N277AY

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 84,211 hrs · 11,863 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 1R INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER STANDARD PRACTICES.

Part: ACTUATOR — FAULTY (R3 DOOR) · airframe 83,553 hrs · 11,758 cycles

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

Part: ACTUATOR — FAULTY (L3 DOOR) · airframe 83,553 hrs · 11,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR L3 DAMPER, IN PASSENGER CABIN, DID NOT PASS OPERATIONAL TEST. MAINTENANCE REPLACED L3 DOOR DAMPER (ACTUATOR) PER AMM 52-22-14-400-801-A.

Part: FITTING — CRACKED (FRAME 64) · airframe 83,909 hrs · 11,805 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT CARGO DOOR FRAME FORK FITTING FORWARD LEG AND BEAM 4 AT FR 64. REPLACED FRAME FORK FITTING PER AARD 52-32-00-2.

Part: SUPPORT FITTING — LEAKING (FUEL SYSTEM) · airframe 83,553 hrs · 11,758 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS FUEL LEAKS AT BOTH LT AND RT ROTATING FITTINGS FOR THE THS. ***SUPPLEMENTAL INFORMATION: MAINTENANCE REPORTS ACCOMPLISHED FINAL RESTORATION ON THS TRIM TANK REAR SUPPORT FITTING LT AND RT IAW EA 297773B.*** (CLOSED)

Part: PROBE — UNRELIABLE (FUEL SYS) · airframe 83,547 hrs · 11,757 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING FLIGHT WERE MONITORING FUEL BURN & FUEL PG SLIGHTLY DOWN ON FUEL INITIALLY, THEN SLIGHTLY UP FOR OVER 1HR 45MIN. THEN 2HRS & 23 MIN INTO FLIGHT NOTICED 3300 MORE POUNDS IN LEFT INNER TANK THEN RIGHT(13,060 US 9780) OTHER INDICATIONS NML EXCEPT DOWN 2,000 #'S TOTAL. THEN TAIL TANK FED RIGHT INNER BUT IT WENT HIGHER THEN LEFT (10.800 VS 13,200) THEN THEY BALANCED OUT AT ABOUT 2:53 INTO FLT (STILL DOWN 2100 #'S TOTAL) THEN AT 3:10 INTO FLT LEFT GOES UP BY 1100 #'S MORE THAN RIGHT THEN AT 3:36 INTO FLIGHT BOTH SIDES STABILIZED BUT DOWN 3100S TOTAL. PARKING AT LAX FUEL DOWN ONLY 2700'S FOB US PLAWWED, ALSO NOTICED 3:45 MIN INTO FLT TOTAL FUEL SHOWED BY GAUGES IN ALL TANKS EQUALS 33,600 BUT FOB 27,200. NOTE FUEL USED & FOB EQUALS CORRECT #, BUT TANKS SHOW OVER 6,000 LBS MORE ADDED UP. UPON SUTDOWN AT LAX FUEL TANKS READ 0+22+74.6 (LEFT) 0+2080+7140 (RIGHT) 19,080 #'S VS 14,800 FOB, FUEL USED (73,380) + FOB 14.8=87 + CHANGE WHICH IS WHAT WE LEFT WITH CORRECT # - BUT INDIVIDUAL TANKS ARE READING MUCH MORE -TNKS READ 4,280#'S MORE THAN FOB. MAINTENANCE REMOVED AND REPLACED FQI PROBES; FIN 28GH, 30QT1, 30QT2, 28QT2 AND 123QT2. LEAK AND OPS CHECKED GOOD IAW A330 AMM 28-42-15 PB 401 AND 57-27-11-400-801-A.

Part: PROBE — UNRELIABLE (FUEL SYSTEM) · airframe 83,547 hrs · 11,757 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING FLIGHT WERE MONITORING FUEL BURN & FUEL PG SLIGHTLY DOWN ON FUEL INITIALLY, THEN SLIGHTLY UP FOR OVER 1HR 45MIN. THEN 2HRS & 23 MIN INTO FLIGHT NOTICED 3300 MORE POUNDS IN LEFT INNER TANK THEN RIGHT(13,060 US 9780) OTHER INDICATIONS NML EXCEPT DOWN 2,000 #'S TOTAL. THEN TAIL TANK FED RIGHT INNER BUT IT WENT HIGHER THEN LEFT (10.800 VS 13,200) THEN THEY BALANCED OUT AT ABOUT 2:53 INTO FLT (STILL DOWN 2100 #'S TOTAL) THEN AT 3:10 INTO FLT LEFT GOES UP BY 1100 #'S MORE THAN RIGHT THEN AT 3:36 INTO FLIGHT BOTH SIDES STABILIZED BUT DOWN 3100S TOTAL. PARKING AT LAX FUEL DOWN ONLY 2700'S FOB US PLAWWED, ALSO NOTICED 3:45 MIN INTO FLT TOTAL FUEL SHOWED BY GAUGES IN ALL TANKS EQUALS 33,600 BUT FOB 27,200. NOTE FUEL USED & FOB EQUALS CORRECT #, BUT TANKS SHOW OVER 6,000 LBS MORE ADDED UP. UPON SUTDOWN AT LAX FUEL TANKS READ 0+22+74.6 (LEFT) 0+2080+7140 (RIGHT) 19,080 #'S VS 14,800 FOB, FUEL USED (73,380) + FOB 14.8=87 + CHANGE WHICH IS WHAT WE LEFT WITH CORRECT # - BUT INDIVIDUAL TANKS ARE READING MUCH MORE -TNKS READ 4,280#'S MORE THAN FOB. MAINTENANCE REMOVED AND REPLACED FQI PROBES; FIN 28GH, 30QT1, 30QT2, 28QT2 AND 123QT2. LEAK AND OPS CHECKED GOOD IAW A330 AMM 28-42-15 PB 401 AND 57-27-11-400-801-A.

Part: PROBE — UNRELIABLE (FUEL SYSTEM) · airframe 83,547 hrs · 11,757 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING FLIGHT WERE MONITORING FUEL BURN & FUEL PG SLIGHTLY DOWN ON FUEL INITIALLY, THEN SLIGHTLY UP FOR OVER 1HR 45MIN. THEN 2HRS & 23 MIN INTO FLIGHT NOTICED 3300 MORE POUNDS IN LEFT INNER TANK THEN RIGHT(13,060 US 9780) OTHER INDICATIONS NML EXCEPT DOWN 2,000 #'S TOTAL. THEN TAIL TANK FED RIGHT INNER BUT IT WENT HIGHER THEN LEFT (10.800 VS 13,200) THEN THEY BALANCED OUT AT ABOUT 2:53 INTO FLT (STILL DOWN 2100 #'S TOTAL) THEN AT 3:10 INTO FLT LEFT GOES UP BY 1100 #'S MORE THAN RIGHT THEN AT 3:36 INTO FLIGHT BOTH SIDES STABILIZED BUT DOWN 3100S TOTAL. PARKING AT LAX FUEL DOWN ONLY 2700'S FOB US PLAWWED, ALSO NOTICED 3:45 MIN INTO FLT TOTAL FUEL SHOWED BY GAUGES IN ALL TANKS EQUALS 33,600 BUT FOB 27,200. NOTE FUEL USED & FOB EQUALS CORRECT #, BUT TANKS SHOW OVER 6,000 LBS MORE ADDED UP. UPON SUTDOWN AT LAX FUEL TANKS READ 0+22+74.6 (LEFT) 0+2080+7140 (RIGHT) 19,080 #'S VS 14,800 FOB, FUEL USED (73,380) + FOB 14.8=87 + CHANGE WHICH IS WHAT WE LEFT WITH CORRECT # - BUT INDIVIDUAL TANKS ARE READING MUCH MORE -TNKS READ 4,280#'S MORE THAN FOB. MAINTENANCE REMOVED AND REPLACED FQI PROBES; FIN 28GH, 30QT1, 30QT2, 28QT2 AND 123QT2. LEAK AND OPS CHECKED GOOD IAW A330 AMM 28-42-15 PB 401 AND 57-27-11-400-801-A.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 82,861 hrs · 11,668 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR R3 EMERGENCY FLASH LIGHT INOPERABLE. MAINTENANCE REPLACED FLASH LIGHT BATTERY PER AMM 25-65-00.

Part: RELAY — MALFUNCTIONED (GENERATOR)

AIRCRAFT IN BASE MAINTENANCE: DURING TRANSIT CHECK OPS TEST OF EMERGENCY GEN SYS FAILED, WOULD NOT SHUT OFF. REMOVED AND REPLACED RELAY 6XE REF ESPM 20-46-50-01, OP CHECKED EMERGENCY GENERATION SYSTEM REF JOB CARD 33L00005001. OPS CHECKS NORMAL.

Part: DECODER — FAULTY (R1 DOOR) · airframe 81,030 hrs · 11,415 cycles

ON CLOSING THE R1 DOOR, DOOR\SLIDE PRESSURE ILLUMINATED. REPLACED DEU B FIN 300RH2 IAW AMM 23-73-47, FAULT CLEARED ON FAP DOOR PAGE.

Part: PIN — PULLED (L4 SLIDE COVER) · airframe 80,841 hrs · 11,388 cycles

L4 DOOR SLIDE COVER FORWARD ALIGNMENT PIN PULLED OUT OF COVER. ORDERED SERVICEABLE SLIDE COVER. INSTALLED DURING SLIDE REPLACEMENT PER J/C 33L00025001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 80,078 hrs · 11,284 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT (12WL) FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 80,078 hrs · 11,284 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT (13WL) FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,445 hrs · 10,957 cycles

SEAT 3A EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 77,056 hrs · 10,902 cycles

EMERGENCY FLASHLIGHT AT THE AFT RIGHT FLIGHT ATTENDANT STATION IS INOPERATIVE. REPLACED BATTERY. OPS CHECKED NORMAL IAW AMM 25-65-00.

Part: DAMPER — DEFECTIVE (EMERGENCY EXIT) · airframe 77,032 hrs · 10,896 cycles

EMERGENCY EXIT DOOR 844 DAMPER, DAMPING EFFECT DOES NOT OCCUR IN PASSENGER CABIN. REPLACED EMERGENCY EXIT DOOR DAMPER IAW AMM 52-22-14.

Part: FITTING — DEFECTIVE (SLIDE) · airframe 77,032 hrs · 10,896 cycles

TEST OF THE CONTROL UNIT SLIDE F FAILED. HEATING 4DH IN FORWARD AVIONIC COMPARTMENT. REMOVED AND REPLACED HEATED SLIDE FITTING IAW AMM 30-46-11-801-A, AMM 52-11-31-400-801-A, AND AWM 30-46-02. PERFORMED OPS CHECK OF THE ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION. TESTED OK.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

TRAPPED WATER INDICATED ON THE LEFT ELEVATOR HONEYCOMB CORE STRUCTURE LOWER PANEL LOCATED BETWEEN ER2 AND ER3 AND 4 INCHES FROM TRAILING EDGE AND 16 INCHES FROM OUTBOARD ELEVATOR RIB 2. REPAIRED THE LT ELEVATOR HONEY COMB CORE STRUCTURE LOWER PANEL IAW EA 277206 AND SRM 55-21-11-300-008.

Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

TRAPPED WATER INDICATION ON RIGHT ELEVATOR HONEYCOMB CORE STRUCTURE LOWER PANEL AT RIB 4, 4 INCHES FROM TRAILING EDGE ON RIGHT HORIZONTAL STABILIZER. REPAIRED THE RIGHT ELEVATOR HONEY COMB STRUCTURE IAW EA 277207 AND SRM 55-21-11-300-016.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON RIGHT HAND ELEVATOR HONEYCOMB CORE STRUCTURE UPPER PANEL LOCATED 8.750 INCHES INBOARD FROM ELEVATOR RIB 3 AND 20.5 INCHES AFT FROM LEADING EDGE FASTENER ROW ON RIGHT HAND HORIZONTAL STABILIZER. REPAIRED RIGHT HAND ELEVATOR HONEY COMB CORE STRUCTURE UPPER PANEL PER EA 277207 AND SRM 55-21-11-300-016.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 77,032 hrs · 10,896 cycles

CRACK LOCATED ON THE FRONT SPAR LOWER SKIN BETWEEN RIBS 19 - 20 ON THE RIGHT HORIZONTAL STAB. REPAIRED THE SPAR LOWER SKIN IAW SRM 55-77-133-911-008.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 161AF, IN THE AFT CARGO BAY BETWEEN FRAMES 65 TO 67, LBL Y1470 TO RBL -Y805. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: ACTUATOR — INOPERATIVE (PAX DOOR) · airframe 77,032 hrs · 10,896 cycles

EMERGENCY EXIT DOOR DAMPER, DAMPING EFFECT DOES NOT OCCUR . AIRCRAFT WAS GROUNDED. REPLACED THE ACTUATOR.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 272AG, FRAMES 71 TO 73, Y1254 TO Y2161.1. REPLACED THE FLOOR PANEL SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: WINDOW — GLAZED (PAX DOOR) · airframe 77,032 hrs · 10,896 cycles

GLAZED OUTER PANE OF THE L1 WINDOW PASSENGER DOOR. REPLACED THE WINDOW WINDOW IAW AMM 56-31-11-400-801-A STEP 4.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 77,032 hrs · 10,896 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON TOP LAYER OF FLOOR PANEL 251WF IN PASSENGER CABIN. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER A330 SRM 53-02-00-300-009 PAR 2A FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 252YF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 53-55) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 262LF, BETWEEN FRAMES 53.9 TO 55, AND Y-1456 TO Y-953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 251EG IN PASSENGER CABIN BETWEEN FR 42 TO FR 47 AT LBL Y1456 TO LBL Y1959. REPLACED FLOOR PANEL 251EG PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: BEAM — CORRODED (FRAMES 71-72) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION ON BEAM BETWEEN FRAMES 71 AND 72. REPLACED BEAM IAW SRM 51-72-11-911-001, AND DWG F53478101.

Part: BEAM — CORRODED (FRAMES 71-72) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE BEAM ASSEMBLY LOCATED BETWEEN -0YA TO -YB, AND BETWEEN FRAMES 71 AND 72. REPLACED THE BEAM IAW SRM 51-42-11, SRM 51-72-11, AND DWG F53478101.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 232BF IN PASSENGER CABIN BETWEEN FR 15 TO FR 19 AT RBL -Y953 TO RBL -Y450. REPLACED FLOOR PANEL 232BF PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 242EF IN PASSENGER CABIN, BETWEEN FRAMES 25 TO 27, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 251ZF IN PASSENGER CABIN BETWEEN FR 40 TO FR 42 AT LBL Y1456 TO LBL Y1959. REPLACED FLOOR PANEL 251ZF PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: COUPLING — CRACKED (FUSELAGE) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED COUPLING AT TORSION BOX RUN-OUT FOR DOOR 3 IN PASSENGER CABIN, AT FR 53.5, RIGHT HAND STRINGER 15. REPLACED COUPLING PER SRM 51-72-11 AND DRAWING F53370020.

Part: FLOOR PANEL — DELAMINATED (FRAME 39) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 252NF LOCATED BETWEEN FRAMES 39 TO 39.2 AND Y953 TO Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIG 20109, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 251JF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DAMAGED (GALLEY) · airframe 77,032 hrs · 10,896 cycles

CORROSION AND DELAMINATION FOUND ON FLOOR PANEL 272CF INSERT IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 73-76) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 271HF, BETWEEN FRAMES 73 TO 76 AND Y794.3 TO Y1247.8. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 41-42) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 251 CG, BETWEEN FRAMES 42 TO 41, Y450 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIG 20109, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (FRAME 53-55) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 261NF, BETWEEN FRAMES 53.9 TO 55, AND Y1959 TO Y1456. REPLACED THE FLOOR PANEL SRM 53-02-00-300-009, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37-39) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 251FF, FRAMES 37.4 TO 39, -Y450 TO Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REV G.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

CORROSION ON FLOOR PANEL 241FF, IN THE PASSENGER CABIN. PERFORMED A VISUAL AND TAP TEST INSPECTIONS AND FOUND DELAMINATION AROUND THE CORRODED INSERTS. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PAR 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 14-15) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 221EF BETWEEN FRAMES 14 AND 15, Y953 TO -Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIG 20109.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 77,032 hrs · 10,896 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 232 CG (TOP LAYER) IN PASSENGER CABIN. REPLACED FLOOR PANEL PER A330 SRM 53-02-00-300-009 PAR 2A FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 271PF IN PASSENGER CABIN BETWEEN FRAMES 78 TO 80, LBL Y450 TO RBL -Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2.A, FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 77,032 hrs · 10,896 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 232DF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER A330 SRM 53-02-00-300-009 PAR 2A FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE FLOOR PANEL IN THE PASSENGER CABIN. REPLACED FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 232GF IN PASSENGER CABIN BETWEEN FR 19 TO FR 22 AT RBL -Y1959 TO LBL Y2462. REPLACED FLOOR PANEL 232GF PER SRM 53-02-00-300-009, PARAGRAPH 2A, FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

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

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 231BF IN PASSENGER CABIN BETWEEN FRAMES 15A TO 19 AT LBL Y450 TO LBL Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 271CF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

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

Part: FLOOR PANEL — DELAMINATED (FRAMES 50-51) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 251KG, BETWEEN FRAMES 50 TO 51, Y953 TO Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REV.G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON TOP LAYER OF FLOOR PANEL 251AG IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 77,032 hrs · 10,896 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 251PG IN PASSENGER CABIN. REPLACED FLOOR PANEL WITH REPLACEMENT MATERIAL PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 271FF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK BETWEEN FR 73 TO FR 74 AT RBL -YB. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 231DG, FRAMES 26.4 TO 31, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 221AF IN PASSENGER CABIN BETWEEN FR 11 TO FR 14 AT RBL -Y728 TO LBL Y230. REPLACED FLOOR PANEL 221AF PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 272BF IN PASSENGER CABIN, BETWEEN FRAMES 71 TO 73, -Y450 TO -Y794.3. REPLACED FLOOR PANEL 272BF PER A330 SRM 53-02-00-300-009, PARAGRAPH 2A, FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 14-17) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 221JF, BETWEEN FRAMES 14 TO 17, Y1456 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: SEAT TRACK — CORRODED (FRAMES 71-75) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 71 AND 75, BL Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 241CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009 PARA 2A FIGURE 20109, IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 272QF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 252CF IN PASSENGER CABIN BETWEEN FR 37 TO FR 37.4 AT RBL -Y1959 TO RBL -Y953. REPLACED FLOOR PANEL 252CF PER SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON TOP LAYER OF FLOOR PANEL 261WG, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 271AF IN PASSENGER CABIN BETWEEN FR 71 TO FR 73 AT RBL Y-450 TO LBL Y450. REPLACED FLOOR PANEL 271AF PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 19-22) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 231JF BETWEEN FRAMES 19 TO 22, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 271AG IN THE PASSENGER CABIN, FRAMES 71 TO 73, Y1187.6 TO Y2161.1. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 231AG BETWEEN FR 26.4 TO FR 31 AT LBL Y450 TO RBL -Y450. REPLACED FLOOR PANEL 231AG PER SRM 53-02-00-300-009, PARAGRAPH 2 A, FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 262MF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: SEAT TRACK — CORRODED (FRAMES 37-38) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORRODED SEAT TRACK IN THE PAX CABIN, BETWEEN FRAMES 37 TO 38 AT RBL -Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS F53279681, AND F53278700.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 252FG, FRAMES 42 TO 47, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 241GF IN PASSENGER CABIN, BETWEEN FRAMES 33 TO 37, Y450 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

CORROSION AND DELAMINATION ON FLOOR PANEL 252BF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 19-22) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 232HF, BETWEEN FRAMES 19 TO 22 AND Y1456 TO Y1959. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIG 20109, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 252EF IN PASSENGER CABIN BETWEEN FR 37 TO FR 37.4 AT RBL -Y2462 TO RBL -Y1959. REPLACED FLOOR PANEL 252EF PER SRM 53-02-00-300-009, PARAGRAPH 2A, FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 271QF IN THE PASSENGER CABIN, FRAMES 78 TO 80, Y1447.8 TO Y480. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 252PG IN PASSENGER CABIN (TOP LAYER). REPLACED FOOR PANEL WITH REPLACEMENT MATERIAL PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE FLOOR PANEL 271LF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 242HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 251BF IN PASSENGER CABIN BETWEEN FR 37 TO FR 37.4 AT LBL Y450 TO LBL Y953. REPLACED FLOOR PANEL 251BF PER SRM 53-02-00-300-009, PARAGRAPH 2A, FIGURE 20109 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 231CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009 PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 262JH IN PASSENGER CABIN BETWEEN FR 53.7 TO FR 53.9 AT RBL Y-1456 TO RBL Y-1959. REPLACED FLOOR PANEL 262JH PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON TOP LAYER OF THE FLOOR PANEL LOCATED BETWEEN FRAMES 75 TO 78, Y381.0 -Y1857.5. REPAIRED THE FLOOR PANEL IAW EA 277354, SRM 53-02-00-300-010, AND 53-02-00-300-03.

Part: FLOOR PANEL — DELAMINATED (FRAMES 53-55) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 261MF BETWEEN FRAMES 53.9 AND 55, Y1456 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED FLOORBEAM AFT GALLEY AREA BETWEEN FR 71 TO FR 75 AT RBL -Y450. REPLACED FLOORBEAM PER SRM 51-72-11 DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE TOP LAYER OF FLOOR PANEL 261PF, IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PAR 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 15-19) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 231AF BETWEEN FRAMES 15A TO 19, -Y450 TO Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION ON FLOOR PANEL 272HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 30-33) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 241DF, BETWEEN FRAMES 30 TO 33, Y2462 TO Y1959. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIG 20109.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 271MF, FRAMES 75 TO 78, Y381 TO -Y381. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIG 20109, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 73-76) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 271GF, BETWEEN FRAMES 73 TO 76, Y381 TO Y794.3. REPLACED THE FLOOR PANEL SRM 53-02-00-300-009, AND IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 272GF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON FLOOR PANEL 231EG, FRAMES 26.4 TO 31, Y1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 47-51) · airframe 77,032 hrs · 10,896 cycles

DELAMINATION FOUND ON THE FLOOR PANEL 251GG BETWEEN FRAMES 47 AND 51, -Y450 AND Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2A, FIG 20109.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 241HF IN PASSENGER CABIN BETWEEN FR 33 TO FR 37 AT LBL Y4501 TO LBL Y953. REPLACED FLOOR PANEL 241HF PER SRM 53-02-00-300-009 AND IRM 9701, REVISION G.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 73 AND 74, BL -YB TO -YC1. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING F53478018.

Part: SHEAR WEB — CRACKED (FRAMES 75A-76) · airframe 77,032 hrs · 10,896 cycles

CRACKED SHEAR WEB BETWEEN FRAMES 75A TO 76, STRINGER 26R IN THE AFT GALLEY AREA. REPLACED THE SHEAR WEB IAW SRM 51-72-11, AND DRAWING F53479320.

Part: FITTING — CRACKED (FRAME 12A) · airframe 77,032 hrs · 10,896 cycles

CRACK FOUND ON THE STIFFNER FITTING AT FRAME 12A, STRINGER 26R. REPLACED THE FITTING IAW SRM 51-72-11, AND EO 5315U155-002.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75A-77) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 75A TO 77. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53479335.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED FLOORBEAM IN AFT GALLEY AREA BETWEEN FR 73 TO FR 74, LEFT HAND STRINGER 26, LBL YA. REPLACED FLOOR BEAM PER SRM 51-72-11 AND DRAWING F53478101.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 73 TO 74, YA TO YB1. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING F53478018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED FLOORBEAM AFT GALLEY AREA BETWEEN FR 75 TO FR 76, LEFT HAND STRINGER 26. REPLACED SRM 51-72-11 AND DRAWING F53479335.

