N275AY

Part: FITTING — OUT OF ADJUST (R1 GIRT BAR) · airframe 84,768 hrs · 11,991 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 DOOR SLIDE GIRT BAR DID NOT DISENGAGE FWD POSITION WITH HANDLE IN DISENGAGED POSITION DURING DISARM. FOUND R-1 DOOR FWD GIRT BAR FITTING INTERFERING WITH GIRT BAR WHEN DISARMING SLIDE; DISARM LEVER WOULD NOT TRAVEL TO FULL DISARM POSITION. ACCOMPLISHED ADJUSTMENT OF FWD FITTING IAW AMM 52-11-31 & 52-11-00. ACCOMPLISHED SLIDE REMOVAL AND REINSTALLATION IAW JOB CARD 33L00025001 AND OPS TESTS.

Part: FITTING — DISCONNECTED (R1 DOOR) · airframe 84,618 hrs · 11,964 cycles

AIRCRAFT NOT GROUNDED: DURING ETOPS PRE-DEPARTURE CHECK FOUND R1 DOOR DIFFICULT TO OPEN. FOUND QUICK RELEASE BAR DETACHED FROM DOOR ASSY. CONNECTED QUICK RELEASE FITTING TO R1 DOOR ASSY IAW AMM 25-62-41.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 84,260 hrs · 11,897 cycles

AIRCRAFT IN BASE VISIT: DOES NOT PASS TEST, PASSENGER CREW DOOR, DURING EMERGENCY LIGHT TEST COME ONESCAPE SLIDE LT SW/EPSU 2L (13WL) ON MAINTENANCE SYSTEM REPORT TEST IN PASSENGER CABIN (1 EA). REPLACED ESCAPE SLIDE OF PASSENGER CREW DOOR 2L AND PERFORMED OPERATIONAL EMERGENCY LIGHT TEST IS OK IAW AMM 25-62-41-400-801-A.

Part: ACTUATOR — NO TEST (R3 DOOR) · airframe 84,260 hrs · 11,897 cycles

AIRCRAFT IN BASE MAINTENANCE: DOOR R3 DAMPING CHECK IN PASSENGER CABIN DID NOT PASS TEST. REPLACED DOOR DAMPER (ACTUATOR) PER AMM 52-22-14-400-801-A.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 83,933 hrs · 11,856 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE PERFORMED JOB CARD 33C22033002, EPSU 2L FOUND FAULTED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-02-01.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 83,933 hrs · 11,856 cycles

AIRCRAFT NOT GROUNDED: 1L AND 2R DOOR DAMPENER ASSIST BOTTLES LOW PSI. SERVICED 1L AND 2R DOOR DAMPENER ASSIST BOTTLES IAW AMM 52-10-00.

Part: GENERATOR — FAILED (LT VACUUM) · airframe 83,662 hrs · 11,821 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ELECTRICAL ODOR IN AND AROUND LAV# L73. MAINTENANCE ACCOMPLISHED JOB CARD 33L00021001, FOUND LH VACUUM GENERATOR FAULT WITH STRONG ELEC SMELL COMES FROM IT, ALSO IT'S C/B POPPED OUT. REMOVED AND REPLACED RIGHT VACUUM GENERATOR IAW AMM 38-31-55-PAGEBLOCK 401.

Part: FITTING — INOPERATIVE (EVAC SLIDE) · airframe 81,189 hrs · 11,494 cycles

AIRCRAFT WAS GROUNDED: INOPERABLE DOOR FITTING ASSEMBLY, ESCAPE SLIDE, AT FORWARD GALLEY AREA. MAINTENANCE REPLACED DOOR FITTING ASSEMBLY ESCAPE SLIDE PER AMM 52-11-31-400-801-A STEP 4D, AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 52-11-31-400-801-A STEP 4D AND AMM 30-46-00-710-801-A.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 81,189 hrs · 11,494 cycles

SEAT 7A EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGECY EXIT LIGHT HARNNESS (1EA) ON PASSENGER SEAT 7A IN PASSENGER CABIN IAW DWG F923-93044 AND PERFORMED OPERATIONALTEST OF THE CABIN EMERGENCY LIGHTS IAW AMM 33-51-11-400-801-A STEP 4.F.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 81,023 hrs · 11,467 cycles

EMERGENCY FLASHLIGHT BY THE L1 DOOR, BATTERY WAS LOW. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW STANDARD PRACTICES. PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 81,029 hrs · 11,468 cycles

EMERGENCY FLASHLIGHT BY THE L1 DOOR, BATTERY WAS LOW. REPLACED THE FLASHLIGHT BATTERY.

Part: COMPUTER — MALFUNCTIONED · airframe 80,437 hrs · 11,377 cycles

5000 FT MSL, AUTOPILOT 2, ON, AIRCRAFT YAWED LEFT UNCOMMANDED, ALL ENGINES NORMAL. NO ECAM INDICATION. RUDDER TRIM INDICATED R 6.8. PFD TURN COORDINATOR, BAR RIGHT OF CENTER. FIRST OFFICER DISC. AP 2, MANUALLY SELETED RUDDER TRIM RESET BUTTON. AP 2 RESELECTED BACK ON. ALL SYSTEMS NORMAL. ACCOMPLISHED A DVI OF RUDDER MECHANICAL, CONTROL, RUDDER CENTERLINE & RUDDER TRAVEL LIMIT CHECKS AND REPLACED FMGEC NR 2 IAW TSI 0080111, 0080105, & 0080109. ALL CHECKED SATISFACTORY. THE TEAR DOWN REPORT FOR THE REMOVED FMGEC REFELCTS THE UNIT WAS INSPECTED AND TESTED WITH NO FAULTS NOTED, AND THE UNIT WAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (RUDDER INPUT) · airframe 80,136 hrs · 11,333 cycles

DURING CLIMB OUT, AT APPROXIMATELY 7000 FT HAD AN UNCOMMANDED 6.0 DEGREE LEFT RUDDER INPUT. DISCONNECTED THE NR 2 AUTOPILOT AND MANUALLY RESET THE RUDDER TRIM TO ZERO. USED THE NR 1 AUTOPILOT FOR THE REMAINDER OF THE FLIGHT. NO FAULTS FOUND DURING AFS TEST AND EFCS TEST. NO 30 DAY HISTORY. PERFORMED A SATISFACTORY LAND CAT 3 CAPABILITY TEST IAW JC 33T21022001. LMP STATUS REMAINS CAT 3 DUAL. OK TO CONTINUE. NO SPECIFIC PART WAS IDENTIFIED AS CAUSING THE DIFFICULTY BY MAINTENANCE DURING THE AFS AND EFCS TESTS.

Part: ADIRU — FAULTY · airframe 79,402 hrs · 11,243 cycles

1.5 HOURS INTO FLIGHT, AT FL350, RECEIVED A MESSAGE FOR NAV ADR 2 & 3 FAULT. RECEIVED AN AUTO FLT AP OFF /AUTO FLT, A/THR OFF / F/CTL ALTN LAW. DECLARED AN EMERGENCY, RETURNED TO DEPARTURE, AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED AIR DATA INERTIAL REFERENCE UNIT NR 2 AND 3 IAW AMM 34-12-34. OPS CHECKED GOOD. PERFORMED AN OPS TEST IAW AMM 34-10-00-860-801-A, 34-10-00-860-802-A, AND 34-10-00860-803-A. TESTED GOOD. RECEIVED AN IR3 FAULT FOR REMAINDER OF FLIGHT, NO F/D, NO AUTO PILOT, NO AUTO THRUST. PERFORMED CAT III CAPABILITY TEST.

Part: ADIRU — FAULTED · airframe 79,395 hrs · 11,242 cycles

1.5 HOURS INTO FLIGHT, AT FL350, RECEIVED A MESSAGE FOR NAV ADR 2 & 3 FAULT. RECEIVED AN AUTO FLT AP OFF /AUTO FLT, A/THR OFF / F/CTL ALTN LAW. FLIGHT DECLARED AN EMERGENCY, RETURNED TO DEPARTURE, AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED AIR DATA INERTIAL REFERENCE UNIT NR 2 AND 3 IAW AMM 34-12-34. OPS CHECKED GOOD. ALSO PERFORMED AN OPS TESTED IAW AMM 34-10-00-860-801-A, 34-10-00-860-802-A, AND 34-10-00860-803-A. ALL TESTED GOOD.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 79,279 hrs · 11,228 cycles

FIRST OFFICER`S SLIDING WINDOW HAS BURN MARK ON THE AFT LOWER PART OF WINDOW. FOUND TWO CRACKS IN THE BURN AREA. THE AIRCRAFT WAS GROUNDED. MAINTENANCE R & R THE SLIDING WINDOW IAW AMM 56-12-11-000-802-A,, & 56-12-11-400-802-A. OPS & LEAK CHECKED OK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 78,162 hrs · 11,093 cycles

THE FLASHLIGHT AT THE L3 DOOR WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-65-00. OPERATIONS TESTED GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 78,086 hrs · 11,084 cycles

CABIN FLOOR PANEL 251DG WAS SOFT. REPAIRED THE FLOOR PANEL IAW EA 281601. AIRCRAFT WAS GROUNDED

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 77,767 hrs · 11,044 cycles

WHILE PERFORMING JOB CARD 33C80052002, SERVICED FOUND R3 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED THE BOTTLE AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 77,236 hrs · 10,968 cycles

R3 CEILING EXIT SIGN BROKEN. REPAIRED THE SIGN IAW AMM 25-20-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 76,992 hrs · 10,931 cycles

EMERGENCY POWER SUPPLY UNIT BATTERIES AT 11WL AND 17WL FAILED CAPACITANCE BITE CHECK. REPLACED THE BATTERY PACKS IAW AMM 33-51-38. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. INOPERATIVE EMERGENCY POWER SUPPLY UNITS , 12WL, 16WL AND 18WL IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNITS 12WL, 16WL AND 18WL IN PASSENGER CABIN PER A330 AMM 33-51-38-000-801-A AND AMM 33-51-38-400-801-A. (SEE AALA201712289023 AND AALA201712289013 FOR ADDITIONAL POWER SUPPLY UNIT INFORMATION)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. INOPERATIVE EMERGENCY POWER SUPPLY UNIT 16WL IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 16WL IN PASSENGER CABIN PER AMM 33-51-38-000-801-A AND A330 AMM 33-51-38-400-801-A. (SEE AALA201712289013 AND AALA201712289024 FOR ADDITIONAL POWER SUPPLY UNIT INFORMATION)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. INOPERATIVE EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN PER AMM 33-51-38-000-801-A AND AMM 33-51-38-400-801-A. (SEE AALA201712289023 AND AALA201712289024 FOR ADDITIONAL POWER SUPPLY UNIT INFORMATION)

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 28R ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 8L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 16L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 21L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 25L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 11L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 19L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,046 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 28L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 13L ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 8R ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 11R ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER SEAT 31R ELECTRICAL CONNECTOR BACKSHELL FOR EMERGENCY LIGHTS BROKEN. REPLACED CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-803-A.

Part: DAMPER — DEFECTIVE (L3 DOOR) · airframe 76,064 hrs · 10,777 cycles

EMERGENCY EXIT DOOR DAMPER DAMPENING EFFECT DOES NOT OCCUR. REPLACED THE L3 DOOR DAMPER IAW AMM 52-22-14-400-801-A

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FLOOR PANEL 271LF. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231EG IN PASSENGER CABIN. REPLACED FLOOR PANEL 231EG IN PASSENGER CABIN PER NCN 5192292.

Part: SUPPORT ANGLE — CRACKED (FRAME 39) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT SIDE LOWER FUSELAGE BELLY FAIRING ANGLE SUPPORT STRUCTURE AT FR 39.1 (1 EACH). REPLACED ANGLE SUPPORT STRUCTURE PER SRM A330 51-72-11-911-001.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR PANEL 272LF AT AFT GALLEY AREA. REPLACED FLOOR PANEL 272LF PER AMM 53-00-00-400-801-A.

Part: LENS — CRACKED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS GROUNDED. CRACK GALLEY LENS EMERGENCY IN PASSENGER CABIN (2 EA). REPLACED GALLEY EMERGENCY LENS.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED TOP LAYER FLOOR PANEL 272AG IN PASSENGER CABIN. REPLACED FLOOR PANEL 272AG PER SRM 53-02-00-300-009 FIG 10109 AND IRM 9701 REV G.

