIGHT DOOR OPENING FOR CATERING, SLIDE PACK FELL INTO AIRCRAFT CABIN". MAINTENANCE FOUND THE PACK SLIDE BOTTLE INDICATOR ELECTRICAL CABLE DAMAGED IN TWO PLACES, AND THE DOOR ASSIST BOTTLE DISCHARGED. ADDITIONALLY, MAINTENANCE WAS UNABLE TO RE-INSTALL THE SLIDE ONTO THE DOOR. THE AIRCRAFT WAS PLACED ON MEL, MAKING THE RIGHT, NUMBER ONE ENTRY DOOR/SLIDE INOPERATIVE. MAINTENANCE REPLACED THE ESCAPE SLIDE/RAFT AND SERVICED THE DOOR ASSIST BOTTLE. ONCE COMPLETED, THE MEL FOR THE RIGHT, NUMBER ONE ENTRY DOOR/SLIDE WAS REMOVED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR)

PHL - THE L3 DOOR ASSIST PRESSURE WAS FOUND LOW. SERVICED THE L3 DOOR ASSIST BOTTLE.

Part: WIRE HARNESS — FAULTY (CABIN)

PHL - SEAT 6B, SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY WIRE HARNESS.

Part: WIRE HARNESS — FAULTY (CABIN)

PHL - SEAT 5G, SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. REMOVED AND REPLACED SEAT MOUNTED LIGHT WIRE HARNESS.

Part: GIRT BAR — LOOSE (R1 DOOR)

MAD - DOOR R1 COULD NOT ARM. GIRT BAR FOUND LOOSE ON FLOOR. GIRT BAR RE-FITTED TO SLIDE PACK. SLIDE ARM/DISARM OPERATION CHECKED SATISFACTORY.

Part: EPSU — FAILED (CABIN)

PHL - THE EPSU AT DOOR L3 FAILED THE OPERATIONAL TEST. REMOVED AND REPLACED THE EPSU AT THE L3 DOOR.

Part: HEAT EXCHANGER — CRACKED (AC BAY)

PHL - FLT 1071 - EN ROUTE PHL TO SJU. AIR RT WING LEAK OCCURRED CLIMBING THROUGH 39500 FEET. DUE TO ICING CONDITIONS EN ROUTE, THE FLIGHT CREW AND OPERATIONS DECIDED TO RETURN TO PHL. THE FLIGHT DECLARED AN EMERGENCY TO GET DOWN OUT OF ICING CONDITIONS. THE FLIGHT LANDED IN PHL WITHOUT FURTHER INCIDENT. FOUND THE RIGHT PACK PRIMARY HEAT EXCHANGER CRACKED. REMOVED AND REPLACED THE CRACKED RIGHT PACK PRIMARY HEAT EXCHANGER.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FRA - THE FLASHLIGHT AT 3L DOOR INOP. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BATTERY AT 3L DOOR.

Part: BOLT — SHEARED (R4 DOOR)

PHL - WHILE ACCOMPLISHING THE SLIDE OPERATIONAL CHECK OF THE R4 DOOR, DOOR DAMPER ASSIST BOLT SHEARED. REMOVED AND REPLACED THE R4 DOOR SHEARED DOOR DAMPER ASSIST BOLT.

Part: SLIDE — MALFUNCTIONED (R4 DOOR)

PHL - WHILE ACCOMPLISHING A SLIDE OPERATIONAL CHECK, THE R4 SLIDE DID NOT INFLATE PROPERLY. INSTALLED NEW SERVICEABLE SLIDE ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN)

PHL - BATTERY NUMBER TWO FAILED CHECK. REPLACED ASPSU BATTERY NUMBER TWO.

Part: BRAKE ASSY — LEAKING (NR 4)

BFM - FLT 9244 EN ROUTE BFM TO PHL. AFTER TAKEOFF, A STRONG ODOR ENTERED THE COCKPIT RESULTING IN THE BURNING SENSATION OF THE CREW'S EYES. THE CREW DONNED THEIR OXYGEN MASKS AND RETURNED TO FIELD BFM WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A LEAKING NUMBER FOUR BRAKE ASSEMBLY, AND SERVICED A DEPLETED BLUE HYDRAULIC SYSTEM.

Part: HYDRAULIC SYSTEM — LEAKING (MLG)

ACFT DEPARTED, BUT PROMPTLY RETURNED. PILOT DISCREPANCY STATES; CLIMBING OUT OF 5000 FT, OUT EYES BEGAN TO BURN AND STING, AND A STRONG ODOR FILLED THE COCKPIT. PROBABLE CAUSE RELATES TO HYD LEAK ON RT MLG ASSY. PATHWAY FOR INGESTION INTO AIR CONDITIONING IS BEING EVALUATED.

Part: SENSE LINE — BROKEN (P4.95)

MAN FLT 735 EN ROUTE MAN TO PHL. DURING TAKEOFF ROLL, ECAM MESSAGE 'L ENG EPR MODE FAULT' WAS GENERATED. THE FLIGHT REJECTED THE TAKEOFF AT APPROXIMATELY 100 KNOTS AND MADE A HIGH ENERGY STOP. THE REJECTED TAKEOFF RESULTED IN A BLOWN NUMBER ONE TIRE. THE AIRCRAFT REQUIRED TO BE TOWED BACK TO THE GATE. MAINTENANCE FOUND THE P4.95 SENSE LINE BROKEN AT CLAMP. MAINTENANCE REPLACED THE P4.95 SENSE LINE.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200)

CLT - THE CAPTAIN'S SIDE FLASHLIGHT, JUST FORWARD OF FLIGHT KIT STORAGE SPACE IS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT.

Part: EPSU — DISCHARGED (CABIN)

BFM - MAINTENANCE REPORTED THE EMERGENCY LIGHT EPSU 14WL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EPSU 14WL. OPERATIONAL CHECK GOOD IAW WITH MM 33-51-38.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 36,775 hrs · 5,859 cycles

BFM - EEL - C2 CHECK - EMERGENCY LIGHT POWER SUPPLY UNIT 14WL INOPERATIVE. REPLACED AND OPERATIONAL CHECKED EMERGENCY LIGHT POWER SUPPLY UNIT 14WL IAW A330 AMM 33-51-38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,775 hrs · 5,859 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON SEAT TRACK, BS 3674 / FR 49, -Y1959. REPLACED SEAT TRACK, BS 3674 / FR 49, -Y1959 IAW A330 SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,775 hrs · 5,859 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON SEAT TRACK, BS 3727 / FR 50, -Y450. REPLACED SEAT TRACK, BS 3727 / FR 50, -Y450 IAW A330 SRM 53-31-15.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,986 hrs · 5,463 cycles

FLIGHT 718, PHL - FCO: ON CLIMBOUT, A/C TOOK A LIGHTNING STRIKE. FLIGHT RETURNED TO PHL. MAINTENANCE ACCOMPLISHED A LIGHTNING STRIKE INSPECTION, AND THE A/C WAS FERRIED TO CLT FOR FURTHER REPAIRS. CLT MAINTENANCE ACCOMPLISHED NUMEROUS BURNISHMENTS/REPAIRS TO AFFECTED AREAS OF FUSELAGE.

Part: CONTROL UNIT — FAULTY (MLG)

PHL FLT 1071 ON CLIMBOUT FROM PHL, EN ROUTE TO SJU, CREW RECEIVED ECAM L/G LGCIU 1 FAULT. CREW TRIED TO RESET FAULT ON OVERHEAD PANEL WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 LGCIU PER MM 32-31-71-000-801. PERFORMED SATISFACTORY FUNCTIONAL CHECK.