N278AY

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 85,002 hrs · 11,841 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR ATTACHMENT RETRACT MECHANISM SUPPORT RIB FITTING AT STATION 2913 AND RIB 5. REPAIRED SUPPORT RIB FITTING PER EA 301699.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 85,002 hrs · 11,841 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON REPAIRED WING MAIN LANDING GEAR ATTACHMENT SUPPORT RIB FITTING AT STATION 2913 AND RIB 5. REPAIRED SUPPORT RIB FITTING PER EA 301581.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 85,002 hrs · 11,841 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR ATTACHMENT SUPPORT RIB FITTING AT STATION 2913 AND RIB 5. REPAIRED SUPPORT RIB FITTING PER EA 301583.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 85,002 hrs · 11,841 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE SKIN EXISTING REPAIR DOUBLER IS DEBONDED BETWEEN RIB 12-13 AND 12 INCHES FROM THE TRAILING EDGE . REPAIRED FLAP LOWER SURFACE SKIN PER SRM 57-54-00-300-005 AND EA 265778B.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 83,686 hrs · 11,650 cycles

AIRCRAFT NOT GROUNDED: ROW 8 LIGHT FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AT SEAT 8C. IAW CMM 25-23-54. OPS CK OK.

Part: SENSE LINE — LEAKING (BLEED SYSTEM) · airframe 82,714 hrs · 11,525 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF ENGINE BLEED SYSTEM ISSUES. FLIGHT WAS OVERWEIGHT FOR LANDING, LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND SENSE LINE LEAK. REMOVED AND REPLACED PRV SENSE LINE IAW AMM. BLEED SYSTEM OPS CKS NORMAL IAW AMM 36-11-00-710-810-A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 81,978 hrs · 11,419 cycles

L3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW MM 52-10-00-600-802-A, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: ATTACH FITTING — OUT OF ADJUST (GIRT BAR) · airframe 81,639 hrs · 11,365 cycles

MAINTENANCE REPORTED THAT THE PASSENGER DOOR FITTING, AT THE AFT POSITION, DID NOT PASS A TEST. REMOVED AND REPLACED GIRT BAR FITTING IAW AMM 30-46-11-400-801-A, STEP 3A(1)(2), B THRU 4A(1)(A)(2), B, C. ADJUSTMENT OK.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 81,266 hrs · 11,305 cycles

R2 DOOR SLIDE LOW PRESSURE DISPLAYED ON CIDS. MAINTENANCE REPLACED THE DOOR SLIDE ASSEMBLY IAW JC 33L00025001, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 80,427 hrs · 11,182 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR FLASHLIGHT LED WOULD NOT FLASH. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD MAINTENANCE PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 78,930 hrs · 10,997 cycles

AIRCRAFT WAS NOT GROUNDED. 4R FLASHLIGHT INOPERATIVE. REPLACED BATTERY PER AMM 33-51-11. OPERATIONS CHECK OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 77,236 hrs · 10,780 cycles

EMERGENCY LIGHT LENS MISSING AT 34G AND 37G. REPLACED THE EMERGENCY LIGHTS ASSEMBLIES IAW AMM 33-00-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 77,236 hrs · 10,780 cycles

L3 DOOR FLIGHT ATTENDANT STATION LOWER FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY IAW AMM 25-65-00.

Part: LENS — UNSECURE (CABIN) · airframe 76,909 hrs · 10,728 cycles

AIRCRAFT WAS NOT GROUNDED. 2R DOOR EMERGENCY EXIT LIGHT COVER CAME OFF. INSTALLED 2R EXIT SIGN LENS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 76,681 hrs · 10,691 cycles

MID GALLEY LEFT SIDE EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED THE CONNECTOR.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS)

DURING OPERATIONAL TESTS OF THE EMERGENCY LIGHT POWER SUPPLY. THE TEST DID NOT PASS. REPLACED EPSU.

Part: BOTTLE — INOPERATIVE (EMERGENCY EXIT) · airframe 76,510 hrs · 10,657 cycles

EMERGENCY EXIT R3 DOOR DAMPER DOES NOT WORK IN PASSENGER CABIN . REPLACED EMERGENCY DOOR DAMPER.