Part: FLOORBEAM — CRACKED (FRAME 82) · airframe 76,064 hrs · 10,777 cycles

CRACK ON AFT GALLEY FLOORBEAM ANGLE AT Y1447.8 AND FRAME 82. REPLACED FLOORBEAM ANGLE IAW SRM 51-72-11, AND DRAWING F53478226200.

Part: FITTING — CRACKED (FRAME 73) · airframe 76,064 hrs · 10,777 cycles

CRACK ON FITTING LOCATED ON FRAME 73 PLUS 12 INCHES AT -Y2462. REPLACED THE FITTING IAW SRM 51-72-11 AND DRAWING F53479335.

Part: WEB — CRACKED (FRAMES 79-80) · airframe 76,064 hrs · 10,777 cycles

CRACKED FLOOR SUPPORT UPPER WEB AT Y1450.8, BETWEEN FRAMES 79 AND 80. REPLACED THE WEB IAW SRM A330 51-72-11, AND DRAWING F53479750.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261JF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-30-009 FIG 20109 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 271FF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 272BF BETWEEN FR 71 TO FR 72 AT RIGHT BUTTLINE -Y794.3 TO RIGHT BUTTLINE -Y450. REPLACED FLOOR PANEL 272BF BETWEEN FR 71 TO FR 72 AT RIGHT BUTTLINE -Y794.3 TO RIGHT BUTTLINE -Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 261LF BETWEEN FRAME 53.9 AND FRAME 55, Y450 TO Y953. REMOVED AND REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM A330 53-20-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — CORRODED (FWD GALLEY) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY HEATED FLOOR PANEL 221GF INCLUDING TOP PLY BETWEEN FRAME 14 AND FRAME 17. REMOVED AND REPLACED FLOOR PANEL INCLUDING TOP PLY PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 241RF TOP LAYER, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIG 20109, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FLOOR PANEL 251RF TOP LAYER IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIG 20109 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 252KG BETWEEN FRAME 47 AND FRAME 51, -Y1456 TO Y-953. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 232BG BETWEEN FR 26.4 TO FR 31 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y540. REPLACED FLOOR PANEL 232BG BETWEEN FR 26.4 TO FR 31 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y540. PER IRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 232NF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — CORRODED (AFT GALLEY) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOOR PANEL 272LF INCLUDING TOP PLY BETWEEN FRAMES 74 AND 76. REMOVED AND REPLACED FLOOR PANEL INCLUDING TOP PLY PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — CORRODED (AFT GALLEY) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOOR PANEL 271LF, INCLUDING TOP PLAY, BETWEEN FR 74 AND FR 76. REPLACED FLOOR PANEL 271LF PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 232BF BETWEEN FRAME 15 AND FRAME 19, -Y450 TO -Y953. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 252VF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 271BF IN PASSENGER CABIN. REPLACED FLOOR PANEL IN PASSENGER CABIN PER SRM 53-02-00-300-009 PARAGRAPH 2 A FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 242GF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 262BH BETWEEN FR 57.1 TO FR 58 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 262BH BETWEEN FR 57.1 TO FR 58 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261EG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261WG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 232DF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 251LF BETWEEN FRAME 39 AND FRAME 39.2, -Y450 TO Y450. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231DG BETWEEN FR 26.4 TO FR 31 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y1456. REPLACED FLOOR PANEL 231DG BETWEEN FR 26.4 TO FR 31 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y1456 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 232FF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y450. REPLACED FLOOR PANEL 232FF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y450 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND THE ON TOP LAYER OF FLOOR PANEL 232WF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 232DG BETWEEN FR 26.4 TO FR 31 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 232DG BETWEEN FR 26.4 TO FR 31 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION OF FLOOR PANEL 252HF BETWEEN FR 37 TO FR 39 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 252HF BETWEEN FR 37 TO FR 39 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-0-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 231AG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENENACE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 262ZG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 221BF IN PASSENGER CABIN. REPLACED FLOOR PANEL IN PASSENGER CABIN PER SRM 53-02-00-300-009 PARAGRAPH 2 A FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 232F BETWEEN FR 26.1 AND FR 26.4 AT RIGHT BUTTLINE -Y2462 AND RIGHT BUTTLINE -Y1959. REPLACED FLOOR PANEL 232F BETWEEN FR 26.1 AND FR 26.4 AT RIGHT BUTTLINE -Y2462 AND RIGHT BUTTLINE -Y1959 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 73-75) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED TOP LAYER OF THE FLOOR PANEL 272GF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-300-009, PARAGRAPH 2.A, FIGURE 20109,

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 222DF BETWEEN FR 11 AND FR 14 AT RIGHT BUTTLINE -Y2462 AND RIGHT BUTTLINE -Y450. REPLACED FLOOR PANEL 222DF BETWEEN FR 11 AND FR 14 AT RIGHT BUTTLINE -Y2462 AND RIGHT BUTTLINE -Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION OF FLOOR PANEL 252UF BETWEEN FR 39.2 TO FR 40 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -Y1659. REPLACED FLOOR PANEL 252UF BETWEEN FR 39.2 TO FR 40 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -Y1659 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 231AF BETWEEN FRAME 15A AND FRAME 19, -Y450 TO Y450. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 231TF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (FRAMES 71-73) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 271AG AT FRAMES 71 TO 73 FROM Y1456 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 242HF AT FRAMES 33 TO 37, -Y953 TO -Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON FLOORBEAM LONGITUDINAL LOWER SURFACE ON FR 74, Y1451.8 AT AFT GALLEY AREA. REPAIRED FLOORBEAM PER SRM 53-00-14-300-002.

Part: FLOOR PANEL — DELAMINATED (FRAMES 19-22) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 232GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 262SG BETWEEN FRAME 65 AND FRAME 69, -Y1456 TO -Y953. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 262QC BETWEEN FR 62 AND FR 65 AT RIGHT BUTTLINE Y-2462 TO RIGHT BUTTLINE Y-1959. REPLACED FLOOR PANEL 262QC BETWEEN FR 62 AND FR 65 AT RIGHT BUTTLINE Y-2462 TO RIGHT BUTTLINE Y-1959 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261DH BETWEEN FR 60 TO FR 62 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 261DH BETWEEN FR 60 TO FR 62 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 221CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 232UF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 231VF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231BG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 272AG, FRAMES 71 TO 73, -Y2462 TO -Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 262XG BETWEEN FR 69 TO FR 71 AT RIGHT BUTTLINE -Y953 TO -Y450. REPLACED FLOOR PANEL 262XG BETWEEN FR 69 TO FR 71 AT RIGHT BUTTLINE -Y953 TO -Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAME 53) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION OF FLOOR PANEL 261HF BETWEEN FR 53.6 TO FR 53.9 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE 1456. REPLACE FLOOR PANEL 261HF BETWEEN FR 53.6 TO FR 53.9 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE 1456 PER A330 SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 232HF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED AREA ON FLOOR PANEL 242TF IN PASSENGER CABIN BETWEEN FR 33 TO FR 35 AT STRINGER 25 BETWEEN RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959. REPLACE FLOOR PANEL 242TF IN PASSENGER CABIN BETWEEN FR 33 TO FR 35 AT STRINGER 25 BETWEEN RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959 PER AMM 25-27-51-400-801-A.

Part: FLOOR PANEL — DELAMINATED · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TO FLOOR PANEL 261XG BETWEEN FR 69 TO FR 71 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y794.3. REPLACED FLOOR PANEL 261XG BETWEEN FR 69 TO FR 71 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y794.3 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 232JF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y2462. REPLACED FLOOR PANEL 232JF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y2462 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 231MF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 78-80) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 271PF AT FRAMES 78 TO 80, -Y450 TO Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 19-22) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION ON FLOOR PANEL 231HF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 71-73) · airframe 76,064 hrs · 10,777 cycles

DELAMINTATED FLOOR PANEL 271AF AT FRAMES 71 TO 73, Y450 TO -Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 262FH BETWEEN FR 62 TO FR 65 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y959. REPLACED FLOOR PANEL 262FH BETWEEN FR 62 TO FR 65 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y959 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261QG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIG 20109 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER FLOOR PANEL 221AF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 232XF BETWEEN FR 26.1 AND 26.4 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -Y953. REPLACED FLOOR PANEL 232XF BETWEEN FR 26.1 AND 26.4 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -Y953 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 232YF BETWEEN FR 26.1 AND FR 26.4 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 232YF BETWEEN FR 26.1 AND FR 26.4 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 73-76) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION ON THE FLOOR PANEL 271HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251S BETWEEN FR 51 AND FR 53.2 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462. REPLACED FLOOR PANEL 251S BETWEEN FR 51 AND FR 53.2 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 19-22) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION ON FLOOR PANEL 231FF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 272HF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 232CG IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231EF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 231EF BETWEEN FR 19 TO FR 22 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 261UG BETWEEN FR 65 TO FR 69 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462. REPLACED FLOOR PANEL 261UG BETWEEN FR 65 TO FR 69 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231CF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 231CG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251SF BETWEEN FR 39.2 AND FR 40 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 251SF BETWEEN FR 39.2 AND FR 40 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y953 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 232TF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231BF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIG 20109.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 231GF. REPLACED FLOOR PANEL PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 231Q. REPLACED FLOOR PANEL PER SRM 53-02-00-300-004 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 232EG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 221EF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 151EG BETWEEN FR 42 TO FR 47 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 151EG BETWEEN FR 42 TO FR 47 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL BETWEEN FR 22 AND FR 25 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL BETWEEN FR 22 AND FR 25 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 232MF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION OF FLOOR PANEL 262TG BETWEEN FR 65 TO FR 69 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y1858.4. REPLACED FLOOR PANEL 262TG BETWEEN FR 65 TO FR 69 AT RIGHT BUTTLINE -Y953 TO RIGHT BUTTLINE -Y1858.4 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 75-78) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 271MF, FRAMES 75 TO 78 RBL 450 TO LBL 450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 271GF BETWEEN FRAMES 73 AND 76, Y450 TO Y794.3. REMOVED AND REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM A330 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251DG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-00-009 PAR 2A(2).

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 231SF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 231WF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER OF FLOOR PANEL 271NF IN PASSENGER CABIN BETWEEN FRAMES 75 TO 78. REPLACED THE FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENENACE. DELAMINATION ON TOP LAYER FLOOR PANEL 231JF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — CORRODED (AFT GALLEY) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT SIDE AFT GALLEY FLOOR PANEL 271KF. REPLACED FLOOR PANEL 271KF PER AMM 25-27-51-400-801-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251VF BETWEEN FR 39.2 TO FR 40 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462. REPLACED FLOOR PANEL 251VF BETWEEN FR 39.2 TO FR 40 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 231KF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37.4-39) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 251HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251UF BETWEEN FR 39.2 AND FR 40 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 251UF BETWEEN FR 39.2 AND FR 40 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED OF FLOOR PANEL 241SF, FRAMES 33 TO 37, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 241GF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED TOP LAYER ON PASSENGER CABIN FLOOR PANEL 242RF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL252VG BETWEEN FR 53.2 TO FR 53.4 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456. REPLACED FLOOR PANEL252VG BETWEEN FR 53.2 TO FR 53.4 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456 PER IRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED STRUCTURE FLOORBEAM AT AFT GALLEY AREA. REPLACED FLOORBEAM AT AFT GALLEY PER SRM 51-72-11 AND DRAWING F53478222.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 252EF BETWEEN FR 37 TO FR 37.4 AT RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959. REPLACED FLOOR PANEL 252EF BETWEEN FR 37 TO FR 37.4 AT RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: STIFFENER — CRACKED (FRAME 12) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FR 12 AT RIGHT STRINGER 26. REPLACED PER JOB CARD 5315U155-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261CF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM Y2462, FR73+4" OF UPPER AND LOWER SURFACE AT AFT GALLEY AREA. REPLACED FLOORBEAM PER 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 242EF IN PASSENGER CABIN. REPLACED FLOOR PANEL IN PASSENGER CABIN PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 261PF BETWEEN FR 53.9 TO FR 55 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE 2462. REPLACED FLOOR PANEL 261PF BETWEEN FR 53.9 TO FR 55 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE 2462 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 261BH BETWEEN FR 57.1 TO FR 58 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 261BH BETWEEN FR 57.1 TO FR 58 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER PASSENGER CABIN FLOOR PANEL 251NF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261QF BETWEEN FR 55 TO FR 57.7 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 261QF BETWEEN FR 55 TO FR 57.7 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 30-33) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED FLOOR PANEL 242BF, FRAMES 30 TO 33, -Y450 TO -Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 252PF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 PAR 2.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 241FF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 242CF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251MF BETWEEN FR 39 TO FR 39.2 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 251MF BETWEEN FR 39 TO FR 39.2 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENENACE. DELAMINATION FOUND ON TOP LAYER FLOOR PANEL 251EF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 241AF BETWEEN FRAME 30 AND FRAME 33, -Y450 TO Y450. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 241BF BETWEEN FR 30 TO FR 33 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 241BF BETWEEN FR 30 TO FR 33 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953 PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER OF PASSENGER CABIN FLOOR PANEL 262EG BETWEEN FRAMES 58 AND 60, Y-2462 TO Y-1959. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 25-27) · airframe 76,064 hrs · 10,777 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 241EF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER PASSENGER CABIN FLOOR PANEL 252GF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

CORROSION ON THE FLOORBEAM AUXILIARY ASSEMBLY AT FRAME 73 PLUS 4 INCHES, BETWEEN Y1959 AND Y2464. REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 51-42-11, AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 252JB BETWEEN FR 37.4 AND FR 39 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 252JB BETWEEN FR 37.4 AND FR 39 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00300-009 FIG 20109 AND IRM 9701 REVISION G.