Part: FITTING — CRACKED (FRAME 80) · airframe 77,032 hrs · 10,896 cycles

CRACK FOUND UNDER THE FLOOR IN THE FITTING AT FRAME 80, BL-Y1447. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING F53479750.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER FITTING AT FR 12A, LEFT STRINGER 26, FLOOR PANEL LEVEL LEFT HAND SIDE AT FORWARD GALLEY AREA. REPAIRED STIFFENER FITTING PER SRM 51-72-11 AND EO 5315U155-001.

Part: BEAM — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE BEAM LOCATED BETWEEN FRAMES 73 AND 74, -YA AND YB1. REPLACED BEAM IAW SRM 51-42-11, SRM 51-72-11, AND DWG F53478018.

Part: FRAME — CRACKED (FRM 40) · airframe 77,032 hrs · 10,896 cycles

CRACK INDICATION ON FRAME 40, VERTICAL WEB FASTENER HOLE 263. PERFORMED A TIME LIMITED REPAIR ON THE FRAME IAW EA 276983.

Part: CROSSBEAM — CRACKED (FRAME 74) · airframe 77,032 hrs · 10,896 cycles

CRACK LOCATED ON THE CROSSBEAM, FRAME 74, Y1453. REPAIRED THE CROSSBEAM IAW SRM 53-00-14-300-002, FIGURE 20102.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORRODED SEAT TRACK AT FRAME 17, -Y450. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING F53114410.

Part: FLOORBEAM — CORRODED (FRAME 35) · airframe 77,032 hrs · 10,896 cycles

CORRODED FLOORBEAM IN PASSENGER CABIN, FRAME 35, RBL -Y2462. REPAIRED THE FLOORBEAM IAW EA 277469.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TRAPPED WATER INDICATED ON LEFT HAND ELEVATOR HONEYCOMB CORE STRUCTURE LOWER PANEL LOCATED BETWEEN RIB 6 AND RIB 7. REPAIRED LEFT HAND ELEVATOR HONEYCOMB PER EA 277206 AND A330 SRM 55-21-11-300-008.

Part: SEAT TRACK — CORRODED (FRAMES 31-37) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORRODED SEAT TRACK IN PASSENGER CABIN BETWEEN FRAMES 31 TO 37 AT RBL -Y2462. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS F53275849 AND F53275795.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

RIGHT ELEVATOR HAD TRAPPED WATER INDICATED IN THE ELEVATOR HONEYCOMB CORE STRUCTURE UPPER PANEL LOCATED 15 INCHES OTBD FROM ELEVATOR RIB 9 AND 7.25 INCHES FROM TRAILING EDGE OF RIGHT HAND HORIZONTAL STABILIZER. REPAIRED THE RIGHT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER PANEL IAW EA 277207, AND SRM 55-21-11-300-016.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

TRAPPED WATER INDICATED ON LEFT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER PANEL LOCATED BETWEEN ER 8 AND ER9 AT 8.75 INCHES FROM TRAILING EDGE AND 7.0 INCHES INBOARD FROM ELEVATOR RIB 8. REPAIRED THE LEFT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER PANEL IAW EA N.277206, AND SRM 55-21-11-300-015.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK IN FORWARD GALLEY AREA AT FR 17, LBL Y450. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53111248.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK IN PASSENGER CABIN BETWEEN FR 30 TO FR 37 AT LBL Y450. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275849.

Part: FITTING — CORRODED (FRAME 15-17) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON HARD POINT FITTING BETWEEN FR15 AND FR17, AND Y-953, AND Y-1456. REPLACED HARD POINT FITTING PER SRM A330 51-72-11 AND DRAWING F25310032.

Part: FITTING — CORRODED (FRAMES 15-17) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE HARD POINT FITTING BETWEEN FRAMES 15 AND 17, WL -Y1456 TO -Y1959. REPLACED FITTING IAW SRM 51-72-11, AND DWG F25310032.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 77,032 hrs · 10,896 cycles

LEFT ELEVATOR HAS TRAPPED WATER LOCATED BETWEEN RIBS 7 AND 8, 3.25 INCHES INBOARD FROM ELEVATOR RIB 8 AND 8 INCHES FROM TRAILING EDGE. REPAIRED THE LEFT ELEVATOR HONEYCOMB CORE STRUCTURE LOWER PANEL IAW EA 277206 AND SRM 55-21-11-300-008.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED SEAT TRACK IN PASSENGER CABIN BETWEEN FR 32 TO FR 34, RIGHT HAND STRINGER 26 AT RBL -Y1552.5. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275677.

Part: SEAT TRACK — CORRODED (FRAME 35) · corrosion level 2 · airframe 77,032 hrs · 10,896 cycles

CORROSION FOUND ON THE SEAT TRACK, FRAME 35, -Y1959. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53275849.

Part: SKIN — DAMAGED (RUDDER) · airframe 77,032 hrs · 10,896 cycles

TRAPPED WATER FOUND ON THE RUDDER LEFT SURFACE BETWEEN HSS 463 AND 576, AND BETWEEN BR 4 TO BR 5. REPAIRED THE RUDDER SURFACE IAW EA 276974.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 77,032 hrs · 10,896 cycles

DELAMINATED FLOOR PANEL 161EF IN AFT CARGO COMPARTMENT BETWEEN FR 69 TO FR 72 AT LBL Y140 TO LBL Y1470. REPLACED FLOOR PANEL 161EF PER SRM A330 53-02-00-283-001.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,968 hrs · 10,887 cycles

SEAT 13G EMERGENCY LIGHT LENS MISSNG. REPLACED THE LIGHT ASSEMBLY.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 76,583 hrs · 10,827 cycles

AIRCRAFT WAS NOT GROUNDED. A/C LEFT NEAR AFT LAV FACING THE AISLE, EMERGENCY EXIT LIGHT BROKEN. REPLACED MISSING LENS.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 76,419 hrs · 10,807 cycles

AIRCRAFT WAS NOT GROUNDED. ARMING LEVER ON 2L DOOR DOES NOT FULLY GO TO ARM POSITION, BUT SHOWS ARMED IN COCKPIT. REMOVED DEBRIS FROM GIRT (BAR) FITTING, 2L DOOR ARMING LEVER OPERATIONAL CHECK SATISFACTORY. DOOR ARM INDICATION NORMAL ON FLIGHT ATTENDANT PANEL AND ECAM.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 76,344 hrs · 10,797 cycles

WHILE ACCOMPLISHING JOB CARD 33C20033002, THE EMERGENCY POWER SUPPLY UNIT 13WL FAULTED. REPLACED THE POWER SUPPLY IAW AMM 33-51-38-000-801 AND 33-51-38-400-801.

Part: DECODER — FAULTY (EMERGENCY LIGHTS) · airframe 76,344 hrs · 10,797 cycles

WHILE ACCOMPLISHING JOB CARD 33C20033002, DECODER - ENCODER-B 300RH3 FAULTED. REPLACED DECODER ENCODER IAW AMM 23-73-47-000-801 AND 23-73-47-400-801.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,092 hrs · 10,765 cycles

WHILE CHECKING EMERGENCY LIGHTS, FOUND A LOW LEVEL LIGHT AT SEAT 3G INOPERATIVE. REPLACED THE WIRE HARNESS ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 75,936 hrs · 10,743 cycles

R3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 75,689 hrs · 10,711 cycles

FOUND THE R3 DOOR EMERGENCY CYLINDER TO LOW PRESSURE DURING A PDC CHECK. SERVICED THE EMERGENCY CYLINDER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,611 hrs · 10,701 cycles

EMERGENCY LIGHT LENS ADJACENT TO LAVATORY L73 MISSING. REPLACED THE LIGHT ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 75,306 hrs · 10,663 cycles

R3 DOOR ASSIST BOTTLE LOW. SERVICED THE DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 75,017 hrs · 10,629 cycles

DURING DAILY CHECK, FOUND THE R3 DOOR EMERGENCY OPERATION CYLINDER IN THE YELLOW BAND. CHARGED BOTTLE IAW AMM 52-22-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,775 hrs · 10,599 cycles

EMERGENCY LIGHT LENS AT L4 DOOR BY THE F/A JUMPSEAT IS MISSING. REPLACED LENS.

Part: LENS — MISSING (CABIN) · airframe 74,413 hrs · 10,555 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT COVER LENS MISSING AT DOOR 4L. REPLACED WALL MOUNT EMERGENCY LIGHT ASSEMBLY.

Part: BOLT — CORRODED (LT FLAP TRACK) · airframe 74,228 hrs · 10,532 cycles

FLAP TRACK FAIRING ON LEFT WING CAME LOOSE AFTER FLAP RETRACTION. FOUND CORRODED BOLT CAME LOOSE. REPLACED WITH NEW BOLT. AIRCRAFT WAS GROUNDED.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR SLIDE) · airframe 74,132 hrs · 10,519 cycles

L4 DOOR SLIDE WILL NOT ARM. REMOVED DEBRIS FROM SLIDE ARMING LEVER GIRT BAR. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 74,081 hrs · 10,513 cycles

POWER SUPPLY UNIT OVER THE L2 DOOR, FAULT LIGHT ILLUMINATED. REPLACED POWER SUPPLY IAW AMM 33-51-38.

Part: FMC — FAILED (NR 2) · airframe 73,860 hrs · 10,485 cycles

BOTH CREW FMC FAILED ON FINAL APPROACH AT 14,000 FEET. EMERGENCY DECLARED. ATC PROVIDED RADAR VECTORS FOR APPROACH AND LANDING. FLIGHT LANDED WITHOUT INCIDENT. REPLACED FMGC 2. AIRCRAFT WAS GROUNDED.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 73,185 hrs · 10,394 cycles

11WL EPSU SUSPECT BAD. REPLACED EPSU. AIRCRAFT WAS GROUNDED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 73,185 hrs · 10,394 cycles

SEAT 3A EMERGENCY LIGHT INOPERATIVE. CONNECTED THE CONNECTOR. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,185 hrs · 10,394 cycles

13WL EPSU WONT SELF TEST. R & R THE BATTERY PACK. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,185 hrs · 10,394 cycles

11WL EPSU SUSPECT BAD. REPLACED THE BATTERY PACK. AIRCRAFT WAS GROUNDED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 73,185 hrs · 10,394 cycles

13WL EPSU WONT SELF TEST. R & R THE EPSU. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (CABIN) · airframe 73,150 hrs · 10,388 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS MISSING BY 4R DOOR. INSTALLED EMERGENCY LIGHT LENS.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 72,614 hrs · 10,290 cycles

SEAT 3A TERMINAL LUG BROKE ON EMERGENCY LIGHT. REPLACED TERMINAL IAW EPSM 20-43-14 AND AMM 33-51-00-710-801-A01.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

L2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

R3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R3 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

L3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L3 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

R2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R2 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R4 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

R4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R4 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — LOOSE (R3 DOOR ASSIST) · airframe 72,614 hrs · 10,290 cycles

R3 DOOR EMERGENCY ASSIST ACTUATOR HAS EXCESSIVE PLAY. REPLACED THE ACTUATOR IAW AMM 52-32-14.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 72,036 hrs · 10,204 cycles

L4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L4 DOOR ASSIST BOTTLE AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FITTING — NO TEST (DOOR SLIDE) · airframe 72,612 hrs · 10,289 cycles

HEATED DOOR SLIDE FITTING, FAILED OPERATIONAL RESISTANCE CHECK. REPLACED THE SLIDE FITTING IAW AMM 30-44-11 AND AMM 30-46-11. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 30-46-710-801-A.