Part: FLOOR PANEL — CRACKED (PAX CABIN)

AIRCRAFT IN BASE MAINTENANCE. CRACKED FLOOR PANEL 272KF IN PASSENGER CABIN. REPLACED FLOOR PANEL 272KF IN PASSENGER CABIN EA 275873.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN)

DELAMINATED FLOOR PANEL 271NF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW EA 275858, AND SRM 53-02-00-300-010.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 30 TO 37.1, +Y1959. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53275849.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON TOP LAYER OF FLOOR PANEL 252GF IN PASSENGER CABIN. MAINTENANCE REPLACED FLOOR PANEL 252GF IN PASSENGER CABIN PER A330 SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 262MF IN PASSENGER CABIN. REPAIRED FLOOR PANEL 262MF IN PASSENGER CABIN PER A330 SRM 53-02-00-300-010 PARAGRAPH 2B.

Part: PIN — CORRODED (BS 732-1469) · airframe 76,510 hrs · 10,657 cycles

CORROSION TO UPPER PIN BETWEEN BS 732 TO 1469, BETWEEN RIBS 2 AND 3. REPLACED THE PIN IAW EA 275970.

Part: NUT — CORRODED (ZONE 700) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF UPPER CARDAN NUT ON RIGHT HAND MAIN LANDING GEAR SIDE STAY BETWEEN STA 732 TO STA 1469 BETWEEN RIB 2 AND RIB 3. REPLACED UPPER CARDAN NUT PER EA 275970.

Part: STRAP — CORRODED (FRAMES 74-75) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON FLOOR STRUCTURE ANGLE AT LEVEL STGR 26L AND BTW FR74 AND FR75 AT AFT GALLEY AREA. REPLACED STRAP PER SRM A330 51-72-11-911-001.

Part: PLATE — CORRODED (FRAME 76) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN CHECK: CORRODED PLATE AT BUTT LINE -Y1447.3, BODY STATION FR76 AT AFT GALLEY AREA. REPLACED PLATE AT AFT GALLEY AREA PER A330 SRM 51-72-11 AND A330 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF FLOORBEAM BETWEEN FR 73 TO FR 74 AT RIGHT BUTTLINE -YB. REPLACED FLOORBEAM BETWEEN FR 73 TO FR 74 AT RIGHT BUTTLINE -YB PER SRM 51-72-11, 51-42-11 AND DRAWINGS F53478008, F53478018.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FLOOR STRUCTURE ANGLE AT STRINGER 26L AND BETWEEN FR 75 & FR7 6 AT AFT GALLEY AREA. REPLACED FLOOR STRUCTURE ANGLE AND FASTENERS SRM 51-72-11, 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 221CF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY FLOORBEAM AT -Y1959 FRAME 17. REMOVED AND REPLACED FALSE TRACK (FLOORBEAM) BETWEEN FRAME 12A AND FRAME 18 PER SRM 51-72-11 AND DRAWING F53111248.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 242SF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (FRAMES 39-40) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 251RF BETWEEN FR 39.2 TO FR 40 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450. REPLACE FLOOR PANEL 251RF BETWEEN FR 39.2 TO FR 40 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FLOOR STRUCTURE BETWEEN FR73 & FR74 AND +Y1250 AT AFT GALLEY AREA. REPLACED FLOOR STRUCTURE PER SRM 51-72-11 AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 242DF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 242GF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 231JF, BETWEEN FRAMES 25 TO 26.1, Y1456 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672653.

Part: FLOOR PANEL — DELAMINATED (FRAMES 35-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 241RF BETWEEN FR 35 TO FR 37 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 241RF BETWEEN FR 35 TO FR 37 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR SUPPORT — CORRODED (FRAME 80) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT +Y794.3 AT FRAME 80 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 262GG IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (FRAMES 39-40) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 251UF BETWEEN FR 39.2 TO FR 40 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 251UF BETWEEN FR 39.2 TO FR 40 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y1959 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 242CF IN PASSENGER CABIN. REPLACED FLOOR PANEL IAW SRM 53-02- 00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251KF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 231XF, BETWEEN FRAMES 26.1 AND 26.4, Y1456 TO Y953. 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 76,510 hrs · 10,657 cycles