Part: STIFFENER — CRACKED (FRAME 12) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FR 12 AT STRINGER 26 LEFT. REPLACED PER JOB CARD 5315U155-001.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER OF PASSENGER CABIN FLOOR PANEL 251DF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37.4-39) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 251JF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37.4-39) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 251GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37-37.4) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 251AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER FLOOR PANEL 261AF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37-37.4) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 251BF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 252SF IN PASSENGER CABIN. REPLACED FLOOR PANEL SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 252DG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-00-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER PASSENGER CABIN FLOOR PANEL 252ZF BETWEEN FRAME 40 AND FRAME 42, -Y1456 TO -Y1959. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: WEB — CRACKED (FRAME 80) · airframe 76,064 hrs · 10,777 cycles

CRACK FOUND ON THE PASSENGER CABIN FLOOR STRUCTURE WEB AT Y1447.8, FRAME 80 PLUS 2 INCHES. REPLACED THE FLOOR WEB IAW SRM 51-72-11, 51-42-11 AND DRAWING F53479750.

Part: SEAT TRACK — CORRODED (FRAMES 74-75) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON SEAT TRACK Y1454.8 BETWEEN FR 74 TO FR 75 AT AFT GALLEY AREA. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 76,064 hrs · 10,777 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BETWEEN FRAMES 53.2 AND 54 PLUS 18 INCHES. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING F53326972.

Part: FLOOR SUPPORT — CORRODED (FRAME 75-78) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

CORROSION FOUND ON THE AFT GALLEY FLOOR SUPPORT, -Y453, BETWEEN FRAMES 75 AND 78. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, AND DRAWING F53478018.

Part: FLOORBEAM — CRACKED (FRAME 82) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT GALLEY FLOORBEAM ANGLE AT -Y1447.8, FRAME 82. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-72-11 DRAWING F53479750.

Part: WEB — CRACKED (FRAME 80) · airframe 76,064 hrs · 10,777 cycles

CRACKED FLOOR WEB -Y1447.8 AT FRAME 80 PLUS 2 INCHES. REPLACED THE FLOOR WEB IAW SRM 51-72-11, SRM 51-42-11, AND DRAWING F53479750.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK Y1451.8 BETWEEN FR 73 TO FR 74 AT AFT GALLEY A. REPLACED SEAT TRACK SRM 51-72-11-001.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED SHEAR PLATE AT FR 76 PLUS 12 INCHES IN PASSENGER CABIN. REPLACED SHEAR PLATE LOCATED AT FR 76 IN PASSENGER CABIN PER SRM 53-41-14-300-008.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT -Y450, BETWEEN FR 75 AND FR 82. REPLACED FLOORBEAM PER SRM 51-72-11 DRAWING F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

CORROSION FOUND ON AFT GALLEY FLOOR SUPPORT Y381, BETWEEN FRAMES 75 - 78. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SEAT TRACK AT STRINGER 26R AND -Y1454.8, BETWEEN FR 73 AND FR 74. REPLACED SEAT TRACK PER SRM 51-72-11, 51-42-11 AND DRAWING F53478018.

Part: SHEAR PLATE — CRACKED (FRAME 76) · airframe 76,064 hrs · 10,777 cycles

CRACK ON PASSENGER CABIN SHEAR PLATE AT Y2462 AND FRAME 76 MINUS 12 INCHES. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, 51-42-11, AND DRAWING F53479330.

Part: FLOOR PANEL — DELAMINATED (FRAMES 47-51) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 252HG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701 REVISION G, AND DRAWING F53671398.

Part: RAIL — CORRODED (FUSELAGE) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY RAIL AT STRINGER 26R, FR 17, AND -Y1959. REPLACED RAIL PER SRM 51-72-11, 51-42-11 AND DRAWING F53114410.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,064 hrs · 10,777 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY FLOOR BEAM LOCATED AT LEVEL FRAME 17, STRINGER 26R, -Y1954. REPLACED RAIL (FLOOR BEAM) PER SRM 51-72-11, SRM 51-42-11, AND DRAWING F53114410.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37-37.4) · airframe 76,064 hrs · 10,777 cycles

DELAMINATION FOUND ON FLOOR PANEL 251CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: ADIRU — FAULTY (FIRST OFFICER'S) · airframe 75,447 hrs · 10,703 cycles

AT 80 KNOTS DURING TAKEOFF, THE FIRST OFFICER`S SPEED TAPE INDICATION DISAPPREAD AND TURNED RED. REJECTED TAKE OFF AT 90 KNOTS. REPLACED ADIRU.

Part: SIGN — MISSING (CABIN) · airframe 75,096 hrs · 10,659 cycles

EXIT SIGN MISSING AT THE R1 DOOR. REPLACED THE SIGN.

Part: AIR DUCT — FROZEN (ZONE 200) · airframe 74,298 hrs · 10,559 cycles

AIRCRAFT WAS GROUNDED. AIR CONDITIONER NOT WORKING IN COCKPIT. PACK FLOW WAS RESTRICTED DUE TO ICE BUILD UP IN DUCTS. THAWED ICE. SYSTEM CHECKS NORMAL.

Part: UNKNOWN — ODOR (ENGINE) · airframe 74,145 hrs · 10,538 cycles

DIVERTED DUE TO AN ODOR IN THE VICINTY OF ROW 22 ABC, IDENTIFIED AS A BURNING RUBBER TYPE OF ODOR. CREW CHECKED, EMERGENCY DECLARED AND LANDED. MAINTENANCE ISOLATED THE ODOR TO THE LEFT ENGINE PRODUCING BURNING PLASTIC ODOR FROM THE NR 1 BLEED SYSTEM. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED 33L00021001 AND 33L00071002. NO LEAKS OR DISCREPANCIES NOTED. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: STRUT — FAULTED (RT WING FLAP) · airframe 73,905 hrs · 10,508 cycles

CREW REPORTED FLAPS LOCKED ECAM MESSAGE DURING DESCENT. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. REPLACED SENSOR STRUT TRACK 4 RIGHT WING. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 73,018 hrs · 10,360 cycles

MISSING LENS ON FLOOR LEVEL EMERGENCY LIGHT). MAINTENANCE REPLACED THE LENS IAW AMM 33-51-12.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 72,774 hrs · 10,309 cycles

DELAMINATION ON AFT CARGO FLOOR PANEL 152NW. REPLACED THE CARGO FLOOR PANEL IAW AMM 25-53-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 72,482 hrs · 10,250 cycles

L1 DOOR DAMPER ACTUATOR CYLINDER GAUGE SHOWING PRESSURE LOWER THAN 1783 PSI. SERVICED L1 DOOR DAMPER ACTUATOR CYCLINDER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 72,482 hrs · 10,250 cycles

R4 DOOR DAMPER ACTUATOR CYLINDER GAUGE SHOWING PRESSURE LOWER THAN 1783 PSI. SERVICED R4 DOOR DAMPER ACTUATOR CYLINDER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: OVEN — ODOR (GALLEY) · airframe 72,621 hrs · 10,275 cycles

FLIGHT ATTENDANTS REPORTED ODOR LIKE OVEN NR 2 OVERHEATING. NO SMOKE REPORTED. AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE OVEN 1-7 AT FORWARD GALLEY IAW AMM 25-35-19.

Part: BATTERY — FAULTED (CABIN) · airframe 72,482 hrs · 10,250 cycles

AIRCRAFT WAS NOT GROUNDED. CLASS 1 MESSAGE FOR THE EMERGENCY POWER SUPPLY UNIT 14WL BATTERY AT THE R2 DOOR. REPLACED EMERGENCY POWER SUPPLY UNIT 14WL BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00-710-801-A-01 AND 25-23-46-000-801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,754 hrs · 10,155 cycles

EMERGENCY POWER SUPPLY UNIT 13WL FAILS OPERATIONAL TEST IAW TASK CARD 33C22033002. REPLACED THE BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,754 hrs · 10,155 cycles

EMERGENCY POWER SUPPLY UNIT 15WL FAILS OPERATIONAL TEST PER TASK CARD 33C22033002. REPLACED BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 71,209 hrs · 10,089 cycles

CEILING MOUNTED EXIT SIGN CAME OFF AT L2 DOOR. REPLACED EXIT SIGN COVER IAW AMM 33-50-01.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 70,982 hrs · 10,060 cycles

L3 DOOR ASSIST BOTTLE IN GREEN BAND BUT LESS THAN 1783 PSI. SERVICED L3 DOOR ASSIST BOTTLE PER TASK CARD 33C80052002.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 70,982 hrs · 10,060 cycles

R3 DOOR ASSIST BOTTLE IN GREEN BAND BUT LESS THAN 1783 PSI. REQUIRES SERVICING. SERVICED R3 DOOR ASSIST BOTTLE PER TASK CARD 33C80052002.

Part: OVEN — OVERTEMP (GALLEY) · airframe 70,836 hrs · 10,042 cycles

OVEN OVER HEATED NEAR POSITION C-24. OVER TEMP LIGHT CAME ON, AND AN ODOR OF BURNING WIRING. CIRCUIT BREAKER PULLED. REPLACED C-24 OVEN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-35-19.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,717 hrs · 10,026 cycles

EMERGENCY LIGHT LENS COVER AT 3R INBOARD SIDEWALL MISSING. INSTALLED LENS IAW AMM 33-50-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 70,272 hrs · 9,964 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT SEAT 6A IS INOPERATIVE. REPLACED FEMALE CONNECTOR ON EMER LIGHT HARNESS AT SEAT 6A IAW CMM 25-01-75 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — FAILED (CABIN) · airframe 70,190 hrs · 9,951 cycles

AIRCRAFT WAS NOT GNDED. R1 DOOR EMER EXIT LIGHT POWER SUPPLY UNIT FAILED BATTERY TEST. REPLACED THE BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 70,190 hrs · 9,951 cycles

AIRCRAFT WAS NOT GNDED. L2 DOOR EMER EXIT LIGHT POWER SUPPLY UNIT FAILED BATTERY TEST. REPLACED THE BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 70,190 hrs · 9,951 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR EMER EXIT LIGHT POWER SUPPLY UNIT FAILED BATTERY TEST. REPLACED THE BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 69,080 hrs · 9,744 cycles

R2 DOOR FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-20-00.

Part: LIGHT — UNSECURE (CABIN) · airframe 68,997 hrs · 9,720 cycles

AIRCRAFT IN BASE MX. SEAT 7A EMER LIGHT INOPERATIVE. CONNECTED LOOSE EMER EXIT LIGHT IAW CMM 25-02-38. PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-803.