Part: WIRE — LOOSE (CABIN) · airframe 71,041 hrs · 10,076 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 6H EMERGENCY LIGHT INOPERATIVE. RECONNECTED LOOSE WIRE FOR SEAT 6H EMERGENCY EXIT LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 70,906 hrs · 10,059 cycles

AIRCRAFT WAS NOT GROUNDED, 4R DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED 4R DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: TRANSFORMER — DEFECTIVE (CHILLER) · airframe 70,545 hrs · 10,013 cycles

FUMES AND EXCESSIVE HEAT DETECTED IN AFT GALLEY. MAINTENANCE REPLACED THE RIGHT AFT CHILLER CIRCUIT BREAKER AND TRANSFORMER IAW WDM 25-56-07 AND 25-33-14/15. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.

Part: CIRCUIT BREAKER — DEFECTIVE (GALLEY) · airframe 70,545 hrs · 10,013 cycles

FUMES AND EXCESSIVE HEAT DETECTED IN AFT GALLEY. MAINTENANCE REPLACED THE RIGHT AFT CHILLER CIRCUIT BREAKER AND TRANSFORMER IAW WDM 25-56-07 AND 25-33-14/15. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.

Part: LINER — OUT OF POSITION (L3 DOOR) · airframe 70,465 hrs · 10,003 cycles

L3 DOOR UPPER HINGE INTERIOR DOOR LINING CONTACTING FUSELAGE WHEN OPENING. MAINTENANCE FOUND THE OVERHEAD LINING AND LIGHT LENS ABOVE THE 3L DOOR OBSRTUCTING THE OPERATION OF THE DOOR. MAINTENANCE REPOSITIONED AND SECURED THE LINING AND LENS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 70,222 hrs · 9,973 cycles

ACFT WAS NOT GROUNDED: R4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 69,906 hrs · 9,933 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-13-14.

Part: BATTERY — FAILED (CABIN) · airframe 69,745 hrs · 9,913 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT, 11WL, BATTERY FAILED CAPACITY CHECK. REPLACED BATTERY AND ACCOMPLISHED A SATISFACORY OPS CHECK IAW AMM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 69,745 hrs · 9,913 cycles

AIRCRAFT WAS NOT GROUNDED, EMERGENCY POWER SUPPLY UNIT, 16WL, BATTERY FAILED CAPACITY CHECK. REPLACED BATTERY AND ACCOMPLISHED A SATISFACORY OPS CHECK IAW AMM 33-51-38.

Part: CONTROL SERVO — DEFECTIVE (LT AILERON) · airframe 69,488 hrs · 9,882 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTED THAT THE LT OTBD AILERON WAS OSCILLATING & FLUTTERING RHYTHMICALLY DURING CRUISE & DECLARED AN EMER AS A PRECAUTIONARY MEASURE WHERE THE ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT & TAXIED TO THE GATE UNDER ITS OWN POWER. REPLACED THE LT OTBD AILERON SERVO CONTROL 10CS1 & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 27-14-51.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 69,282 hrs · 9,853 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT ON SEAT 6H INOPERATIVE. RE-SEATED CONNECTOR BEHIND SEAT 6H ACCESS PANEL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 69,248 hrs · 9,849 cycles

AIRCRAFT WAS NOT GNDED. ELEC SMELL COMING FROM ESPRESSO MAKERS IN MID GALLEY. REPLACED ESPRESSO MAKERS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 68,896 hrs · 9,799 cycles

AIRCRAFT WAS GNDED. ON FWD FLIGHT ATTENDANT CIDS PANEL DOOR 4R DOES NOT SHOW ARMED & CHECK DOOR 4R PRESS IS ALSO INDICATED. DOOR 4R SHOWS ARMED ON ECAM PAGE. SERVICED 4R DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802-A. MSG CLEARED ON CIDS.

Part: LENS — MISSING (CABIN) · airframe 68,794 hrs · 9,784 cycles

AIRCRAFT WAS NOT GNDED. LENS COVER MISSING FROM FLOOR EMER LIGHTS NEAR THE LAVATORY 73 DOOR. INSTALLED LENS COVER IAW AMM 33-51-16.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 68,627 hrs · 9,746 cycles

AIRCRAFT WAS NOT GNDED. DOOR 4R CIDS CAUTION LOW PRESS. SERVICED 4R DOOR ASSIST BOTTLE IAW AMM 52-10-00, FAULT CLEARED.

Part: FITTING — FAILED (ZONE 800) · airframe 68,496 hrs · 9,714 cycles

AIRCRAFT IN BASE MX. SLIDE LOCK CONTROL BOX 4DH FAILED TEST AFT. R & R SLIDE FITTING IAW AMM 30-46-11-000-809-A. OPERATIONAL CHECKED GOOD IAW AMM 30-46-00-710-801. DOOR ADJUSTMENT COMPLETED IAW AMM 52-11-00-801-A.

Part: FITTING — FAILED (ZONE 800) · airframe 68,496 hrs · 9,714 cycles

AIRCRAFT IN BASE MX. CONTROL SLIDE LOCK 21DH FAILED TEST FWD. R & R LT SIDE FITTING IAW AMM 30-46-11-000-87-A. OPERATIONAL CHECKED GOOD IAW AMM 30-46-00-710-801-A. DOOR ADJUSTMENT COMPLETED IAW AMM 52-11-00-820-801-A.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 68,487 hrs · 9,710 cycles

AIRCRAFT WAS NOT GNDED. FUEL AFT XFR INOPERATIVE. ACCOMPLISHED TSM 28-27-00-810-825 NR 3 TRIM TRANSFERS TO INNER TANK. OPERATIONAL TEST OF TRIM TRANSFER PUMP, NO FAULTS NOTED FCMC 1 SHOWS TRIM PIPE ISOLATION VLV FAULT. REPLACED TRIM PIPE ISOLATION VLV ACTUATOR IAW AMM 28-27-53.

Part: SCHRADER VALVE — LEAKING (R4 DOOR) · airframe 68,439 hrs · 9,703 cycles

AIRCRAFT WAS NOT GNDED. LOW PSI 4R DOOR. REPLACED 4R DOOR DAMPNER SCHRADER VLV. SERVICED DOOR DAMPNER IAW 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 68,252 hrs · 9,648 cycles

CIDS PANEL SAYS CHECK DOOR PRESS. SERVICED 4R DOOR ASSIST BOTTLE SYS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 67,606 hrs · 9,532 cycles

R4 DOOR PRESS LOW. SERVICED R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802A.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 67,505 hrs · 9,518 cycles

4R DOOR SHOWS LOW PRESS ON CIDS WHEN ARMING DOORS. SERVICED IAW AMM 52-10-00-600-802-A.

Part: SIGN — DETACHED (CABIN) · airframe 67,471 hrs · 9,512 cycles

3L EXIT SIGN HAS BECOME DETACHED. EXIT SIGN COVER REFITTED IAW AMM 33-51-16-400-801-A.

Part: TERMINAL — BROKEN (CABIN) · airframe 67,129 hrs · 9,468 cycles

EMERGENCY LIGHT AT SEAT 3A INOPERATIVE. REPLACED DAMAGED TERMINAL AT CONNECTOR 5731VC AT SEAT 3LH IAW ESPM 20-48-14. SATISFACTORY OPERATION CHECK ACCOMPLISHED.

Part: CABLE — LOOSE (CABIN) · airframe 66,526 hrs · 9,379 cycles

ROW 3A EMER LIGHT INOPERATIVE. R & R LAMPS BULB AT SEAT 3A, FOUND CABLE LOOSE, CONNECTED TESTED OK.

Part: LENS — MISSING (CABIN) · airframe 66,088 hrs · 9,317 cycles

DURING CHECK FOUND EMER LENS COVER MISSING FROM AFT OUTSIDE WALL OF LAVATORY L62. REPLACED LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,008 hrs · 9,170 cycles

LHR ON ETOPS CHECK FOUND EMER LIGHTS AT 6H, 11H & 31H INOPERATIVE. MX PENDING.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 64,958 hrs · 9,164 cycles

SEAT 25F EMERGENCY LIGHT COVER MISSING. REPLACED THE MISSING COVER AT SEAT 25F.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 64,527 hrs · 9,108 cycles

R4 DOOR ASSIST CYLINDER PRESS LOW. CHARGED R4 DOOR ASSIST CYLINDER. LEAK CHECK IS GOOD.

Part: SLIDE RAFT — UNLACED (L2 DOOR) · airframe 64,316 hrs · 9,066 cycles

FOUND L2 DOOR SLIDE, LACING UNLACED. REPLACED L2 DOOR SLIDE RAFT ASSEMBLY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,136 hrs · 9,024 cycles

C2 CHECK, CABIN SEAT TRACK AT -Y1956 BETWEEN FRAME 62 & 71 HAS CORROSION. REPLACED WITH NEW SEAT TRACK IAW SRM 51-42-11 & 51-44-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,016 hrs · 9,001 cycles

EMERGENCY LIGHT ON SEAT 3A INOPERATIVE. R & R LAMP ASSEMBLY & RELAMPED.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 63,978 hrs · 8,992 cycles

CIDS PANEL SHOWS DOOR SLIDE 4R PRESS CHECK. SERVICED 4R DOOR ASSIST BOTTLE PRESS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,621 hrs · 8,924 cycles

DURING R4 SLIDE REPLACEMENT EMER LIGHT OPERATIONS TEST, FAULT L4 LIGHT SWITCH. R & R POWER SUPPLY UNIT EMER BATTERY. ALSO FOUND L4 LIGHTING SWITCH PIN REMOVED, INSTALLED. OPERATIONS CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (R4 DOOR)

R4 DOOR EMER OPERATION CYLINDER LOW PRESS. SERVICED R4 DOOR EMER OPERATION CYLINDER.

Part: BATTERY — FAULTED (CABIN) · airframe 63,199 hrs · 8,859 cycles

WHILE ACCOMPLISHING JOB CARD EPSU BATTERIES AT 4L & 4R FAULTED. R & R ESPU BATTERIES 4L & 4R.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 61,843 hrs · 8,680 cycles

FOUND AT 4R DOOR DAMPER CYLINDER LOW PRESS. RECHARGED 4R DOOR DAMPER CYLINDER.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 61,646 hrs · 8,654 cycles

A23 VISIT R4 DOOR ASSIST BOTTLE PRESS IS LOWER THAN 1783 PSI, FIN 360RH8. SERVICED CYLINDER TO REQUIRED PRESS IAW JOB CARD 33C80052002.

Part: WIRE — BROKEN (CABIN) · airframe 61,438 hrs · 8,627 cycles

EMERGENCY LIGHT AT SEAT 2G INOPERATIVE. REPAIRED BROKEN WIRE.

Part: SOCKET — LOOSE (CABIN) · airframe 61,357 hrs · 8,617 cycles

SEAT 1A EMERGENCY PATH LIGHT INOPERATIVE. SECURED SOCKET GND AT CF20 WIRE 5276 SEAT ROW 1A.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 61,207 hrs · 8,597 cycles

THE CAPTAIN CALLED DISPATCH SHORTLY AFTER TAKEOFF FROM CLT TO REPORT A GREEN HYD SYS LEAK. THE FLIGHT RETURNED TO CLT & LANDED SAFELY. REMOVED THE NR 1 GREEN HYD PUMP. CLEANED PANELS 191AB & 197FB.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 61,207 hrs · 8,597 cycles

THE CAPTAIN CALLED DISPATCH SHORTLY AFTER TAKEOFF FROM CLT TO REPORT A GREEN HYD SYS LEAK. THE FLIGHT RETURNED TO CLT & LANDED SAFELY. REMOVED THE NR 2 GREEN HYD PUMP. CLEANED PANELS 191AB & 197FB.

Part: LINK PIN — CORRODED (LT MLG) · airframe 61,116 hrs · 8,585 cycles

ALI & MLG LLP LIGHT CORROSION ON LT MLG RETRACTION LINK PIN. REPLACED LT MLG RETRACTION LINK PIN IAW AMM 32-11-11-400-806-A.