DELAMANATION ON FLOOR PANEL 232DF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 231F BETWEEN FR 19 TO FR 22 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 231F BETWEEN FR 19 TO FR 22 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 242HF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE -Y1456 TO LEFT BUTTLINE -Y953. REPLACED FLOOR PANEL 242HF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE -Y1456 TO LEFT BUTTLINE -Y953 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF SEAT TRACK FLOOR STRUCTURE BETWEEN FR 30 TO FR 37.1 AT LEFT BUTTLINE +Y2462. REPLACED SEAT TRACK FLOOR STRUCTURE BETWEEN FR 30 TO FR 37.1 AT LEFT BUTTLINE +Y2462 PER SRM 51-72-11 AND DRAWINGS F53275848, F53275795.

Part: WEB — CRACKED (FRAME 75) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENENACE. CRACKED WEB T FR75 AND +Y2462 AT STGR 26 LEFT AT AFT GALLEY AREA. REPLACED WEB PER SRM 51-72-11, 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 232SF BETWEEN FRAMES 25 AND 26.1, Y1456 TO Y953. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY AUXILIARY BEAM. REPLACED AUXILIARY BEAM PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF THE FLOOR PANEL 232MF, BETWEEN FRAMES 22 AND 25 AT -Y953 TO -Y1456. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 37-69) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION TOP LAYER FLOOR PANEL 261NH BETWEEN FR 67 TO FR 69 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 261NH BETWEEN FR 67 TO FR 69 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 232N BETWEEN FR 22 TO FR 25 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -1959. REPLACED FLOOR PANEL 232N BETWEEN FR 22 TO FR 25 AT RIGHT BUTTLINE -Y1456 TO RIGHT BUTTLINE -1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 251TG IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02- 00-300-009.

Part: FLOORBEAM — CORRODED (FRAME 74) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CRACKED AND CORRODED FLOORBEAM AT FRAME 74, +1547.8. REPAIRED THE FLOORBEAM IAW SRM A330 53-00-14-300-002.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FOUND IN TOP LAYER FLOOR PANEL 232XF OF PASSENGER CABIN. REPLACED FLOOR PANEL SRM 53-02-00-300-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON PASSENGER CABIN SEAT TRACK AT -Y1959, BETWEEN FR 32 AND FR 34. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275849.

Part: SEAT TRACK — CORRODED (FRAMES 35-37) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORROSION ON THE SEAT TRACK BETWEEN FRAMES 35 TO 37, +Y1556. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 231TF BETWEEN FRAMES 25 & 26.1, Y1456 TO Y1959. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 241HF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456. REPLACED FLOOR PANEL 241HF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: BEAM — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF AUXILIARY BEAM BETWEEN FR 75 AND FR 76 AT STRINGER 26L TO LEFT BUTTLINE +YB TO LEFT BUTTLINE +YA. REPLACED AUIXILLARY BEAM BETWEEN FR 75 AND FR 76 AT STRINGER 26L TO LEFT BUTTLINE +YB TO LEFT BUTTLINE +YA PER SRM A330 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION TOP LAYER FLOOR PANEL 252GF BETWEEN FR 37.4 TO FR 39 AT RIGHT BUTTLINE -Y53 TO RIGHT BUTTLINE -Y450. REPLACED FLOOR PANEL 252GF BETWEEN FR 37.4 TO FR 39 AT RIGHT BUTTLINE -Y53 TO RIGHT BUTTLINE -Y450 PER A330 SRM 53-0-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAME 53) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED FLOOR PANEL 262DF BETWEEN FR 53.4 TO FR 53.7 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 262DF BETWEEN FR 53.4 TO FR 53.7 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAME 53) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 251XG BETWEEN FR 53.2 TO FR 53.4 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462. REPLACED FLOOR PANEL 251XG BETWEEN FR 53.2 TO FR 53.4 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 30-33) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 241CF BETWEEN FR 30 TO FR 33 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 241CF BETWEEN FR 30 TO FR 33 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 262VG IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (FRAMES 35-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 242RF BETWEEN FR 35 TO FR 37 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456. REPLACED FLOOR PANEL 242RF BETWEEN FR 35 TO FR 37 AT RIGHT BUTTLINE -Y1959 TO RIGHT BUTTLINE -Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: WEB — CRACKED (FRAME 75) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENACE. CRACKED WEB, FRAME 75+13 INCHES, -Y2462 IN THE AFT GALLEY AREA. REPLACED THE WEB IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF FLOORBEAM (TRACK) STRUCTURE BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE +Y1456. REPLACED FLOORBEAM (TRACK) STRUCTURE BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE +Y1456 PER SRM 51-72-11 AND DRAWING F53275849.