Part: LINKAGE — STICKING (R1 DOOR) · airframe 68,691 hrs · 9,656 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR INDICATES OPEN WITH DOOR CLOSED. EXERCISED DOOR SWITCH LINKAGE. DOOR SLIDE ARMED INDICATIONS NORMAL.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 68,048 hrs · 9,545 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK NEED TO BE ACCOMPLISHED. R & R ALL CABIN EMER LIGHT BATTERIES IAW AMM 33-51-38-000-802-A & AMM 33-51-38-400-802-1A. ACCOMPLISHED JC 33C20033002.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 68,048 hrs · 9,545 cycles

A10 CHECK, MCDU EMER POWER SUPPLY 14WL, FAULT MSG FOR THE 2R DOOR SLIDE LIGHT. REPLACED SLIDE IAW 33L00025001.

Part: LENS — MISSING (CABIN) · airframe 67,193 hrs · 9,424 cycles

MISSING EMER LIGHT LENS AT L74 LAVATORY. REPLACED MISSING EMER LIGHT LENS AT L74 LAVATORY, CHECKED OK.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 66,769 hrs · 9,364 cycles

FLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOWED TO THE GATE AFTER LANDING. REPLACED LT & RT EDP GREEN SYS IAW TASK 29-11-51. REPLACED GREEN ELEC PUMP IAW TASK 29-21-51. REPLACED GREEN HYD FILTERS IAW TASK 29-11-06. REPLACED GREEN CASE DRAIN FILTERS IAW TASK 29-11-43. REPLACED GREEN LOW PSI FILTER IAW TASK 29-11-44. RESET NORMAL EXTENSION SYS IAW TASK 32-00-00-860-803-A. SEE ALSO SDR'S AALA201507169009 & AALA201507169010.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 66,769 hrs · 9,364 cycles

FLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. AN EMER WAS DECLARED, & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOWED TO THE GATE AFTER LANDING. REPLACED LT & RT EDP GREEN SYS IAW TASK 29-11-51. REPLACED GREEN ELEC PUMP IAW TASK 29-21-51. REPLACED GREEN HYD FILTERS IAW TASK 29-11-06. REPLACED GREEN CASE DRAIN FILTERS IAW TASK 29-11-43. REPLACED GREEN LOW PSI FILTER IAW TASK 29-11-44. RESET NORMAL EXTENSION SYS IAW TASK 32-00-00-860-803-A. SEE ALSO SDR'S AALA201507169009 & AALA201507169010.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 66,769 hrs · 9,364 cycles

FLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. AN EMER WAS DECLARED, & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOWED TO THE GATE AFTER LANDING. REPLACED LT & RT EDP GREEN SYS IAW TASK 29-11-51. REPLACED GREEN ELEC PUMP IAW TASK 29-21-51. REPLACED GREEN HYD FILTERS IAW TASK 29-11-06. REPLACED GREEN CASE DRAIN FILTERS IAW TASK 29-11-43. REPLACED GREEN LOW PSI FILTER IAW TASK 29-11-44. RESET NORMAL EXTENSION SYS IAW TASK 32-00-00-860-803-A. SEE ALSO SDR'S AALA201507169009 & AALA201507169010.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 66,696 hrs · 9,354 cycles

FLIGHT 748 EN-ROUTE, LOST ENG 1 HYD B SYS PRESS AT FL 370. FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. PERFORMED BLEEDING OF THE BLUE HYD SYS IAW TASK 29-00-00-870-805-A. REPLACED BLUE RESERVOIR AIR PRESS SWITCH IAW TASK 29-31-11-000-802-A.

Part: CABLE — DISCONNECTED (CABIN) · airframe 65,943 hrs · 9,244 cycles

7A SEAT MOUNTED FLOOR PROX EMER LIGHT INOPERATIVE. CONNECTED THE LOOSE CABLE INSIDE THE SEAT.

Part: ACTUATOR — FAULTY (NR 1 ENGINE) · airframe 64,869 hrs · 9,041 cycles

IN CRUISE, THE NR 1 ENG COMPRESSOR STALLED. PAX REPORTED LARGE FLAME FROM NACELLE. THRUST RESTORED WITHIN 10 SECONDS. REPLACED LT ENG VSV ACTUATOR. THE INTEGRITY OF ECS TEMP CONTROL WITH ENGS RUNNING WAS ACCOMPLISHED. A BORESCOPE WAS ACCOMPLISHED ON THE LT ENG & A CHIP DETECTOR INSPECTION WAS PERFORMED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 64,770 hrs · 9,018 cycles

C2 CHECK CRACK IN FLOOR PANEL 131PF BETWEEN FRAME 26.3 TO 30 & BETWEEN Y2462 TO Y1959. REPLACED FLOOR PANEL 131PF IAW SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 64,770 hrs · 9,018 cycles

C2 CHECK CRACK IN FLOOR PANEL 131AG BETWEEN FRAME 37 TO 37.4 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 131AG IAW SRM 53-02-00 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,770 hrs · 9,018 cycles

C2 CHECK CORROSION ON SEAT TRACK BETWEEN FRAME 40 TO 47, Y2462. REPLACED SEAT TRACK BETWEEN FRAME 40 TO 47, Y2462 IAW SRM 53-31-15-101 FIG 102.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 64,770 hrs · 9,018 cycles

C2 CHECK CRACK IN FLOOR PANEL 131DG BETWEEN FRAME 37.4 TO 39.1 & BETWEEN Y953 TO Y1465. REPLACED FLOOR PANEL 131DG IAW SRM 53-02-00 FIG 211 & 53-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,770 hrs · 9,018 cycles

C2 CHECK, CORROSION ON SEAT TRACK RAIL BETWEEN FRAME 61 TO 62, -Y2462. REPLACED SEAT TRACK RAIL IAW SRM 53-41-15 FIG 101 & 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,835 hrs · 8,744 cycles

L2 DOOR FLASHLIGHT INOPERATIVE. R & R L2 DOOR FLASHLIGHT BATTERY. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,546 hrs · 8,572 cycles

R3 DOOR UPPER FLASHLIGHT LED NOT FLASHING. REPLACED R3 EMERGENCY FLASHLIGHT BATTERY, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,499 hrs · 8,566 cycles

EPSU BATTERIES FAILED AT 1L, 11WL & 2L, 13WL, FOR J/C 33C20033002. R & R EPSU BATTERIES AT 1L, 11WL & 2L, 13WL.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 60,057 hrs · 8,357 cycles

C1 CHECK CHAFFING DAMAGE ON FWD CARGO DOOR INNER SKIN AT FR 23 BETWEEN BEAM 4 TO BEAM 5. REPAIRED FWD CARGO DOOR INNER SKIN AT FR 23 BETWEEN BEAM 4 TO BEAM 5 IAW EA 505778.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 60,057 hrs · 8,357 cycles

C1 CHECK DELAMINATION ON BULK CARGO DOOR FLOOR PANEL 161AF BETWEEN FR 65 TO FR 67 & BETWEEN Y 560 TO Y 1140. REPLACED BULK CARGO DOOR FLOOR PANEL 161AF IAW SRM 53-02-00, FIG 211 & 51-42-11.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 59,737 hrs · 8,315 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING COVER. MX INSTALLED MISSING COVER.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 59,534 hrs · 8,288 cycles

R1 AND R3 EMERGENCY BATTERIES FAILED CAPACITY CHECK IAW J/C 33C2003302L. MX R & R R1 AND R3 EMERGENCY BATTERIES OPS CHECK OK.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 58,924 hrs · 8,209 cycles

L1 DOOR SLIDE OFF FORWARD HOOK. MX COMPLETED L1 DOOR ESCAPE SLIDE REPLACEMENT

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 57,524 hrs · 8,024 cycles

CUST. CARE - DOOR DAMPER AND EMERGENCY OPERATION CYLINDERS REQUIRE SERVICING ON DOOR 1L. SERVICED DOOR 1L DAMPER & EMERGENCY OPERATION CYLINDER IAW A330 AMM 52-10-00-600-802-A.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 57,524 hrs · 8,024 cycles

CUST. CARE - DOOR DAMPER AND EMERGENCY OPERATION CYLINDERS REQUIRE SERVICING ON DOOR 4L. SERVICED DOOR 4L DAMPER & EMERGENCY OPERATION CYLINDER IAW A330 AMM 52-10-00-600-802-A.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 57,524 hrs · 8,024 cycles

CUST. CARE - DOOR DAMPER AND EMERGENCY OPERATION CYLINDERS REQUIRE SERVICING ON DOOR 1R. SERVICED DOOR 1R DAMPER & EMERGENCY OPERATION CYLINDER IAW A330 AMM 52-10-00-600-802-A.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 57,524 hrs · 8,024 cycles

CUST. CARE - DOOR DAMPER AND EMERGENCY OPERATION CYLINDERS REQUIRE SERVICING ON DOOR 4R. SERVICED DOOR 4R DAMPER & EMERGENCY OPERATION CYLINDER IAW A330 AMM 52-10-00-600-802-A.

Part: BATTERY — DISCHARGED (CABIN)

ESPU 13WL FAIL BATTERY CAPACITANCE TEST. MAINTENANCE REPLACED BATTERY.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 55,215 hrs · 7,707 cycles

JUST BEFORE PUSH FLIGHT REPORTED CIDS CAUTION ALERT CHECK 4L SLIDE PRESSURE. MAINTENANCE SERVICED 4L DOOR ASSIST BOTTLE.

Part: COVER — MISSING (CABIN) · airframe 54,947 hrs · 7,671 cycles

MID GALLEY RIGHT LOWER EMERGENCY EGRESS PATH LIGHT COVER MISSING. MAINTENANCE INSTALLED EMERGENCY EGRESS PATH LIGHT COVER.

Part: SIGN — LOOSE (CABIN) · airframe 53,992 hrs · 7,550 cycles

CLT - EXIT SIGN 2R LOOSE. REPLACE 2R EMERGENCY EXIT SIGN. OPS CHECKS GOOD.

Part: COVER — MISSING (CABIN) · airframe 53,417 hrs · 7,474 cycles

EXIT LIGHT PLASTIC COVER MISSING IN GALLEY NEAR 3-17, NEXT TO TRASH BIN. MAINTENANCE REPLACED MISSING COVER LIGHT, OPS CHECKS NORMAL.

Part: COVER — MISSING (CABIN) · airframe 53,136 hrs · 7,437 cycles

EMERGENCY LIGHT COVER AT REAR GALLEY POSITION 5-16 MISSING. MAINTENANCE REPLACED MISSING EMERGENCY LIGHT COVER AT 5-16.

Part: BATTERY — DISCHARGED (CABIN)

PHL - CIDS FAULT L3 EMERGENCY LIGHTS BATTERY FAULT (15WL). REMOVED AND REPLACED 15WL EMERGENCY BATTERY. OPS CHECK NORMAL AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

PHL - CIDS FAULT 2R EMERGENCY LIGHTS BATTERY FAULT (14WL). REMOVED AND REPLACED 14WL EMERGENCY BATTERY. OPS CHECK NORMAL AT THIS TIME.

Part: ANGLE — DEFECTIVE (LT WING) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 AIRCRAFT'S, REPLACE RIB 1/FR42 OUTER ANGLES. REPLACED LEFT RIB 1 OUTER RIB ANGLE IAW EA 130520.

Part: ANGLE — DEFECTIVE (RT WING) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 AIRCRAFT'S, REPLACE RIB 1/FR42 OUTER ANGLES. REPLACED RIGHT RIB 1 OUTER RIB ANGLE IAW EA 130520.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR32 TO FR33, -Y1959. REPLACED SEAT TRACK BETWEEN FR32 TO FR33, -Y1959 IAW A330 SRM 53-00-15 FIG 101.

Part: PIN — WORN (NR 1 PYLON) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - THREADS WORN ON NR 1 ENGINE PYLON AFT MOUNT PIN AT FRAME 18A, WS 6261. REPLACED NR 1 ENGINE PYLON AFT MOUNT PIN IAW A330 AMM 54-51-17-400-8040.

Part: WIRE — REVERSED (CABIN) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - EMERGENCY PATH LIGHTING INOP AT ALL SEATS. PERFORMED T/S ON EMERGENCY FLOOR PATH LIGHTING IAW A330 AMM 33-51-23 & FOUND REVERSE POLARITY ON EACH SEAT RECONNECT WIRING & PERFORMED OPS CHECKED & FOUND OPS CHECKED GOOD IAW AMM 33-51-13.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON RIGHT WING FLAP TRAILING EDGE AFT OF NR 3 FLAP CARRAGE AT FR43, RIB 14. REPAIRED RIGHT WING FLAP TRAILING EDGE AFT OF NR 3 FLAP CARRAGE AT FR43, RIB 14 IAW A330 SRM 57-55-00.