Part: LINK PIN — CORRODED (LT MLG) · airframe 61,116 hrs · 8,585 cycles

ALI & MLG LLP LIGHT CORROSION ON LT MLG RETRACTION LINK PIN. REPLACED LT MLG RETRACTION LINK PIN IAW AMM 32-11-11-400-806-A.

Part: LINK PIN — CORRODED (RT MLG) · airframe 61,116 hrs · 8,585 cycles

ALI & MLG LLP LIGHT CORROSION ON RT MLG RETRACTION LINK PIN. REPLACED RT MLG RETRACTION LINK PIN IAW AMM 32-11-11-400-806-A.

Part: LINK PIN — CORRODED (RT MLG) · airframe 61,116 hrs · 8,585 cycles

ALI & MLG LLP LIGHT CORROSION ON RT MLG RETRACTION LINK PIN. REPLACED RT MLG RETRACTION LINK PIN IAW JOB CARD 33-3211-9-0068.

Part: MONITOR — MALFUNCTIONED (CABIN) · airframe 60,558 hrs · 8,513 cycles

SEAT 17D VIDEO MONITOR SMOKING WAS SHUT DOWN. R & R VIDEO MONITOR 17D. OPERATIONAL CHECK IS OKAY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,569 hrs · 8,349 cycles

JUMP SEAT BY 4L DOOR, BREAKAWAY FLASHLIGHT NEEDS REPLACED. REPLACED BATTERY IN CABIN FLASHLIGHT AT JUMP SEAT BY 4L DOOR, CHECKED OK.

Part: FITTING — FAILED (R3 DOOR) · airframe 59,381 hrs · 8,320 cycles

C1 CHECK, DURING OPERATIONS CHECK OF ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION, ALL FOUR EACH LIGHTS TEST FAILED TO ILLUMINATE ON THE 21DH & 22DH CONTROL UNITS. R & R R3 DOOR AFT HEATED SLIDE FITTING, 26DH, IAW A330 AMM 30-46-11-000-801-A & 30-46-11-400-801A. CHECKED ADJUSTMENT OF 26DH HEATED SLIDE FITTING. ARMED & DISARMED GOOD IAW A330 AMM 52-13-00-820-801-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 59,381 hrs · 8,320 cycles

C1 CHECK, AFT CARGO FLOOR PANEL 151EF IS PUNCTURED & SOFT. FABRICATED & INSTALLED NEW CARGO FLOOR PANEL IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,381 hrs · 8,320 cycles

BC1CHECK, CABIN FLOOR PANEL 151AF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW A330 SRM 53-02-00 FIGURE 211.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,381 hrs · 8,320 cycles

BC1 CHECK, CABIN FLOOR PANEL 151AJ DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW A330 SRM 53-02-00 FIG 211.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,381 hrs · 8,320 cycles

C1 CHECK, DELAMINATION ON FLOOR PANEL 151HF BETWEEN FR 57.1 TO FR 58 & BETWEEN Y 140 TO Y 805. REPLACED FLOOR PANEL 151HF IAW A330 SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,381 hrs · 8,320 cycles

BC1 CHECK, CABIN FLOOR PANEL 151CF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW A330 SRM 53-02-00 FIGURE 211.

Part: MONITOR — SMOKE (SEAT 13E) · airframe 58,886 hrs · 8,245 cycles

SEAT 13C VIDEO MONITOR REPORTED TO HAVE SMOKE COMING FROM BEHIND THE SCREEN. MAINTENANCE FOUND SEAT 13C MONITOR CONNECTED AND OPERATIONAL. NOTED SEAT 13E TO BE DISCONNECTED. REPLACED MONITOR ASSEMBLY AT SEAT 13E AND OPERATES SATISFACTORY.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 58,708 hrs · 8,222 cycles

EXIT SIGN AT R2 DOOR FELL OUT OF ITS RECEPTACLE AND BROKE. MX RESECURED EXIT SIGN AT 2R.

Part: DAMPER — LOW PRESSURE (R4 DOOR ASSIST) · airframe 58,540 hrs · 8,200 cycles

AFT PAX DOOR R4 DOOR DAMPER CYLINDER IS ON YELLOW BAND. MX SERVICED R4 DOOR CYLINDER DAMPER. LEAK TEST OK.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 57,898 hrs · 8,118 cycles

EMERGENCY EXIT SIGN FELL OFF AT 2L. MX REPLACED SIGN.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 56,142 hrs · 7,892 cycles

AFTER ARRIVAL AT GATE, F/A REPORTED L1 DOOR SLIDE WILL NOT DISARM. MAINTENANCE REMOVED AND REPLACED L1 DOOR GIRT BAR AND SLIDER.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 56,097 hrs · 7,885 cycles

R4 DOOR ASSIST BOTTLE IS LOW. MAINTENANCE CHARGED EMERGENCY OPERATIONAL CYLINDER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,585 hrs · 7,818 cycles

BREAKAWAY FLASHLIGHT AT 4R INOPERATIVE. MAINTENANCE REPLACED BREAKAWAY FLASHLIGHT BATTERY. CHECKS GOOD.

Part: COVER — BROKEN (CABIN) · airframe 55,327 hrs · 7,779 cycles

L62 3RD EMERGENCY LIGHT COVER BROKEN BY 25F. MAINTENANCE REPLACED COVER AS REQUIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 53,724 hrs · 7,562 cycles

FLIGHT 721, FCO - CLT - PASSENGER REPORTED SLIGHT ELECTRICAL BURNING SMELL FROM VIDEO AT SEAT 31E TURNED OFF UNIT FOR DURATION OF FLIGHT. MAINTENANCE COULD NOT VERIFY. OPERATED SYSTEM AT NOTED SEAT CONTINUOUSLY NOTING NO ODOR. INSPECTED SEB'S AT LOCATION 30E/31E AND SEAT CABLING NOTING NO FAULTS. REPLACED MONITOR ASSEMBLY AT SEAT 31E AS PRECAUTION.

Part: LENS — BROKEN (CABIN) · airframe 52,862 hrs · 7,453 cycles

CLT - 1L DOOR NEAR HANDSET EXIT LENS BROKEN. REPLACED BROKEN EMERGENCY LENSE AT 1L DOOR. OK FOR SERVICE.

Part: COVER — OUT OF POSITION (CABIN) · airframe 52,439 hrs · 7,399 cycles

THE 1L GALLEY EMERGENCY LIGHT PLASTIC COVER MISSING ON WALL NEXT TO POSITION 2-12. MAINTENANCE FOUND AND REPOSITIONED PLASTIC COVER ON EMERGENCY LIGHT, OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 51,775 hrs · 7,314 cycles

THE 3L DOOR EXIT LIGHT COVER MISSING. MAINTENANCE RE-INSTALLED 3L DOOR EXIT LIGHT COVER. OK FOR SERVICE.

Part: BATTERY — FAULTY (CABIN) · airframe 51,658 hrs · 7,299 cycles

THE EPSU BATTERY AT DOOR 2L (14WL) FAULTED DURING TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU BATTERY 14WL AT DOOR 2L. OPERATIONAL CHECK IS NORMAL.

Part: COVER — MISSING (CABIN) · airframe 50,730 hrs · 7,182 cycles

WALL ON LEFT SIDE BEFORE REAR GALLEY EMERGENCY LIGHT COVER MISSING. MAINTENANCE REFITTED COVER.

Part: COVER — MISSING (CABIN) · airframe 50,274 hrs · 7,124 cycles

PLASTIC COVER ON EXIT SIGN 3L MISSING. MAINTENANCE REPLACED COVER.

Part: SIGN — BROKEN (CABIN) · airframe 50,054 hrs · 7,095 cycles

S2 CHECK - CEILING EXIT SIGN ABOVE R2 DOOR BROKEN. REPLACED CEILING EXIT SIGN ABOVE R2 DOOR.

Part: FITTING — FAILED (R4 DOOR) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION CONTROL UNIT 22DH FAILED BITE TEST ON AFT POSITION. REPLACED R4 DOOR AFT HEATED FITTING 26DH IAW AMM 30-46-34. PERFORMED CONTROL UNIT BITE TEST & ADJUSTED GIRT BAR FITTING IAW A330 AMM 30-46-00 & 52-11-00-820-801-A.

Part: FITTING — FAILED (R1 DOOR) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION CONTROL UNIT 4DH FAILED BITE TEST ON AFT POSITION. REPLACED R1 DOOR AFT HEATED FITTING 8DH IAW A330 AMM 30-46-34. PERFORMED CONTROL UNIT BITE TEST & ADJUSTED GIRT BAR FITTING IAW A330 AMM 30-46-00, 52-11-00-820-801-A.

Part: FITTING — FAILED (L2 DOOR) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION CONTROL UNIT 9DH FAILED BITE TEST ON AFT POSITION. REMOVED & REPLACED L2 DOOR AFT HEATED FITTING 13DH IAW AMM 30-46-34. PERFORMED CONTROL UNIT BITE TEST & ADJUSTED GIRT BAR FITTING IAW A330 AMM 30-46-00 & 52-11-00-820-801-A.

Part: FITTING — FAILED (L2 DOOR) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION CONTROL UNIT 9DH FAILED BITE TEST ON FORWARD POSITION. REPLACED L2 DOOR FORWARD HEATED FITTING 9DH IAW AMM 30-46-34. PERFORMED CONTROL UNIT BITE TEST & ADJUSTED GIRT BAR FITTING IAW A330 AMM 30-46-00 & 52-11-00-820-801-A.

Part: SIGN — BROKEN (CABIN) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - L3 EXIT DOOR CEILING EXIT SIGN 59WL BROKEN. REPLACED L3 EXIT DOOR CEILING EXIT SIGN 59WL IAW A330 AMM 33-51-17.