Part: FLOOR SUPPORT — CORRODED (FRAME 30) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT AT FRAME 30 AND Y 0 IN PASSENGER CABIN. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FRAMES 31-32) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 242EF BETWEEN FR 31 TO FR 32 AT RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959. REPLACED FLOOR PANEL 242EF BETWEEN FR 31 TO FR 32 AT RIGHT BUTTLINE -Y2462 TO RIGHT BUTTLINE -Y1959 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261PF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 232LF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 231CF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 232GF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FRAMES 39) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 251LF BETWEEN FR 39 TO FR 39.2 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 251LF BETWEEN FR 39 TO FR 39.2 AT RIGHT BUTTLINE -Y450 TO LEFT BUTTLINE Y450 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 242BF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR STRUCTURE BETWEEN +YB1 & +YA AND BETWEEN FR 73 & FR 74 AT AFT GALLEY AREA. REPLACED FLOOR STRUCTURE BEAM SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 251ZF IN PASSENGER CABIN. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: FLOOR SUPPORT — CORRODED (FRAMES 79-80) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT +Y450 AND PLATE BETWEEN FRAMES 79 - 80 AT THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 13 TO 14, +Y1456. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53111987.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF SEAT TRACK BETWEEN FR 12 TO FR 18 AT RIGHT BUTTLINE +Y450. REPLACED SEAT TRACK BETWEEN FR 12 TO FR 18 AT RIGHT BUTTLINE +Y450 PER SRM 51-72-11 AND DRAWING F53111987.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED STRINGER BETWEEN FR 53.4 PLUS 14 INCHES TO FR 53.5A AT RIGHT STRINGER 13 EMERGENCY DOOR 3R CUTOUT DOOR IN PASSENGER CABIN. REPLACED STRINGER BETWEEN FR 53.4 PLUS 14 INCHES TO FR 53.5A AT RIGHT STRINGER 13 EMERGENCY DOOR 3R CUTOUT DOOR IN PASSENGER CABIN PER SRM 51-72-11 AND DRAWING F53370020.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON SEAT TRACK -Y450 AT FWD GALLEY AREA ON FRAME 17. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO FLOOR BEAM BETWEEN FR 75 AND FR 78 AT LEFT BUTTLINE +YE1. REPLACED FLOOR BEAM BETWEEN FR 75 AND FR 78 AT LEFT BUTTLINE +YE1 PER SRM 51-72-11.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED FLOOR PANEL 272KF IN PASSENGER CABIN BETWEEN FR 73 TO FR 76 AT RIGHT BUTTLINE -Y1447.8 TO RIGHT BUTTLINE -Y1137.1. REPLACED FLOOR PANEL 272KF IN PASSENGER CABIN BETWEEN FR 73 TO FR 76 AT RIGHT BUTTLINE -Y1447.8 TO RIGHT BUTTLINE -Y1137.1 PER EA 275873.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-80) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT -Y450 BETWEEN FRAMES 75 - 80 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

COROSION FOUND ON THE FLOOR SUPPORT AT -Y648 BETWEEN FRAMES 73 - 75 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51- 42-11-001.