Part: CLEVIS PIN — WORN (NR 2 PYLON) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - EVIDENCE OF WEAR & MISSING PLATING ON NR 2 PYLON FORWARD ATTACH LUG INBOARD UPPER & LOWER PINS. REPLACED NR 2 PYLON FORWARD ATTACH LUG INBOARD UPPER & LOWER PINS IAW A330 AMM 54-51-17.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 13 INCHES OUTBOARD OF ER9. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 13 INCHES OUTBOARD OF ER9 IAW EO 5511U056.

Part: SKIN — SATURATED (ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 5 INCHES FORWARD OF TRAILING EDGE & 4 INCHES OUTBOARD OF ER10. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 5 INCHES FORWARD OF TRAILING EDGE & 4 INCHES OUTBOARD OF ER10 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON RIGHT ELEVATOR UPPER SURFACE AT 7 INCHES FORWARD OF TRAILING EDGE & 29 INCHES OUTBOARD OF ER6. REPAIRED RIGHT ELEVATOR UPPER SURFACE AT 7 INCHES FORWARD OF TRAILING EDGE & 29 INCHES OUTBOARD OF ER6 IAW EO 5511U056.

Part: FITTING — INOPERATIVE (EVAC SLIDE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - ESCAPE SLIDE ICE PROTECTION CONTROL UNIT 10DH FAILS TEST FORWARD LIGHT DOES NOT ILLUMINATE. REPLACED FORWARD HEATED SLIDE FITTING 12DH IAW A330 AMM 30-46-11. OPS CHECKED GOOD, GIRT BAR ADJUSTED GOOD IAW AMM 52-12-21 & AMM 30-46-00.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 4.5 INCHES FORWARD OF TRAILING EDGE & 39TH TRAILING EDGE FASTENER FROM OUTBOARD END. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 4.5 INCHES FORWARD OF TRAILING EDGE & 39TH TRAILING EDGE FASTENER FROM OUTBOARD END IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 14 INCHES INBOARD OF ER5. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 14 INCHES INBOARD OF ER5 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 8TH TRAILING EDGE FASTENER FROM OUTBOARD END. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 4 INCHES FORWARD OF TRAILING EDGE & 8TH TRAILING EDGE FASTENER FROM OUTBOARD END IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - MOISTURE INGRESS ON LEFT ELEVATOR UPPER SURFACE AT 5 INCHES FORWARD OF TRAILING EDGE & 4 INCHES INBOARD OF ER10. REPAIRED LEFT ELEVATOR UPPER SURFACE AT 5 INCHES FORWARD OF TRAILING EDGE & 4 INCHES INBOARD OF ER10 IAW EO 5511U056.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 241LF BETWEEN FR33 TO FR35, BETWEEN Y2462 TO Y2805. REPLACED FLOOR PANEL 241LF IAW A330 SRM 51-42-11.