Part: FITTING — FAILED (L4 DOOR) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION CONTROL UNIT 25DH FAILED BITE TEST ON AFT POSITION. REPLACED L4 DOOR AFT HEATED FITTING 25DH IAW A330 AMM 52-13-31. PERFORMED L4 DOOR CONTROL UNIT BITE TEST & ADJUSTED GIRT BAR FITTING IAW A330 AMM 30-46-00 & 52-13-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 271LF BETWEEN FR74 TO FR75, Y2462. REPLACED FLOOR PANEL 271LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 271LF BETWEEN FR74 TO FR75, -Y2462. REPLACED FLOOR PANEL 271LF IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR40 TO FR47, Y450. REPLACED SEAT TRACK BETWEEN FR40 TO FR47, Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 242LF BETWEEN FR33 TO FR37, -Y2462. REPLACED FLOOR PANEL 242LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 262GG BETWEEN FR60 TO FR62 & BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 262GG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252EF BETWEEN FR37 TO FR37.4 & BETWEEN -Y2462 TO -Y1959. REPLACED FLOOR PANEL 252EF IAW A330 SRM 53-02-22 FIG 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR37.1 TO FR37.4, Y953. REPLACED SEAT TRACK BETWEEN FR37.1 TO FR37.4, Y953 IAW A330 SRM 53-00-15 FIG 101, 53-21-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR29 TO FR31, -Y953. REPAIRED SEAT TRACK BETWEEN FR29 TO FR31, -Y953 IAW A330 SRM 53-31-15 & 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261CH BETWEEN FR53.6 TO FR53.7, Y1580. REPLACED FLOOR PANEL 261CH IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR53.2 TO FR54, Y1959. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR54, Y1959 IAW A330 SRM 53-31-15 FIG 101, 51-44-11 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 262ZF BETWEEN FR57.1 TO FR58, BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 262ZF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR30 TO FR37, -Y953. REPLACED SEAT TRACK BETWEEN FR30 TO FR37, -Y953 IAW A330 SRM 51-42-11, 51-44-11 & 53-00-15.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CRACK ON FLOOR PANEL 251HG BETWEEN FR47 TO FR51, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 251HG IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR65, -Y2462. REPLACED SEAT TRACK AT FR65, -Y2462 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR53.2 TO FR53.4, -Y450. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR53.4, -Y450 IAW A330 SRM 53-30-00, 51-42-11, 51-44-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FORWARD CARGO FLOOR PANEL 132DG BETWEEN FR37.4 TO FR39.2, BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 132DG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR33 TO FR37, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL BETWEEN FR33 TO FR37, BETWEEN Y450 TO Y953 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR56 TO FR57.4, -Y450. REPLACED SEAT TRACK BETWEEN FR56 TO FR57.4, -Y450 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR55 TO FR56, Y2462. REPLACED SEAT TRACK BETWEEN FR55 TO FR56, Y2462 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR53 TO FR54, -Y1959. REPLACED SEAT TRACK BETWEEN FR53 TO FR54, -Y1959 IAW A330 SRM 51-42-11 & 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR30.5 TO FR37, Y953. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR37, Y953 IAW A330 SRM 51-42-11, 51-74-00 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR56 TO FR57, Y450. REPLACED SEAT TRACK BETWEEN FR56 TO FR57, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR33 TO FR37, BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL BETWEEN FR33 TO FR37, BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 241EF BETWEEN FR30 TO FR33, BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 241EF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR55 TO FR58, -Y1959. REPLACED SEAT TRACK BETWEEN FR55 TO FR58, -Y1959 IAW A330 SRM 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT PLATE BETWEEN FR74 TO FR75, Y2462. REPLACED SUPPORT PLATE BETWEEN FR74 TO FR75, Y2462 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11, 51-42-11, 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR57.4 TO FR60, -Y450. REPLACED SEAT TRACK BETWEEN FR57.4 TO FR60, -Y450 IAW A330 SRM 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON DOOR SILL BEAM SUPPORT PLATE AT FR75, Y2462. REPLACED DOOR SILL BEAM SUPPORT PLATE AT FR75, Y2462 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11, 51-42-11, 51-75-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT BEAM BETWEEN FR73A TO FR74, Y2462. REPLACED SUPPORT BEAM BETWEEN FR73A TO FR74, Y2462 IAW A330 SRM 51-42-11, 51-44-11, 53-41-14, 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR37.1 TO FR37.4, Y450. REPLACED SEAT TRACK BETWEEN FR37.1 TO FR37.4, Y450 IAW A330 SRM 53-21-15, 51-42-11 & 53-00-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR13A, -Y1456. REPLACED FLOOR SUPPORT AT FR13A, -Y1456 IAW A330 SRM 51-73-00, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR30.5 TO FR37.5, -Y2462. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR37.5, -Y2462 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11, 51-21-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR13A TO FR14, -Y1959. REPLACED FLOOR SUPPORT BETWEEN FR13A TO FR14, -Y1959 IAW A330 SRM 51-42-11, 53-11-14, 51-74-00, 51-72-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR56 TO FR57, Y450. REPLACED SEAT TRACK BETWEEN FR56 TO FR57, Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FORWARD CABIN FLOOR SUPPORT BETWEEN FR12A TO FR18, Y450. REPLACED FORWARD CABIN FLOOR SUPPORT BETWEEN FR12A TO FR18, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BETWEEN FR30.5 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR37, Y450 IAW A330 SRM 51-42-11, 51-74-00, 53-00-15 & 53-21-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR76, Y1477.8. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR76, Y1477.8 IAW A330 SRM 51-74-00, 53-41-14 FIG 101 SHT 2 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR61 TO FR65, -Y450. REPLACED SEAT TRACK BETWEEN FR61 TO FR65, -Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR30.5 TO FR37.5, -Y450. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR37.5, -Y450 IAW A330 SRM 53-00-15, 51-42-11 & 51-75-12.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CROSS BEAM FORWARD OF FR76, Y1447. REPLACED FLOOR SUPPORT CROSS BEAM FORWARD OF FR76, Y1447 IAW A330 SRM 51-42-11, 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR47 TO FR53.2, -Y450. REPLACED SEAT TRACK BETWEEN FR47 TO FR53.2, -Y450 IAW A330 SRM 53-31-15 FIG 101 & 51-42-11.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CRACK ON PROFILE BETWEEN FR80 TO FR82, -Y1447.8. REPLACED PROFILE BETWEEN FR80 TO FR82, -Y1447.8 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 272QF BETWEEN FR78 TO FR80, BETWEEN -Y450 TO -Y1947.8. REPLACED FLOOR PANEL 272QF IAW A330 SRM 53-02-00.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON PROFILE BETWEEN FR76 TO FR77, -Y2462. REPLACED PROFILE BETWEEN FR76 TO FR77, -Y2462 IAW A330 SRM 53-41-14, 51-44-11 & 51-42-11.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CRACK ON PROFILE BETWEEN FR80 TO FR82, Y1477.8. REPLACED PROFILE BETWEEN FR80 TO FR82, Y1477.8 IAW A330 SRM 51-42-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON Z-PROFILE BETWEEN FR75A TO FR77, Y2462. REPLACED Z-PROFILE BETWEEN FR75A TO FR77, Y2462 IAW A330 SRM 53-41-14 FIGURE 101, 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSSBEAM BETWEEN FR76 TO FR77, BETWEEN -Y450 TO -Y794.3. REPLACED CROSSBEAM BETWEEN FR76 TO FR77, BETWEEN -Y450 TO -Y794.3 IAW A330 SRM 53-41-14, 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON ANGLE PLATE AT FR80, -Y450. REPLACED ANGLE PLATE AT FR80, -Y450 IAW A330 SRM 53-41-14, 51-44-11 & 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSS BEAM AT FR73, -Y2462. REPLACED CROSS BEAM AT FR73, -Y2462 IAW A330 SRM 53-41-14, 51-44-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK RAIL BETWEEN FR40 TO FR41, Y2462. REPLACED SEAT TRACK RAIL BETWEEN FR40 TO FR41, Y2462 IAW A330 SRM 51-42-11, 53-31-15, 51-44-11 & 51-21-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON L4 DOOR SILL CENTER SUPPORT BETWEEN FR73A TO FR75A, S26L. REPLACED L4 DOOR SILL CENTER SUPPORT BETWEEN FR73A TO FR75A, S26L IAW A330 SRM 53-41-39, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR13 TO FR13A, Y230. REPLACED FLOOR SUPPORT BETWEEN FR13 TO FR13A, Y230 IAW A330 SRM 53-11-14 FIG 101, 51-42-11 & AIRBUS DRAWING F3114425.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 271HF BETWEEN FR73 TO FR76, BETWEEN Y794 TO Y1137. REPLACED FLOOR PANEL 271HF IAW A330 SRM 53-02-00, FIGURE 211.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - BROKEN FLOOR PANEL BETWEEN FR53.4 TO FR53.9, BETWEEN -Y1959 TO -Y2055.5. REPLACED FLOOR PANEL BETWEEN FR53.4 TO FR53.9, BETWEEN -Y1959 TO -Y2055.5 IAW A330 SRM 53-02-00, FIGURE 211.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CRACKED FLOOR PANEL 272HF BETWEEN FR73 TO FR76, BETWEEN -Y450 TO -Y794. REPLACED FLOOR PANEL 272HF IAW A330 SRM 53-02-00, FIGURE 211.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION AND LEVEL 2 FILIFORM CORROSION ON FLOOR PANEL 271GF BETWEEN FR73 TO FR76, BETWEEN Y450 TO Y794. REPLACED FLOOR PANEL 271GF IAW A330 SRM 53-02-00, FIGURE 211.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CRACKED AND LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL 271MF BETWEEN FR75 TO FR78, BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL 271MF IAW A330 SRM 53-02-00, FIGURE 211.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR74 TO FR75, -Y450. REPLACED SEAT TRACK BETWEEN FR74 TO FR75, -Y450 IAW A330 SRM 53-00-15 FIG 101 SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR71, Y450. REPLACED SEAT TRACK AT FR71, Y450 IAW A330 SRM 53-00-15 FIGURE 101 SHEET 2, SRM 51-42-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON ATTACH FITTING BETWEEN FR80 TO FR82, Y450. REPLACED ATTACH FITTING BETWEEN FR80 TO FR82, Y4509 IAW A330 SRM 53-41-14 FIG 14 SH 7.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIAITION CORROSION ON ANGLE PLATE BETWEEN FR80 TO FR82, BETWEEN -Y450 TO Y450. REPLACED ANGLE PLATE BETWEEN FR80 TO FR82, BETWEEN -Y450 TO Y450 IAW A330 SRM 53-41-14, FIGURE 14, SHEET 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR75.5, -Y1137.1. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR75.5, -Y1137.1 IAW A330 SRM 51-42-11, 53-41-14 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL ADAPTER SEAT TRACK BETWEEN FR72 TO FR73A, Y2462. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR75.5, -Y1137.1 IAW A330 SRM 51-42-11, 51-74-00 & 53-00-15.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR75.7 & BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL BETWEEN FR73 TO FR75.7 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR53.2, Y450. REPLACED SEAT TRACK AT FR53.2, Y4500 IAW A330 SRM 51-31-15 FIG 101 & SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSS BEAM AT FR17 BETWEEN -Y1952 TO -Y1456. REPLACED CROSS BEAM AT FR17 BETWEEN -Y1952 TO -Y1456 IAW A330 SRM 51-74-00 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR71 TO FR73 & BETWEEN -Y1456 TO -Y2462. REPLACED FLOOR PANEL BETWEEN FR71 TO FR73 & BETWEEN -Y1456 TO -Y2462 IAW A330 SRM 53-02-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSSBEAM BETWEEN FR75 TO FR76, BETWEEN -Y1137 TO -Y1447.8. REPLACED CROSSBEAM BETWEEN FR75 TO FR76, BETWEEN -Y1137 TO -Y1447.8 IAW A330 SRM 53-41-14 FIGURE 14, SHEETS 4 & 5, ITEM 205.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR75.7 & BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL BETWEEN FR73 TO FR75.7 & BETWEEN Y450 TO -Y450 IAW A330 SRM 51-31-15 FIG 101 & SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR PANEL BETWEEN FR78 TO FR80 & BETWEEN -Y450 TO -Y1447.8. REPLACED FLOOR PANEL BETWEEN FR78 TO FR80 & BETWEEN -Y450 TO -Y1447.8 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR78 TO FR80 & BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL BETWEEN FR78 TO FR80 & BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSS BEAM BETWEEN FR75 TO FR76, -Y1477.8. REPLACED CROSS BEAM BETWEEN FR75 TO FR76, -Y1477.8 IAW A330 SRM 53-41-14 FIG 101 & 51-42-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON CROSS BEAM AFT OF FR13A BETWEEN Y=0 TO Y450. REPLACED CROSS BEAM AFT OF FR13A BETWEEN Y=0 TO Y450 IAW A330 SRM 51-42-11, 51-74-00, 51-44-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR71 TO FR73 & BETWEEN Y1456 TO Y2462. REPLACED FLOOR PANEL BETWEEN FR71 TO FR73 & BETWEEN Y1456 TO Y2462 IAW A330 SRM 53-02-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR74 TO FR76, Y794.3. REPLACED FLOORBEAM BETWEEN FR74 TO FR76, Y794.3 IAW A330 51-44-11, 54-42-11 & 51-75-12.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DUMMY RAIL AT FR80, -Y450. REPLACED DUMMY RAIL AT FR80, -Y450 IAW A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR BEAM BETWEEN FR75 TO FR76, -Y1447.8. REPLACED FLOOR BEAM BETWEEN FR75 TO FR76, -Y1447.8 IAW A330 SRM 51-74-00, 53-41-14, 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON DOOR SILL BETWEEN FR74 TO FR75, Y2462. REPLACED DOOR SILL BETWEEN FR74 TO FR75, Y2462 IAW A330 SRM 53-41-14 FIGURE 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR76, Y2462. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR76, Y2462 IAW A330 SRM 53-41-14 FIGURE 101.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