Part: ASPIRATOR — DAMAGED (EVAC SLIDE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DURING SCHEDULED DEPLOYMENT THE DOOR SLIDE AT DOOR 3R IT WAS NOTED THAT THE SLIDE DEFLATED WITHIN 30 SECONDS OF DEPLOYMENT. UPON INSPECTION OF THE SLIDE ASSEMBLY IT WAS DISCOVERED THAT THE ASPIRATOR WAS DAMAGED, CAUSING THE DEFLATION. ADVISED THE RELIABILITY GROUP OF SLIDE FAILURE, ISSUED NEW TASK CARD # 33L20025001 TO PERFORM JOB AGAIN.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK ON CROSS BEAM AT FR9, Y=0. REPLACED CROSS BEAM AT FR9, Y=0 IAW A330 SRM 51-42-11 & AIRBUS DRAWING # A52110744.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 221GF BETWEEN FR14 TO FR16, Y2472. REPLACED FLOOR PANEL 221GF IAW TYPICAL REPAIR 330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 222KF BETWEEN FR14 TO FR16, -Y2472. REPAIRED FLOOR PANEL 222KF IAW TYPICAL REPAIR 330-5302-11-0330.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT FR69, Y=0. REPLACED FLOOR SUPPORT AT FR69, Y=0 IAW A330 SRM 53-41-14 FIG 102 & 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 271KF BETWEEN FR73 TO FR75, BETWEEN Y1950 TO Y2462. REPLACED FLOOR PANEL 271KF IAW TYPICAL REPAIR 330-5302-11-0330.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231UF BETWEEN FR25 TO FR26.1, BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 231UF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 241LF BETWEEN FR33 TO FR37, Y2462. REPLACED FLOOR PANEL 241LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252FG BETWEEN FR42 TO FR47, BETWEEN -Y1959 TO -Y2462. REPLACED FLOOR PANEL 252FG IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK ON FLOOR SUPPORT ANGLE AT FR53.2, Y1959. REPLACED FLOOR SUPPORT ANGLE AT FR53.2, Y1959 IAW A330 SRM 51-42-11 & AIRBUS DRAWING J3F53914435.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR PANEL 272RF BETWEEN FR73 TO FR75 & BETWEEN -Y1447.8 TO -Y2462. REPLACED LONGITUDINAL FLOOR PANEL 272RF IAW TYPICAL REPAIR TR 330-5302-11-0330.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM AT FR78, Y1137.1. REPLACED LONGITUDINAL FLOORBEAM AT FR78, Y1137.1 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231JF BETWEEN FR19 TO FR22, BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 231JF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, -Y450. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, BETWEEN Y=0 TO -Y450. REPLACED FLOOR SUPPORT AT FR13A, BETWEEN Y=0 TO -Y450 IAW A330 SRM 51-42-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAL PROFILE AT FR80, Y450. REPLACED SEAL PROFILE AT FR80, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR49, Y450. REPLACED SEAT TRACK BETWEEN FR47 TO FR49, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y2462. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y2462 IAW A330 SRM 53-00-15 & SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 272HF BETWEEN FR73 TO FR75, -Y1137. REPAIRED FLOOR PANEL 272HF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR76 & BETWEEN Y794 TO Y1137. REPLACED FLOOR PANEL BETWEEN FR73 TO FR76 & BETWEEN Y794 TO Y1137 IAW TYPICAL REPAIR TR 330-5302-11-0330.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON DOOR CUTOUT STRUCTURE BETWEEN FR73 TO FR75, Y2462. REPLACED DOOR CUTOUT STRUCTURE BETWEEN FR73 TO FR75, Y2462 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 272JF, BETWEEN FR73 TO FR75, BETWEEN Y1278 TO Y1447.8. REPLACED FLOOR PANEL 272JF IAW TYPICAL REPAIR 330-5302-11-0330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y1137. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y1137 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK ON FLOOR SUPPORT ANGLE AT FR53.2, -Y1959. REPLACED FLOOR SUPPORT ANGLE AT FR53.2, -Y1959 IAW A330 SRM 51-42-11, 51-42-12 & AIRBUS DRAWING J353914435.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231NF BETWEEN FR22 TO FR25 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 231NF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251LG BETWEEN FR47 TO FR51 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 251LG IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACKED FLOOR SUPPORT AT FR53.2, -Y1959. REPLACED FLOOR SUPPORT AT FR53.2, -Y1959 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR35, -Y1959. REPLACED SEAT TRACK AT FR35, -Y1959 IAW A330 SRM 53-00-15, 51-42-11, 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, Y953. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, Y953 IAW A330 SRM 53-00-15, 51-42-11 & AIRBUS DRAWING 53275845.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 242HF BETWEEN FR33 TO FR37 & BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 242HF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR37.4 TO FR39.2, Y450. REPLACED SEAT TRACK BETWEEN FR37.4 TO FR39.2, Y450 IAW A330 SRM 53-31-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1552.5. REPLACED SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1552.5 IAW A330 SRM 53-31-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR32 TO FR 33, Y1959. REPLACED SEAT TRACK BETWEEN FR32 TO FR 33, Y1959 IAW A330 SRM 53-00-15, 51-42-11, 51-44-11 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251DG BETWEEN FR42 TO FR47 & BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 251DG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 221EF AT FR18, -Y450. REPAIRED FLOOR PANEL 221EF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 232XF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y953 TO -Y 1456. REPLACED FLOOR PANEL 232XF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 241DF BETWEEN FR30 TO FR33 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 241DF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251CB BETWEEN FR42 TO FR47 & BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 251CB IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK DELAMINATION ON FLOOR PANEL 231VF BETWEEN FR26.1 TO FR26.4, BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 231VF IAW A320 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR37, -Y953. REPLACED SEAT TRACK AT FR37, -Y953 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252DG BETWEEN FR42 TO FR47 & BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 252DG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK DELAMINATION ON FLOOR PANEL 232WF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 232WF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR40.2 TO FR42, -Y1959. REPLACED SEAT TRACK BETWEEN FR40.2 TO FR42, -Y1959 IAW A330 SRM 53-31-15, SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 232BF BETWEEN FR15A TO FR19, BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 232BF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231XF BETWEEN FR26.1 TO 26.4 & BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 231XF IAW A320 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR31 TO FR32, Y450. REPLACED SEAT TRACK BETWEEN FR31 TO FR32, Y450 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 232PF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y2462. REPLACED FLOOR PANEL 232PF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231LF BETWEEN FR22 TO FR25 & BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 231LF IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT FR16, Y=0. REPLACED FLOOR SUPPORT AT FR16, Y=0 IAW A330 SRM 53-11-14 FIG 101, 51-42-11 & AIRBUS DRAWING F53113545.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR73 TO FR75, -Y450. REPLACED SEAT TRACK BETWEEN FR73 TO FR75, -Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, -Y1137.1. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y1137.1 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR59 TO FR61, -Y450. REPLACED SEAT TRACK BETWEEN FR59 TO FR61, -Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR32 TO FR34, -Y1552.5. REPLACED SEAT TRACK BETWEEN FR32 TO FR34, -Y1552.5 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1959. REPLACED SEAT TRACK BETWEEN FR53.4 TO FR53.5, -Y1959 IAW A330 SRM 53-31-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK AT FR33, Y1456. REPLACED SEAT TRACK AT FR33, Y1456 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 231VF IS DELAMINATED. REPLACED FLOOR PANEL 231VF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN -Y953 AND -Y1456 HAS DELAMINATION. REPLACED FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN -Y953 AND -Y1456 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 64 AND FR 66 AT Y450. REPLACED SEAT TRACK BETWEEN FR 64 AND FR 66 AT Y450 IAW A330 SRM 53-00-15, 51-42-11 AND 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 16 AND FR 17 AT Y-450. REPLACED SEAT TRACK BETWEEN FR 16 AND FR 17 AT Y-450 IAW A330 SRM 51-44-11, 51-42-11 AND 51-75-12.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN -Y450 AND -Y1953 HAS DELAMINATION. REPLACED FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN -Y450 AND -Y1953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN Y1959 AND Y2462 HAS DELAMINATION. REPLACED FLOOR PANEL LOCATED BETWEEN FR 22 AND FR 25, BETWEEN Y1959 AND Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL LOCATED BETWEEN FR 26.1 AND FR 26.4, BETWEEN -Y1456 AND -Y1959 HAS DELAMINATION. REPLACED FLOOR PANEL LOCATED BETWEEN FR 26.1 AND FR 26.4, BETWEEN -Y1456 AND -Y1959 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK AT FR 19 AND -Y953. REPLACED SEAT TRACK AT FR 19 AND -Y953 IAW A330 SRM 53-00-15, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 16A AND Y-1456. REPLACED FLOOR SUPPORT AT FR 16A AND Y-1456 IAW A330 SRM 53-11-14 FIG 101, 51-44-11 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 16A AND Y-1959. REPLACED FLOOR SUPPORT AT FR 16A AND Y-1959 IAW A330 SRM 53-11-14, 51-44-00 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 34 AND FR 36 AT Y-1456. REPLACED SEAT TRACK BETWEEN FR 34 AND FR 36 AT Y-1456 IAW A330 SRM 53-00-15, 51-44-11, 51-72-11 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 13A AND Y-450. REPLACED FLOOR SUPPORT AT FR 13A AND Y-450 IAW A330 SRM 51-74-00, 53-11-15, 51-44-11 AND 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 242DF IS DELAMINATED. REPLACED FLOOR PANEL 242DF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 232RF IS DELAMINATED. REPLACED FLOOR PANEL 232RF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 221AF IS DELAMINATED. REPLACED FLOOR PANEL 221AF IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 13A AND -Y1959. REPLACED FLOOR SUPPORT AT FR 13A AND -Y1959 IAW A330 SRM 53-11-14, 51-44-00 AND 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 232SF IS DELAMINATED. REPLACED FLOOR PANEL 232SF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 262WF IS DELAMINATED. REPAIRED FLOOR PANEL 262WF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 39 AND FR 39.2 AT Y1959. REPLACED SEAT TRACK BETWEEN FR 39 AND FR 39.2 AT Y1959 IAW A330 SRM 53-31-15 FIG 101, 51-44-11 AND 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 261MH IS DELAMINATED. REPAIRED FLOOR PANEL 261MH IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 262XG IS DELAMINATED. REPAIRED FLOOR PANEL 262XG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 262BG IS DELAMINATED. REPAIRED FLOOR PANEL 262BG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 251RF IS DELAMINATED. REPAIRED FLOOR PANEL 251RF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 47 AND FR 53.2 AT Y450. REPLACED SEAT TRACK BETWEEN FR 47 AND FR 53.2 AT Y450 IAW A330 SRM 51-74-00, 51-31-15 AND 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, FLOOR PANEL 262MG IS DELAMINATED. REPAIRED FLOOR PANEL 262MG IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 80 + 10 INCHES AND Y+450. REPLACED FLOOR SUPPORT AT FR 80 + 10 INCHES AND Y+450 IAW A330 SRM 51-74-00, 51-44-11 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, BETWEEN -Y730 TO -Y953. REPLACED FLOOR SUPPORT AT FR13A, BETWEEN -Y730 TO -Y953 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR49, Y953. REPLACED SEAT TRACK BETWEEN FR47 TO FR49, Y953 IAW A330 SRM 53-31-15 FIG 103 & 51-42-11.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK ON ANGLE SUPPORT BRACKET AT FR80 & BETWEEN -Y2462 TO Y2462. REPLACED ANGLE SUPPORT BRACKET AT FR80 & BETWEEN -Y2462 TO Y2462 IAW A330 SRM 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, BETWEEN -Y450 TO -Y730. REPLACED FLOOR SUPPORT AT FR13A, BETWEEN -Y450 TO -Y730 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 262TG AT FR69, Y953. REPAIRED FLOOR PANEL 262TG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261WG AT FR69, -Y450. REPAIRED FLOOR PANEL 261WG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251VF BETWEEN FR39.2 TO FR40, Y2462. REPAIRED FLOOR PANEL 251VF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261TG AT FR62, Y1959. REPAIRED FLOOR PANEL 261TG IAW A330 SRM 53-02-00.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK ON ANGLE SUPPORT BRACKET AT FR80 & BETWEEN -Y2462 TO Y2462. REPLACED ANGLE SUPPORT BRACKET AT FR80 & BETWEEN -Y2462 TO Y2462 IAW A330 SRM 51-42-11 & 51-44-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252SF BETWEEN FR39.2 TO FR40, Y953. REPAIRED FLOOR PANEL 252SF IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR76, Y1447.8. REPLACED FLOOR SUPPORT AT FR76, Y1447.8 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR15A TO FR19, Y1959. REPAIRED FLOOR PANEL 232DF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261XG BETWEEN FR69 TO FR71, Y450. REPAIRED FLOOR PANEL 261XG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251SF BETWEEN FR39.2 TO FR40, Y1465. REPAIRED FLOOR PANEL 251SF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 242CF BETWEEN FR30 TO FR33, Y450. REPAIRED FLOOR PANEL 242CF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 251UF BETWEEN FR39.2 TO FR40, Y2462. REPAIRED FLOOR PANEL 251UF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252UF BETWEEN FR39.2 TO FR40, Y2462. REPAIRED FLOOR PANEL 252UF IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, -Y730. REPLACED FLOOR SUPPORT AT FR13A, -Y730 IAW A330 SRM 51-73-00, 51-42-11 FIGURE 101 SHEET 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CRACK IN FLOOR PROFILE 'Z' ANGLE AT FR80+4 INCHES, Y1959. REPLACED FLOOR PROFILE 'Z' ANGLE AT FR80+4 INCHES, Y1959 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR12 TO FR22 & BETWEEN -Y1456 TO -Y1959. REPLACED FLOOR PANEL BETWEEN FR12 TO FR22 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR32 TO FR37.4 & BETWEEN -Y1456 TO -Y1959. REPLACED FLOOR PANEL BETWEEN FR32 TO FR37.4 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y1137. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y1137 IAW A330 SRM 51-74-00, 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, Y2462. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, Y2462 IAW A330 SRM 53-00-15 FIGURE 101, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 31 AND FR 32 AT -Y450. REPLACED SEAT TRACK BETWEEN FR 31 AND FR 32 AT -Y450 IAW A330 SRM 51-73-00, 53-00-15 FIG 102 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK AT FR34, -Y1456. REPLACED SEAT TRACK AT FR34, -Y1456 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, Y450 IAW A330 SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR33, -Y1959. REPLACED SEAT TRACK AT FR33, -Y1959 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR35 TO FR36, Y1552.5. REPLACED SEAT TRACK BETWEEN FR35 TO FR36, Y1552.5 IAW A330 SRM 53-00-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 35 AND FR 36 AT Y1959. REPLACED SEAT TRACK BETWEEN FR 35 AND FR 36 AT Y1959 IAW A330 SRM 53-00-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR73 TO FR74, BETWEEN -Y2462 TO -Y1959. REPLACED FLOOR SUPPORT BETWEEN FR73 TO FR74, BETWEEN -Y2462 TO -Y1959 IAW A330 SRM 53-41-14, 51-42-11, 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A & BETWEEN Y232 TO Y450. REPLACED FLOOR SUPPORT AT FR13A & BETWEEN Y232 TO Y450 IAW A330 SRM 53-11-14, 51-44-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR75 TO FR76, -Y1447.8. REPLACED FLOORBEAM BETWEEN FR75 TO FR76, -Y1447.8 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR71 TO FR73, -Y2462. REPLACED FLOORBEAM BETWEEN FR71 TO FR73, -Y2462 IAW A330 SRM 53-31-15 FIG 101, 51-42-11 & 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y350. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y350 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR75, -Y450. REPLACED LONGITUDINAL BEAM AT FR75, -Y450 IAW A330 SRM 53-41-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOOR SUPPORT AT FR 13A AND +Y232. REPLACED FLOOR SUPPORT AT FR 13A AND +Y 232 IAW A330 SRM 53-11-14 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR16 TO FR17, -Y953. REPLACED SEAT TRACK BETWEEN FR16 TO FR17, -Y953 IAW A330 SRM 51-74-00, 53-11-15 FIG 101, 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13 -Y1959. REPLACED FLOOR SUPPORT AT FR13 -Y1959 IAW A330 SRM 53-11-14, 51-44-00 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON LONGITUDINAL FLOORBEAM AT FR 74 AND Y-1137.1. REPLACED LONGITUDINAL FLOORBEAM AT FR 74 AND Y-1137.1 IAW A330 SRM 53-00-15, 51-44-11, 51-72-11 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR68 TO FR69, -Y450. REPLACED SEAT TRACK BETWEEN FR68 TO FR69, -Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK, CORROSION ON FLOORBEAM AT FR 73 AND Y+1278. REPLACED FLOORBEAM AT FR 73 AND Y+1278 IAW A330 SRM 53-41-14, 51-42-11 AND 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR76, -Y2462. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR76, -Y2462 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, -Y450. REPLACED FLOOR SUPPORT AT FR13A, -Y450 IAW A330 SRM 51-74-00, 53-11-15, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR76, BETWEEN -Y450 TO -Y648. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR76, BETWEEN -Y450 TO -Y648 IAW A330 SRM 53-41-14, 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR73, -Y794.3. REPLACED LONGITUDINAL BEAM AT FR73, -Y794.3 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, -Y350. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, -Y350 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR61, Y450. REPLACED SEAT TRACK AT FR61, Y450 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM AT FR78, Y1137.1. REPLACED LONGITUDINAL FLOORBEAM AT FR78, Y1137.1 IAW A330 SRM 53-41-14, 51-44-11, 51-74-00 & 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITIDUNAL BEAM AT FR76, Y2462. REPLACED LONGITIDUNAL BEAM AT FR76, Y2462 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR73+10 INCHES & BETWEEN Y1447 TO Y1959. REPLACED FLOORBEAM AT FR73+10 INCHES & BETWEEN Y1447 TO Y1959 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR78, Y=0. REPLACED FLOORBEAM AT FR78, Y=0 IAW A330 SRM 53-41-14 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, Y1456. REPLACED FLOOR SUPPORT AT FR13A, Y1456 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR78 TO FR80, -Y450. REPLACED SEAT TRACK BETWEEN FR78 TO FR80, -Y450 IAW A330 SRM 53-41-14, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT FR73, Y1278. REPLACED FLOOR SUPPORT AT FR73, Y1278 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGITUDINAL BEAM BETWEEN FR73 TO FR74, Y794.3. REPLACED LONGITUDINAL BEAM BETWEEN FR73 TO FR74, Y794.3 IAW A330 SRM 53-41-14 FIGURE 103, 51-42-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON PROFILE Z ASSY AT FR76, -Y2472. REPLACED PROFILE Z ASSY AT FR76, -Y2472 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR76 Y1447. REPLACED FLOOR SUPPORT AT FR76 Y1447 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PROFILE 'Z' ANGLE BETWEEN FR75 TO FR76, Y2462. REPLACED FLOOR PROFILE 'Z' ANGLE BETWEEN FR75 TO FR76, Y2462 IAW A330 SRM 51-42-11, 51-74-00 & 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR74 TO FR76, Y1137.1. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR74 TO FR76, Y1137.1 IAW A330 SRM 51-74-00, 53-41-14 & 51-42-11.

Part: SEAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON PROFILE SEAL AT FR80+10 INCHES, -Y450. REPLACED PROFILE SEAL AT FR80+10 INCHES, -Y450 IAW A330 SRM 53-41-14 FIG 101 & 51-42-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PROFILE 'Z' ANGLE AT 80+5 INCHES & BETWEEN Y1447.8 TO 1137.1. REPLACED FLOOR PROFILE 'Z' ANGLE AT 80+5 INCHES & BETWEEN Y1447.8 TO 1137.1 IAW A330 SRM 51-14-00 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR76, Y1447.8. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR76, Y1447.8 IAW A330 SRM 53-00-15 & 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM SUPPORT BETWEEN FR75 TO FR76 & BETWEEN Y2462 TO Y1959. REPLACED FLOOR BEAM SUPPORT BETWEEN FR75 TO FR76 & BETWEEN Y2462 TO Y1959 IAW A330 SRM 51-74-00, 51-42-11 & 51-49-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR73, Y2462. REPLACED FLOORBEAM AT FR73, Y2462 IAW A330 SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR80+4 INCHES, Y450. REPLACED FLOORBEAM AT FR80+4 INCHES, Y450 IAW A330 SRM 51-42-11, 51-74-00 & 53-41-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR80+10 INCHES, Y450. REPLACED FLOOR SUPPORT AT FR80+10 INCHES, Y450 IAW A330 SRM 51-74-00, 51-44-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR76, Y794.3. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR76, Y794.3 IAW A330 SRM 53-41-14 FIG 103.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOORBEAM AT FR70, Y1447.8. REPLACED LONGITUDINAL FLOORBEAM AT FR70, Y1447.8 IAW A330 SRM 53-00-15 & 51-42-11.

Part: SEAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAL PROFILE AT FR80+10 INCHES, -Y450. REPLACED SEAL PROFILE AT FR80+10 INCHES, -Y450 IAW A330 SRM 51-42-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PROFILE 'Z' ANGLE AT FR80+5 INCHES & BETWEEN -Y1137 & -Y794.3. REPLACED FLOOR PROFILE 'Z' ANGLE AT FR80+5 INCHES & BETWEEN -Y1137 & -Y794.3 IAW A330 SRM 51-42-11, 51-74-00 & 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR78 TO FR80, Y450. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR78 TO FR80, Y450 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,998 hrs · 7,159 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR73 PLUS 10 INCHES, BETWEEN Y2462 TO Y1959. REPLACED FLOOR SUPPORT AT FR73 PLUS 10 INCHES, BETWEEN Y2462 TO Y1959 IAW A330 SRM 53-41-14, 51-42-11.