2S CHECK - CRACK IN FLOORBEAM AFT OF FR12A BETWEEN Y=0 TO -Y450. REPLACED FLOORBEAM AFT OF FR12A BETWEEN Y=0 TO -Y450 IAW A330 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AFT OF FR13A, BETWEEN -Y953 TO -Y450. REPLACED FLOOR SUPPORT AFT OF FR13A, BETWEEN -Y953 TO -Y450 IAW A330 SRM 51-42-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON ATTACH FITTING BETWEEN FR75 TO FR76, Y1447.8. REPLACED ATTACH FITTING BETWEEN FR75 TO FR76, Y1447.8 IAW A330 SRM 51-42-11 & 53-41-14 FIG 101.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR80, Y450. REPLACED LONGERON BEAM BETWEEN FR75 TO FR80, Y450 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR13 TO FR13A, -Y730. REPLACED FLOOR SUPPORT BETWEEN FR13 TO FR13A, -Y730 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR14 TO FR17, -Y450. REPLACED FLOOR SUPPORT BETWEEN FR14 TO FR17, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT RAIL BETWEEN FR11 TO FR16A, -Y953. REPLACED FLOOR SUPPORT RAIL BETWEEN FR11 TO FR16A, -Y953 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR14A TO FR15, Y953. REPLACED FLOOR SUPPORT BETWEEN FR14A TO FR15, Y953 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR76 & BETWEEN Y1137 TO Y1447. REPLACED FLOOR PANEL BETWEEN FR73 TO FR76 & BETWEEN Y1137 TO Y1447 IAW TYPICAL REPAIR TR 330-5302-11-0330 & A330 SRM 51-21-11 & 51-75-12.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR74 TO FR76, BETWEEN -Y1137 TO -Y1447. REPLACED FLOOR PANEL BETWEEN FR74 TO FR76, BETWEEN -Y1137 TO -Y1447 IAW TYPICAL REPAIR 330-5302-11-0330 AND A330 SRM 51-21-11, 51-75-12.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR76, Y1447. REPLACED FLOOR PANEL BETWEEN FR73 TO FR76, Y1447 IAW TYPICAL REPAIR 330-5302-11-0330 AND A330 SRM 51-21-11, 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR53.3 TO FR53.9, Y2055.5. REPLACED SEAT TRACK BETWEEN FR53.3 TO FR53.9, Y2055.5 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION SEAT TRACK AT FR41, -Y450. REPLACED SEAT TRACK AT FR41, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - CORROSION ON FLOOR SUPPORT BETWEEN FR13A AND FR 15A. REPLACED FLOOR SUPPORT BETWEEN FR13A AND FR 15A IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION SEAT TRACK BETWEEN FR53.2 TO FR54, -Y450. REPLACED SEAT SEAT TRACK BETWEEN FR53.2 TO FR54, -Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION SEAT TRACK BETWEEN FR53.2 TO FR54, Y450. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR54, Y450 IAW A330 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION FLOOR SUPPORT BETWEEN FR16A TO FR17, -Y1959. REPLACED FLOOR SUPPORT BETWEEN FR16A TO FR17, -Y1959 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR39.1 TO FR40, Y450. REPLACED SEAT TRACK BETWEEN FR39.1 TO FR40, Y450 IAW A330 SRM 53-31-01 FIG 101, SRM 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR78, Y450. REPLACED LONGERON BEAM BETWEEN FR75 TO FR78, Y450 IAW A330 53-41-14 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR39 TO FR39.1, Y450. REPLACED SEAT TRACK BETWEEN FR39 TO FR39.1, Y450 IAW A330 53-31-15 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION FLOOR SUPPORT BEAM BETWEEN FR73 TO FR75, Y450. REPLACED FLOOR SUPPORT BEAM BETWEEN FR73 TO FR75, Y450 IAW A330 SRM 53-00-45 103 FIG 101, 51-42-11 & 51-44-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4, BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 252CF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 232CG BETWEEN FR26.4 TO FR31, BETWEEN -Y953 TO -Y1436. REPLACED FLOOR PANEL 232CG IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR80, Y1137.1. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR80, Y1137.1 IAW A330 SRM 51-42-11 & 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR32 TO FR34, -Y1552.5. REPLACED SEAT TRACK BETWEEN FR32 TO FR34, -Y1552.5 IAW A330 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR75 TO FR82, -Y450. REPLACED FLOORBEAM BETWEEN FR75 TO FR82, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR19 TO FR22, BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL BETWEEN FR19 TO FR22, BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN -Y1959 TO -Y2462. REPLACED FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN -Y1959 TO -Y2462 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN Y1456 TO Y1959 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL BETWEEN FR26.4 TO FR31, BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR78, -Y794.3. REPLACED LONGERON BEAM BETWEEN FR75 TO FR78, -Y794.3 IAW A330 53-00-14 FIG 101 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR19 TO FR22, BETWEEN Y450 TO -Y450. REPLACED FLOOR PANEL BETWEEN FR19 TO FR22, BETWEEN Y450 TO -Y450 IAW A330 SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON LONGERON BEAM BETWEEN FR73 TO FR74, -Y1278. REPLACED LONGERON BEAM BETWEEN FR73 TO FR74, -Y1278 IAW A330 SRM 53-44-14 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR73 TO FR74, Y794.3. REPLACED FLOOR SUPPORT BETWEEN FR73 TO FR74, Y794.3 IAW A330 SRM 51-44-11, 51-72-11, 53-41-14 FIG 103 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR73 TO FR74, -Y1278. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y1278 IAW A330 SRM 51-42-11, 51-21-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR78, Y=0. REPLACED FLOOR SUPPORT AT FR78, Y=0 IAW A330 SRM 51-42-11, 51-44-11 & 51-74-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR73 TO FR74, Y1278. REPLACED FLOOR SUPPORT BETWEEN FR73 TO FR74, Y1278 IAW A330 SRM 53-41-14 FIG 101 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR76, Y=0. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR76, Y=0 IAW A330 SRM 51-42-11 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR53.8 TO FR53.9, Y1959. REPLACED SEAT TRACK BETWEEN FR53.8 TO FR53.9, Y1959 IAW A330 SRM 53-31-15 FIG 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT BETWEEN FR73 TO FR74, Y794.3. REPLACED FLOOR SUPPORT BETWEEN FR73 TO FR74, Y794.3 IAW A330 SRM 53-41-14 FIG 101 & 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILFORM CORROSION ON LONGITUDINAL BEAM BETWEEN FR78 TO FR80, -Y450. REPLACED LONGITUDINAL BEAM BETWEEN FR78 TO FR80, -Y450 IAW A330 SRM 53-41-14 FIG 103.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILFORM CORROSION ON LONGITUDINAL BEAM BETWEEN FR73 TO FR74, -Y450. REPLACED LONGITUDINAL BEAM BETWEEN FR73 TO FR74, -Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON DOOR SILL BETWEEN FR73A TO FR75A, -Y1959. REPLACED DOOR SILL BETWEEN FR73A TO FR75A, -Y1959 IAW A330 SRM 53-41-14 FIG 103.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR65 TO FR67, Y450. REPLACED SEAT TRACK BETWEEN FR65 TO FR67, Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR59 TO FR60, Y450. REPLACED SEAT TRACK BETWEEN FR59 TO FR60, Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK AT FR63, Y450. REPLACED SEAT TRACK AT FR63, Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR57.1 TO FR59, Y450. REPLACED SEAT TRACK BETWEEN FR57.1 TO FR59, Y450 IAW A330 SRM 53-00-15 FIG 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,051 hrs · 7,093 cycles

S2 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT FR78, Y794.3. REPLACED FLOOR SUPPORT AT FR78, Y794.3 IAW A330 SRM 53-41-14 FIG 103.

Part: COVER — DETACHED (CABIN) · airframe 50,041 hrs · 7,091 cycles

FRA - 11B EMERGENCY LIGHT COVER OFF - LIGHT PUSHED IN. MAINTENANCE RE-INSTALLED 11B LIGHT AND COVER.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 49,520 hrs · 7,024 cycles

STRONG MUSTY ODOR REPORTED BY FLIGHT ATTENDANTS. PACK ON HIGH ODOR DISSIPATES. MAINTENANCE PERFORMED J/C 33L00021001 - NO DISCREPANCIES. NOTED ON GROUND. NOTE: HEPA FILTER(8EA) REPLACEMENT PROGRAMMED. PHL MAINTENANCE REMOVED AND REPLACED APU ASSEMBLY AND HEPA FILTERS.

Part: FILTER — DIRTY (LAVATORY) · airframe 48,871 hrs · 6,941 cycles

CLT FLT 721 EN ROUTE FCO TO CLT. STRONG SMELL OF URINE IN VICINITY OF AND FORWARD OF AFT LEFT LAV BY 4L DOOR. MAINTENANCE FOUND BOTH WASTE TANK WASTE SEPARATOR FILTERS VERY DIRTY AND VERY STRONG URINE SMELL COMING FROM BOTH SEPARATORS. ALSO O-RING WAS MISPLACED FOR AFT TANK WASTE SEPARATOR. CLEANED BOTH WASTE SEPARATOR HOUSINGS AND REPLACED FILTERS AND O-RINGS FOR BOTH WASTE SEPARATORS. OP'S CHECK TOILET SYSTEM. ON LEAKS OR ODOR OBSERVED FROM INSIDE CABIN OR IN LOWER COMPARTMENT IN AFT BAGGAGE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,524 hrs · 6,898 cycles

LHR - DOOR 1R EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED EPSU AT 1R DOOR, OPS CHECK GOOD. REMOVED MEL 33-51-01D C/N 0643A00. NOTIFIED MOC.

Part: ACM — SEIZED (NR 1) · airframe 48,446 hrs · 6,887 cycles

FLIGHT 732, A/C PACK 1 OVERHEAT, STRONG ODOR ON SHORT FINAL. RESET AND REOCCURED AFTER LANDING. MAINTENANCE REMOVED AND REPLACED LEFT AIR CYCLE MACHINE REF AMM 21-52-21-400-801. OPERATIONAL AND LEAK CHECKS ARE SATISFACTORY.

Part: COVER — OUT OF POSITION (CABIN) · airframe 48,318 hrs · 6,869 cycles

MAN - COVER CAME OFF SEAT LEVEL EMERGENCY LIGHT AT 28GH. MAINTENANCE EMERGENCY LIGHT COVER REFITTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,007 hrs · 6,830 cycles

MAN - FLASHLIGHT AT DOOR 1L INOP. BATTERY CHANGED, NOW OK.

Part: PROBE — FAILED (RT ENGINE)

PHL FLT 732 EN ROUTE CLT TO LGW. DURING CRUISE FLIGHT, THE CREW REPORTS: "NR 2 EPR FAILED, IN N1 MODE LARGE DIFFERENCE IN THRUST LEVERS." AN OPERATIONAL DECISION WAS MADE NOT TO TAKE AIRCRAFT INTO ETOPS ENVIRONMENT WITH THIS CONDITION. THE FLIGHT DIVERTED TO PHL, DECLARED AN EMERGENCY DUE TO THE OVERWEIGHT CONDITION OF THE AIRCRAFT, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE P2/T2 PROBE ON THE RIGHT ENGINE.

Part: RIB — CRACKED (RT WING) · airframe 47,213 hrs · 6,715 cycles

BFM - MOD VISIT - CRACKS AT RIGHT WING VERTICAL ANGLE CHORD AT FR42 RIB 1 AT FASTNER HOLES NR 7 & NR 8. REPAIRED RIGHT WING VERTICAL ANGLE CHORD AT FR42 RIB 1 IAW EA 134473.

Part: RIB — CRACKED (LT WING) · airframe 47,213 hrs · 6,715 cycles

BFM - MOD VISIT - CRACKS AT LEFT WING VERTICAL ANGLE CHORD AT FR42 RIB 1 AT FASTENER HOLES NR 7, 8 & 10. REPAIRED LEFT WING VERTICAL ANGLE CHORD AT FR42 RIB 1 IAW AIRWAYS EA 134473.