Part: COVER — MISSING (CABIN) · airframe 50,447 hrs · 7,089 cycles

LGW - ESCAPE PATH LIGHTING LENS MISSING AT SEAT 22G. LGW MAINTENANCE TEMP REPAIR ACCOMPLISHED PER EA 200874 REF MON 4729278 AND SAD 4729279 FOR ALL FURTHER ACTION. CLT MAINTENANCE REPLACED LENS COVER AT SEAT 22G. OPERATIONAL CHECK IS NORMAL.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 50,355 hrs · 7,077 cycles

FCO - FA'S REPORT THAT EXIT LIGHTS DID NOT ILLUMINATE DURING TAXI OUT. MAINTENANCE - CIDS 1 & 2 RESET ACCOMPLISHED AND EXIT SIGNS OPERATE NORMALLY.

Part: COVER — MISSING (CABIN) · airframe 49,583 hrs · 6,975 cycles

MAD - 2R DOOR EXIT SIGN LENS COVER MISSING. MAINTENANCE LOCATED SIGN AND RE-ATTACHED AT DOOR 2L.

Part: FLUID — OVERHEATED (NR 1 IDG)

PHL FLT 732 EN ROUTE CLT TO LGW. RECEIVED ECAM MESSAGE "ELEC IDG 1 OIL OVHT". TEMP CONTINUED TO INCREASE TO 212 DEGREES C. DIVERTED TO PHL AND LANDED. DECLARED AN EMERGENCY. MAINTENANCE STATES: NR 1 IDG ON MEL 24-22-01A. NORMAL CONDITION UNDER MEL.

Part: BATTERY — DISCHARGED (CABIN)

PHL - DURING THE CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK, THE EPSU BATTERY AT DOOR R1 FAILED. MAINTENANCE REMOVED AND REPLACED THE EPSU BATTERY AT DOOR R1.

Part: FASTENER — LOOSE (CENTER WING) · airframe 48,122 hrs · 6,785 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 WITH CRACK INDICATIONS AT FR42 LEFT & RIGHT SIDE AT RIB 1. THE VERTICAL ANGLES WAS REPAIRED IAW EA 102869A & THE BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102851C.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAN - MAINTENANCE FOUND BOTH FLASHLIGHTS AT THE L3 DOOR IMPROPERLY INSTALLED AND THEIR BATTERIES DISCHARGED. MAINTENANCE REPLACED THE BATTERIES FOR THE FLASHLIGHTS AT THE L3 DOOR, AND PROPERLY INSTALLED THE FLASHLIGHTS IN THEIR HOLDERS.

Part: PROFILE — CORRODED (FUSELAGE) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - CORROSION ON LONGITUDINAL PROFILE BETWEEN FR70 TO FR72, Y=0. REPLACED LONGITUDINAL PROFILE BETWEEN FR70 TO FR72, Y=0 IAW A330 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 161CF BETWEEN FR67 TO FR36, S43, -Z1956. REPLACED CABIN FLOOR PANEL 161CF BETWEEN FR67 TO FR36, S43, -Z1956 IAW A330 SRM 51-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 162EF BETWEEN FR69 TO FR72 & BETWEEN Y=0 TO Y700. REPLACED CABIN FLOOR PANEL 162EF BETWEEN FR69 TO FR72 & BETWEEN Y=0 TO Y700 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251MF BETWEEN FR39 TO FR40 & BETWEEN Y450 TO Y953. REPAIRED CABIN FLOOR PANEL 251MF BETWEEN FR39 TO FR40 & BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 252ZF BETWEEN FR40 TO FR42 & BETWEEN -Y1456 TO -Y1959. REPAIRED CABIN FLOOR PANEL 252ZF BETWEEN FR40 TO FR42 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232DG BETWEEN FR26.4 TO FR27 & BETWEEN -Y1456 TO -Y1959. REPAIRED CABIN FLOOR PANEL 232DG BETWEEN FR26.4 TO FR27 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: CABLE — DISCONNECTED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - EEL - EMERGENCY ESCAPE PATH LIGHT ON SEAT 3AB FAILS. REMOVED FPEEMS SEAT MOUNTED LIGHT MODULE IAW AIRBUS A330 33-51-12-000-803-0. CONNECTED EMERGENCY SEAT LIGHT CABLE TO SLAT 3B IAW A330 AMM 33-51-12-400-803-0, RE-INSTALLED FPEEMS SEAT MOUNTED LIGHT MODULE IAW A330 AMM 33-51-12-400-803-0. OPS CHECK GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 152QF BETWEEN FR58 TO FR60 & BETWEEN -Y867 TO -Y1414. REPLACED CABIN FLOOR PANEL 152QF BETWEEN FR58 TO FR60 & BETWEEN -Y867 TO -Y1414 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 152NF BETWEEN FR58 TO FR60 & BETWEEN -Y203 TO -Y746. REPLACED CABIN FLOOR PANEL 152NF BETWEEN FR58 TO FR60 & BETWEEN -Y203 TO -Y746 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4 & BETWEEN -Y953 TO -Y1456. REPAIRED CABIN FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4 & BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 262LH BETWEEN FR57.1 TO FR58 & BETWEEN -Y953 TO -Y1959. REPAIRED CABIN FLOOR PANEL 262LH BETWEEN FR57.1 TO FR58 & BETWEEN -Y953 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 252CG BETWEEN FR42 TO FR47 & BETWEEN -Y450 TO -Y953. REPAIRED CABIN FLOOR PANEL 252CG BETWEEN FR42 TO FR47 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 252VF BETWEEN FR40 TO FR41 & BETWEEN -Y1959 TO -Y2462. REPAIRED CABIN FLOOR PANEL 252VF BETWEEN FR40 TO FR41 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251LF BETWEEN FR39 TO FR40 & BETWEEN Y450 TO -Y450. REPAIRED CABIN FLOOR PANEL 251LF BETWEEN FR39 TO FR40 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 262DF BETWEEN FR37 TO FR37.4 & BETWEEN -Y1456 TO -Y1959. REPAIRED CABIN FLOOR PANEL 262DF BETWEEN FR37 TO FR37.4 & BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - EEL - L33 EMERGENCY FLASHLIGHT HAVE DEAD BATTERIES. REPLACED BATTERIES IN L33 EMERGENCY FLASHLIGHT IAW A330 AMM 25-65-53-000-801 & 25-65-53-400-801. OPS CHECK GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 151PF BETWEEN FR58 TO FR60 & BETWEEN Y867 TO Y1414. REPLACED CABIN FLOOR PANEL 151PF BETWEEN FR58 TO FR60 & BETWEEN Y867 TO Y1414 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251NF BETWEEN FR39 TO FR39.2 & BETWEEN Y953 TO Y1456. REPAIRED CABIN FLOOR PANEL 251NF BETWEEN FR39 TO FR39.2 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL NR 231EF BETWEEN FR19 TO FR22 & BETWEEN -Y450 TO Y450. REPAIRED CABIN FLOOR PANEL 231EF BETWEEN FR19 TO FR22 & BETWEEN -Y450 TO Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 252EF BETWEEN FR37 TO FR37.4 & BETWEEN -Y1959 TO -Y2462. REPAIRED CABIN FLOOR PANEL 252EF BETWEEN FR37 TO FR37.4 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251CF BETWEEN FR37 TO FR37.4 & BETWEEN Y953 TO Y1456. REPAIRED CABIN FLOOR PANEL 251CF BETWEEN FR37 TO FR37.4 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251RF BETWEEN FR40 TO FR40.1 & BETWEEN Y450 TO -Y450. REPAIRED CABIN FLOOR PANEL 251RF BETWEEN FR40 TO FR40.1 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 151EF BETWEEN FR54 TO FR57.1 & BETWEEN -Y203 TO -Y746. REPLACED CABIN FLOOR PANEL 151EF BETWEEN FR54 TO FR57.1 & BETWEEN -Y203 TO -Y746 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 152AF BETWEEN FR53.2 TO FR53.6 & BETWEEN -Y203 TO -Y456. REPLACED CABIN FLOOR PANEL 152AF BETWEEN FR53.2 TO FR53.6 & BETWEEN -Y203 TO -Y456 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251PF BETWEEN FR39 TO FR40 & BETWEEN Y1456 TO Y1959. REPAIRED CABIN FLOOR PANEL 251PF BETWEEN FR39 TO FR40 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 151HF BETWEEN FR57.1 TO FR58, -Y1931. REPLACED CABIN FLOOR PANEL 151HF BETWEEN FR57.1 TO FR58, -Y1931 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN 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: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251EF BETWEEN FR37 TO FR37.4 & BETWEEN Y1959 TO Y2462. REPAIRED CABIN FLOOR PANEL 251EF BETWEEN FR37 TO FR37.4 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251DF BETWEEN FR37 TO FR37.4 & BETWEEN Y1456 TO Y1959. REPAIRED FLOOR PANEL 251DF BETWEEN FR37 TO FR37.4 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: DAMPER — PUNCTURED (R1 DOOR) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - EEL - R-1 DOOR DAMPER (EMERGENCY OPERATION CYLINDER) IS AT 0 PSI READING. REPLACED R-1 DOOR DAMPER (EMERGENCY OPERATION CYLINDER) IAW A330 AMM 52-10-00-020-050 & 52-10-00-420-050.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 151CF BETWEEN FR53.6 TO FR54 & BETWEEN Y206 TO Y753. REPLACED FLOOR PANEL 151CF BETWEEN FR53.6 TO FR54 & BETWEEN Y206 TO Y753 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 232FF BETWEEN FR19 TO FR22 & BETWEEN -Y950 TO -Y959. REPAIRED FLOOR PANEL 232FF BETWEEN FR19 TO FR22 & BETWEEN -Y950 TO -Y959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 231JF BETWEEN FR19 TO FR22 & BETWEEN Y1959 TO Y2462. REPAIRED CABIN FLOOR PANEL 231JF BETWEEN FR19 TO FR22 & BETWEEN Y1959 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 231LF BETWEEN FR22 TO FR25 & BETWEEN Y450 TO Y959. REPAIRED CABIN FLOOR PANEL 231LF BETWEEN FR22 TO FR25 & BETWEEN Y450 TO Y959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 252KG BETWEEN FR50 TO FR51 & BETWEEN -Y959 TO -Y1456. REPAIRED CABIN FLOOR PANEL 252KG BETWEEN FR50 TO FR51 & BETWEEN -Y959 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 231GF BETWEEN FR19 TO FR20 & BETWEEN Y959 TO Y1456. REPAIRED CABIN FLOOR PANEL 231GF BETWEEN FR19 TO FR20 & BETWEEN Y959 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 232HF AT FR19 BETWEEN -Y1456 TO -Y1959. REPAIRED FLOOR PANEL 232HF AT FR19 BETWEEN -Y1456 TO -Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 231FG AT FR25 & BETWEEN -Y450 TO Y450. REPAIRED CABIN FLOOR PANEL 231FG AT FR25 & BETWEEN -Y450 TO Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 232EG BETWEEN FR26.4 TO FR31 & BETWEEN -Y1959 TO -Y2462. REPAIRED CABIN FLOOR PANEL 232EG BETWEEN FR26.4 TO FR31 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 232CG AT FR26.4 BETWEEN -Y953 TO -Y1456. REPAIRED FLOOR PANEL 232CG AT FR26.4 BETWEEN -Y953 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 232XF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y959 TO -Y1456. REPAIRED CABIN FLOOR PANEL 232XF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y959 TO -Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 231FF BETWEEN FR19 TO FR22 & BETWEEN Y450 TO Y959. REPAIRED CABIN FLOOR PANEL 231FF BETWEEN FR19 TO FR22 & BETWEEN Y450 TO Y959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBOND ON CABIN FLOOR PANEL 261EH BETWEEN FR62 TO FR65 & BETWEEN Y953 TO Y1959. REPAIRED CABIN FLOOR PANEL NR 261EH BETWEEN FR62 TO FR65 & BETWEEN Y953 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 251RG BETWEEN FR51 TO FR53.2 & BETWEEN Y1546 TO Y1959. REPAIRED CABIN FLOOR PANEL 251RG BETWEEN FR51 TO FR53.2 & BETWEEN Y1546 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON AFT CARGO FLOOR PANEL 152HF BETWEEN FR57.1 TO FR58 & BETWEEN -Y456 TO -Y203. REPLACED AFT CARGO FLOOR PANEL 152HF BETWEEN FR57.1 TO FR58 & BETWEEN -Y456 TO -Y203 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232ZF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y1959 TO -Y2462. REPAIRED CABIN FLOOR PANEL 232ZF BETWEEN FR26.1 TO FR26.4 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON AFT CARGO FLOOR PANEL 152CF BETWEEN FR53.6 TO FR54 & BETWEEN -Y456 TO -Y203. REPLACED AFT CARGO FLOOR PANEL 152CF IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231AG BETWEEN FR26.4 TO FR30 & BETWEEN Y450 TO -Y450. REPAIRED CABIN FLOOR PANEL 231AG BETWEEN FR26.4 TO FR30 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232MF BETWEEN FR22 TO FR25 & BETWEEN -Y1456 TO -Y1953. REPAIRED CABIN FLOOR PANEL 232MF BETWEEN FR22 TO FR25 & BETWEEN -Y1456 TO -Y1953 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON FLOOR PANEL 231XF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y959 TO Y1456. REPAIRED FLOOR PANEL 231XF BETWEEN FR26.1 TO FR26.4 & BETWEEN Y959 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231TF BETWEEN FR25 TO FR26.1 & BETWEEN Y1456 TO Y1959. REPAIRED CABIN FLOOR PANEL 231TF BETWEEN FR25 TO FR26.1 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232SG BETWEEN FR65 TO FR67 & BETWEEN -Y450 TO -Y459. REPAIRED CABIN FLOOR PANEL 232SG BETWEEN FR65 TO FR67 & BETWEEN -Y450 TO -Y459 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DELAMINATION ON CABIN FLOOR PANEL 232GF BETWEEN FR19 TO FR22 & BETWEEN -Y1456 TO -Y959. REPAIRED CABIN FLOOR PANEL 232GF BETWEEN FR19 TO FR22 & BETWEEN -Y1456 TO -Y959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232NF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y456. REPAIRED CABIN FLOOR PANEL 232NF BETWEEN FR22 TO FR25 & BETWEEN -Y1959 TO -Y456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231HF BETWEEN FR19 TO FR22 & BETWEEN Y1456 TO Y1959. REPAIRED CABIN FLOOR PANEL 231HF BETWEEN FR19 TO FR22 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - EEL - BOTH FLASHLIGHTS ARE DEAD ON L54. REPLACED BOTH FLASHLIGHT BATTRIES ON AFT WALL OF ON L54 IAW A330 AMM25-65-53-000-801 & 25-65-400-801.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231QF AT FR25 & BETWEEN -Y450 TO Y450. REPAIRED CABIN FLOOR PANEL 231QF AT FR25 & BETWEEN -Y450 TO Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 479,196 hrs · 754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231NF AT FR22 & BETWEEN Y1456 TO Y1959. REPAIRED CABIN FLOOR PANEL 231NF AT FR22 & BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231MF AT FR22 & BETWEEN Y953 TO Y1456. REPAIRED CABIN FLOOR PANEL 231MF AT FR22 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 231UF AT FR25 & BETWEEN Y2462 TO Y1959. REPAIRED CABIN FLOOR PANEL 231UF AT FR25 & BETWEEN Y2462 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN)