Part: FASTENER — LOOSE (CENTER WING) · airframe 47,213 hrs · 6,715 cycles

BFM - TRACES OF FUEL HAVE BEEN FOUND IN THE CENTER WING DRY BAY OF A330-300 AIRCRAFT AT RIB 1. AS A RESULT OF THIS AN INSPECTION WAS PERFORMED ON THIS AIRCRAFT & FASTENERS WERE FOUND LOOSE & LEAKING AT FR42 LEFT & RIGHT SIDE AT RIB 1. BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102841A & 102876A.

Part: WIRE — DAMAGED (CABIN) · airframe 47,213 hrs · 6,715 cycles

BFM - MOD - 6402008 - SEAT 31AB EMERGENCY LIGHT IS INOP. REPAIRED WIRE ON CONNECTORS 5450VCA41 PIN C IAW A330 ESPM 20-48-24. OPS CHECK GOOD IAW A330 AMM 33-51-00.

Part: WIRE — DAMAGED (CABIN) · airframe 47,213 hrs · 6,715 cycles

BFM - MOD - 6402007 - SEAT 31HG EMERGENCY LIGHT IS INOP. REPAIRED WIRE ON CONNECTORS 5450VCA42 PIN B & C IAW A3330 ESPM 20-48-24. OPS CHECK GOOD IAW A330 AMM33-51-00.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE EPSU BATTERY AT L2 DOOR WAS INOPERATIVE. REMOVED AND REPLACED THE EPSU BATTERY AT THE L2 DOOR.

Part: WIRE HARNESS — DEFECTIVE (CABIN)

PHL - THE EMERGENCY LIGHT HARNESSES AT SEAT ROWS TWO AND FIVE ARE INOPERATIVE. REPLACED EMERGENCY LIGHT HARNESSES AT SEAT ROWS TWO AND FIVE.

Part: EPSU — INOPERATIVE (CABIN)

PHL - THE R2 DOOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED BATTERY SUPPLY UNIT AT R2 DOOR POSITION. SHOP ACTION PENDING. (OPEN)

Part: SMOKE DETECTOR — INOPERATIVE (CABIN)

PHL - L73 SMOKE DET INOP. MAINTENANCE REPLACED L73 SMOKE DET.

Part: CONTROL UNIT — FAULTY (SMOKE DETECTION)

PHL - FLT 704 - EN ROUTE CLT TO FRA. ATTEMPTED REBOOT OF IN-FLIGHT ENTERTAINMENT SYSTEM IN FLIGHT AND GOT AN AUTO-SHUTDOWN DUE TO BULK AVIONICS SMOKE LIGHT (INDICATION). THIS CAUSED OVERHEAD LIGHTS AND CALL BELLS TO FAIL. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. PERFORMED A RESET ON SDCU ONE AND SDCU TWO. REMOVED AND REPLACED SMOKE DETECTION CONTROL UNIT (SDCU).

Part: WINDSHIELD — CRACKED (COCKPIT)

FCO - FLT 719 - FCO TO PHL. THE FIRST OFFICER'S OUTER, MID WINDOW CRACKED, DEVELOPED DURING CRUISE FLT AT FLT LEVEL 350. RETURNED TO FCO. REMOVED AND REPLACED F/O WINDSHIELD.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - EMERGENCY CAP CHECK FAILED ON BATTERY R4. REPLACED BATTERY AT R4.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - EMERGENCY CAP CHECK FAILED ON BATTERY L4. REPLACED BATTERY AT L4.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - EMERGENCY CAP CHECK FAILED ON BATTERY R3. REPLACED BATTERY PACK AT R3.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE BATTERY FOR EPSU L3 FAILED TEST. REPLACED BATTERY ON EPSU L3.

Part: BATTERY — DISCHARGED (CABIN)

PHL - THE BATTERY FOR EPSU R1 FAILED TEST. REPLACED BATTERY ON EPSU R1.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

PHL - THE L1 DOOR AMBER YELLOW PHYSICALLY ARMED ON THE FLIGHT ATTENDANT PANEL L1. THE L1 DOOR ASSIST BOTTLE WAS SERVICED.

Part: CYLINDER — LOW PRESSURE (L1 DOOR)

CDG - THE L1 DOOR ASSIST CYLINDER PRESSURE IS LOW IN YELLOW BAND. THE L1 DOOR ASSIST CYLINDER WAS SERVICED.

Part: CYLINDER — LOW PRESSURE (L1 DOOR)

CLT - THE L1 DOOR ASSIST PRESSURE WAS FOUND LOW. THE L1 DOOR ASSIST WAS SERVICED TO THE PROPER PRESSURE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

PHL - THE CIDS PANEL DOES NOT INDICATE THE L1 DOOR ARMED WHEN IT IS. THE ECAM DOOR PAGE INDICATES SLIDE ARMED. THE DOOR ASSIST BOTTLE FOR THE L1 DOOR WAS SERVICED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FORWARD GALLEY FLASHLIGHT RED LIGHT IS NOT FLASHING. THE L1 DOOR FLASHLIGHT BATTERY WAS REPLACED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

LGW - L1 DOOR ASSIST BOTTLE SHOWS LOW PRESS-YELLOW BAND AREA. MAINTENANCE RESTORED BOTTLE PRESSURE TO GREEN BAND AREA IAW MM 52-10-00-03-600-802.

Part: RELAY — FAILED (CABIN) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - EEL - EMERGENCY LIGHT SYSTEM AUTOMATIC CONTROL CIRCUIT FAILED ON TEST. ACCOMPLISHED TROUBLESHOOTING IAW A330 AWM 24-24-02, REPLACED RELAY 26XE IAW A330 SWPM 20-46-50.

Part: RELAY — FAILED (CABIN) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - EEL - EMERGENCY LIGHT SYSTEM AUTOMATIC CONTROL CIRCUIT FAILED ON TEST. ACCOMPLISHED TROUBLESHOOTING IAW A330 AWM 24-24-02, REPLACED RELAY 12XE IAW A330 SWPM 20-46-50.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR42, -Y2462. REPLACED SEAT TRACK AT FR42, -Y2462 IAW A330 SRM 53-37-15 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR38 TO FR39.2, Y450. REPLACED SEAT TRACK BETWEEN FR38 TO FR39.2, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR38 TO FR39.2, Y450. REPLACED CORROSION ON SEAT TRACK BETWEEN FR38 TO FR39.2, Y450 IAW A330 SRM 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR59 TO FR62, Y2462. REPLACED SEAT TRACK BETWEEN FR59 TO FR62, Y2462 IAW A330 SRM 53-00-15 & 51-42-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR44 TO FR47, -Y450. REPLACED SEAT TRACK BETWEEN FR44 TO FR47, -Y450 IAW A330 SRM 53-31-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR53.2 TO FR54, Y450. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR54, Y450 IAW A330 SRM 53-31-15.

Part: PIN — CORRODED (RT MLG) · corrosion level 2 · airframe 37,208 hrs · 5,381 cycles

BFM - C2 - MAJOR REPAIR - LEVEL 2 CORROSION ON RIGHT MAIN LANDING GEAR PINTLE PIN & CAD PLATING IS WORN. REPLACED RIGHT MAIN LANDING GEAR PINTLE PIN IAW US AIRWAYS TASK CARD 33L74032001.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 37,208 hrs · 5,381 cycles

BFM - C2 CHECK - EEL - EMERGENCY EXIT LIGHT AT SEAT 6A FAILED OPERATIONAL CHECK. REPAIRED EMERGENCY EXIT LIGHT WIRING AT SEAT 6A AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW A330 ESPM 20-53-20 AND A330 AMM 33-15-38.

Part: SLIDE — FAULTY (R3 DOOR)

LHR - MAINTENANCE REPORTED LOW PRESSURE FOR THE R3 DOOR. MEL 23-73-02E WAS ASSIGNED. FURTHER TROUBLESHOOTING ON 12/24/08 BY PHL MAINTENANCE PER TSM 25-62-00-810-801, PER STEP 3B(3)(A), FOUND THE R3 DOOR SLIDE AT FAULT. REMOVED AND REPLACED SLIDE PER AMM 25-62-42-04. CHECKS OK. CLEARED MEL 23-73-02E.

Part: UPLOCK — FAULTED (MLG)

PHL FLT 734 PHL TO MAN. ON TAKEOFF AND LANDING GEAR RETRACTION, THE NOSE GEAR DOORS DID NOT CLOSE. THE CREW RECYCLED THE GEAR AND THE DOORS INDICATED PROPERLY CLOSED. DUE TO THE FOLLOW ON MAINTENANCE ACTION REQUIRED UPON LANDING IN MAN, AN OPERATIONAL DECISION WAS MADE TO RETURN TO PHL THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE THE PROBLEM. AFTER ADDITIONAL TROUBLESHOOTING, A FAULT WAS FOUND WITH THE RIGHT MAIN GEAR UPLOCK ASSEMBLY. MAINTENANCE REPLACED THE RIGHT MAIN GEAR UPLOCK ASSEMBLY.

Part: EPSU — DISCHARGED (CABIN)

PHL - DOOR 2L EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REPLACED THE DOOR 2L EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (A)

Part: ACTUATOR — FAILED (TE FLAPS)

MAD FLT 740 ENROUTE PHL TO MAD. DURING APPROACH, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. THE LEADING EDGE FLAPS OPERATED NORMALLY. THE FLIGHT MADE A MISSED APPROACH AND THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING (B) MAINTENANCE REPLACED THE NUMBER TWO, LEFT HAND FLAP ROTARY ACTUATOR (FIN 5022CU). OPERATIONALLY CHECKS OK. [SUPP CLOSED](B)

Part: FLAP SYSTEM — MALFUNCTIONED (WING)

MAD - FLT 740 EN ROUTE PHL TO MAD. DURING APPROACH, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. THE LEADING EDGE FLAPS OPERATED NORMALLY. THE FLIGHT MADE A MISSED APPROACH AND THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO TORQUE LIMITER INDICATORS TRIPPED. PERFORMED OPERATIONAL CHECKS AND FOUND OK. OK FOR CONTINUED SERVICE. (S)

Part: WIRE HARNESS — FAULTY (NR 1 ENGINE)

PHL - FLT 754 EN-ROUTE PHL TO CDG. THE AIRCRAFT FAILED THE VERIFICATION FLIGHT FOR AN ENGINE 1 EGT INDICATION INOPERATIVE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE 1 EGT WIRE HARNESS. OPERATIONALLY CHECKS OK.

Part: ACTUATOR — FAILED (RAM AIR INLET) · airframe 31,675 hrs · 4,620 cycles

FLIGHT 718, PHL-FCO: CREW REPORTED THAT THE RIGHT PACK TEMPERATURE WOULD INCREASE ANYTIME THE THROTTLES WERE ADVANCED. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE RIGHT RAM AIR INLET ACTUATOR.

Part: SLIDE — FAILED (L2 DOOR) · airframe 31,612 hrs · 4,610 cycles

DURING OPERATIONAL CHECK OF L2 DOOR SLIDE, THE SLIDE FAILED TO MAINTAIN PRESSURE DUE TO A HOLE IN THE LOWER RIGHT SIDE OF THE SLIDE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY.

Part: EPSU — NO TEST (EMERGENCY LIGHT) · airframe 26,243 hrs · 3,871 cycles

DURING ACCOMPLISHMENT OF EMERGENCY LIGHTS TEST, MAINTENANCE FOUND EPSU'S AT POSITIONS 3L AND 4L NOT PASSING TEST. REPLACED BOTH EPSU'S. NO FURTHER FAULTS.

Part: COMPUTER — FAILED (FLT MANAGEMENT) · airframe 26,181 hrs · 3,863 cycles

FLIGHT 782, PHL-FRA: EN ROUTE, FMGEC 1 FAILED. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE NUMBER 1 FMGEC. NO FURTHER FAULTS.