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232UF AT FR25 & BETWEEN -Y1959 TO -Y2462. REPAIRED CABIN FLOOR PANEL 232UF AT FR25 & BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 47,919 hrs · 6,754 cycles

CWF - C1 - MAJOR REPAIR - DISBONDING ON CABIN FLOOR PANEL 232LF AT FR22 & BETWEEN -Y450 TO -Y953. REPAIRED CABIN FLOOR PANEL 232LF AT FR22 & BETWEEN -Y450 TO -Y953 IAW A330 SRM 53-02-00.

Part: SEAL — DEFECTIVE (PRESSURE SWITCH)

FLT 734. AFTER TAKEOFF, RECEIVED AN "ENG 2 FUEL FILTER CLOG" ECAM MESSAGE AT APPROXIMATELY 1,500 FEET ABOVE GROUND LEVEL (AGL). MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE FUEL FILTER AND DIFFERENTIAL PRESSURE SWITCH. FOUND CONNECTOR INTERFACIAL SEAL DEFECTIVE.

Part: LIGHT — DEFECTIVE (COCKPIT)

MAD - THE CAPTAIN'S OVERHEAD MAP LIGHT HAD A SHORT AND SOME SMOKE, IT CONTINUED TO WORK. THE CIRCUIT BREAKER WAS PULLED AND COLLARED 722VU, R40. THIS CIRCUIT BREAKER WILL ALSO MAKE THE FIRST OFFICER'S MAP LIGHT INOPERATIVE. MAINTENANCE INSPECTED WIRING IN THE OVERHEAD FOR THE CAPTAIN'S MAP LIGHT ASSEMBLY, NO DEFECTS WERE NOTED. THE LIGHT ASSEMBLY WAS REPLACED AND RESET CIRCUIT BREAKER R40. OPERATIONAL TESTS ARE SATISFACTORY AND MEL REMOVED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

MAD - FOUND FIRST OFFICER'S FLASHLIGHT RED LED NOT BLINKING. REPLACED F/O'S FLASHLIGHT.

Part: SEAL — ODOR (ENGINE)

SJU FLT 1071 EN ROUTE PHL TO SJU. ON DESCENT THROUGH 9000 FT, DETECTED VERY STRONG ODOR THROUGHOUT CABIN AND COCKPIT. ODOR SIMILAR TO TURBINE OIL. PASSENGERS AND FLIGHT ATTENDANTS COMPLAINED OF ODOR. ODOR WENT AWAY AT 2000 FT. MAINTENANCE REPLACED THE NUMBER TWO ENGINE. THE 1.5 BEARING SEAL WAS DISCREPANT.

Part: BATTERY PACK — FAULTY (CABIN)

PHL - L2 BATTERY PACK FAULT. REMOVED AND REPLACED BATTERY PACK L2.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAN - CREW EMERGENCY TORCH AT DOOR 4R FOUND INSTALLED INCORRECTLY AND BATTERY FLAT. BATTERY REPLACED AND TORCH REINSTALLED CORRECTLY.

Part: BOTTLE — LOW PRESSURE (L2 DOOR)

CLT - THE FORWARD CIDS PANEL SHOWS RED ON L2 DOOR. SERVICED L2 DOOR BOTTLE PRESSURE.

Part: BOLT — BROKEN (L2 DOOR)

MAN - GROUND CREW REPORTS LOUD BANG ON DOOR OPENING, DOOR L2. MAN MAINTENANCE FOUND DOOR SPRING ROD ASSY BOLT BROKEN AT GIMBAL END. REPLACED SPRING ROD ASSY AND SPRING ROD BOLT AT L2.

Part: BATTERY — DISCHARGED (CABIN)

MAN - THE TORCH AT DOOR L3 INDICATOR LIGHT WAS INOPERATIVE. BATTERY REPLACED.

Part: BOLT — BROKEN (L2 DOOR)

THE R2 DOOR ATTACHMENT DAMPER BOLT WAS FOUND BROKEN. MX REPLACED THE R2 DOOR ATTACHMENT DAMPER BOLT. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,497 hrs · 5,339 cycles

BFM C2 MAJOR REPAIR NR 6115044 CORROSION ON SEAT TRACK BETWEEN FR39.2 TO FR47, Y450. REPLACED SEAT TRACK BETWEEN FR39.2 TO FR47, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,497 hrs · 5,339 cycles

BFM C2 MAJOR REPAIR NR 6127115 CORROSION ON SEAT TRACK AT FR58 TO FR68, Y450. REPAIRED SEAT TRACK AT FR58 TO FR68, Y450 IAW A330 SRM 53-00-15 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,497 hrs · 5,339 cycles

BFM C2 MAJOR REPAIR NR 6127118 CORROSION ON SEAT TRACK AT FR54 TO FR58, -Y450. REPAIRED SEAT TRACK AT FR54 TO FR58, -Y450 IAW A330 SRM 53-00-15, 51-42-11 AND 51-73-00.

Part: RECEIVER — FAILED (GPS)

LHR FLT 728 PHL TO LHR THE FIRST OFFICERS GPS BECAME INOPERATIVE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED MULTI MODE RECEIVER NR 2. OPS CHECKS OK.

Part: WINDSHIELD — CRACKED (COCKPIT)

YHZ - FLT 700 EN ROUTE PHL TO FRA. THE FLIGHT REPORTED A CRACKED WINDSHIELD DURING CRUISE FLIGHT. PROCEDURES REQUIRED DESCENDING TO FL 230. THE FLIGHT DIVERTED TO YHZ SINCE THE FUEL BURN AT FL 230 WOULD BECOME EXCESSIVE. THE FLIGHT LANDED WTIHOUT FURTHER INCIDENT. (S) MAINTENANCE REPLACED THE FIRST OFFICER`S WINDSHIELD. OPERATIONALLY CHECKS OK. (B)

Part: ADIRU — FAILED (NR 3)

MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS. THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. SUBSEQUENT INFO: MAINTENANCE REPLACED ADIRU 2. OPERATIONAL CHECKS OK. (S)

Part: ADIRU — MALFUNCTIONED (NR 3)

MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS. THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. (S)

Part: ADIRU — FAILED (NR 3)

MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS. THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. MAINTENANCE REPLACED ADIRU 2. OPERATIONAL CHECKS OK. (S)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

PHL FLT 741 MAD TO PHL, CREW STATED 'NLG WHEEL STEERING FAULT DISPLAYED ON ECAMS WHEN NLG EXTENDED.' CREW RECYCLED THE GEAR TO SEE IF THE INDICATION WOULD DISAPPEAR AND IT DID NOT. THE GEAR INDICATION SHOWED THREE GREEN FOR BOTH CYCLES. FLIGHT LANDED AND TAXIED OFF THE ACTIVE RUNWAY UNDER ITS OWN POWER AND STOPPED, REQUESTING A TOW IN BY TUG. AN EMERGENCY WAS DECLARED AS A PRECAUTIONARY MEASURE. MAINTENANCE REPLACED NWS SELECTOR VALVE.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS)

PHL - MAINTENANCE REPORTED THE L1 AND R2 BATTERIES FAULTED ON EMERGENCY LIGHT BATTERY TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU'S AT L1 AND R2. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 30,908 hrs · 4,441 cycles

L1 DOOR EMERGENCY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED THE L1 POWER SUPPLY.

Part: COMPUTER — FAULTED (DMC) · airframe 29,982 hrs · 4,315 cycles

FLIGHT 718, PHL-FCO: AT CRUISE, ENGINE PAGE DISPLAYED ON CAPTAINS NAV DISPLAY PANEL. SELECTED DMC 3 AND NR 1 DMC FAULT DISPLAYED. RESET NR 1 DMC AND PROBLEM CLEARED. RETURNED TO PHL. MAINTENANCE REPLACED THE NR 1 DMC. NO FURTHER FAULTS.

Part: CHIP DETECTOR — MISSING (NR 3) · airframe 28,849 hrs · 4,149 cycles

DURING FLIGHT, CREW REPORTED DECREASING OIL QUANTITY INDICATION ON RT ENGINE. CREW REDUCED THRUST TO IDLE AND CONTINUED. ENGINE WAS NOT SHUTDOWN AND FLIGHT LANDED UNEVENTFULLY. MAINTENANCE FOUND THE NR 3 BEARING CHIP DETECTOR MISSING. REPLACE THE RT ENGINE OIL SCAVENGE PUMP.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,032 hrs · 4,035 cycles

FLIGHT 1403, FCO-PHL: DURING CRUISE, CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN NEAR ROW 15. CREW SHUTDOWN THE INFLIGHT ENTERTAINMENT SYSTEM AND SMELL SUBSIDED. NO FURTHER DIFFICULTIES NOTED, AND FLIGHT CONTINUED TO PHL. MAINTENANCE CONDUCTED AN OPERATIONAL CHECK OF THE INFLIGHT ENTERTAINMENT SYSTEM AND NOTED NO PROBLEMS. A/C RETURNED TO SERVICE, AND NO FURTHER DIFFICULTIES.