Part: SEAT TRACK — CORRODED (FRAMES 11-18) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENENACE. CORROSION FLOOR BEAM (RAIL) +Y953 AT FORWARD GALLEY AREA BETWEEN FRAME 11 AND FRAME 18. REPLACED FLOOR BEAM (RAIL) PER SRM 51-2-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 79-80) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT -Y794.3 BETWEEN FRAMES 79 & 80 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM -YE1 BETWEEN FR 75 & FR 78 AT AFT GALLEY AREA. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FLOORBEAM -Y1447.8 BETWEEN FR74 & FR78 AT AFT GALLEY AREA. REPLACED FLOORBEAM PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED FLOOR SUPPORT -Y794.3 BETWEEN FRAMES 73 & 74 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM BETWEEN FR 79 AND FR 80 AT Y0. REPLACED FLOORBEAM PER SRM 51-72-11 AND DWG F53478018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING F53478018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM -Y1447.8 BETWEEN FR78 & FR80 AT AFT GALLEY AREA. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

CRACKED FLOOR PANEL 271KF, LOWER FACE, IN THE PASSENGER CABIN BETWEEN FRAMES 73 TO 76 AT LBL 1447.8 TO Y1137.1. REPLACED THE FLOOR PANEL IAW EA 275873.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 271MF, BETWEEN FRAMES 75 AND 78, -Y450 TO Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672322.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORROSION ON THE SEAT TRACK BETWEEN FRAMES 73 TO 74, -YB1. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 272HG BETWEEN FRAMES 73 AND 76, -Y1137.1 TO -Y794.3. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672325.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 271AF, BETWEEN FRAMES 71 AND 73, -Y450 AND Y450. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672285.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION FOUND ON FLOOR PANEL 272GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672326.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 272AG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701. REVISION G AND DRAWING NF53672291.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 271HF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009, FIGURE 20109, IRM 9701 REVISION G AND DRAWING F53672325.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 271FF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009, FIGURE 20109, IRM 9701 REVISION G AND DRAWING F53672327.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF SEAT TRACK BETWEEN FR 71 TO FR 75 AT LEFT BUTTLINE +Y450. REPLACED SEAT RAIL BETWEEN FR 71 TO FR 75 AT LEFT BUTTLINE +Y450 PER SRM 51-72-11 AND DRAWING F53478018.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION FOUND ON FLOOR PANEL 271GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672286.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 272CF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G AND DRAWING NF53672286.

Part: STRINGER — CORRODED (FRAME 67) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORROSION ON STRINGER 55L, FRAME 67. REPAIRED STRINGER IAW EA 275913.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 271AG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G AND DRAWING N.F53672291.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 271PF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109, IRM 9701 REVISION G AND DRAWING F53672358.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 271BF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009, FIGURE 20109, IRM 9701 REVISION G AND DRAWING F53672284.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 272BF. REPLACED FLOOR PANEL PER SRM 53-02-02-300-009 FIGURE 20109. IRM 9701 REVISION G AND DRAWING NF53672284.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

CRACKED STIFFENER BETWEEN STRINGERS 25 TO 27R. REPLACED THE STIFFENER IAW EO 5315U155-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION FOUND ON FLOOR PANEL 272GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672326.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF SEAT TRACK BETWEEN FR 72 TO FR 75 AT RIGHT BUTTLINE -Y450. REPLACED SEAT TRACK BETWEEN FR 72 TO FR 75 AT RIGHT BUTTLINE -Y450 PER SRM 51-72-11 AND DRAWING F53478018.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND SIDE UPPER BELLY FAIRING SUPPORT BRACKET BETWEEN FR40 AND FR 40.1 ON LOWER FUSELAGE. REPLACED SUPPORT BRACKET PER SRM 51-72-11 AND DRAWING F53321310.

Part: STIFFENER — CRACKED (FRAME 12A) · airframe 76,510 hrs · 10,657 cycles

CRACKED STIFFENER AT FRAME 12A, BETWEEN STRINGERS 25 TO 27L. REPLACED THE STIFFENER IAW EO 5315U155-00.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED SEAT TRACK -Y1552.5 IN PASSENGER CABIN AT FRAME 33. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED SEAT TRACK -Y450 IN PASSENGER CABIN FROM FRAMES 30 TO 37. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 272QF BETWEEN FR 78 TO FR 80 AT STRINGER 25. REPLACED FLOOR PANEL 272QF BETWEEN FR 78 TO FR 80 AT STRINGER 25 PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 271GF, BETWEEB FRAMES 73 AND 76, Y450 TO Y794.3. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53672326.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF SEAT TRACK BETWEEN FR 73 TO FR 74 AT RIGHT BUTTLINE -Y1456 MINUS 4 INCHES. REPLACED SEAT TRACK BETWEEN FR 73 TO FR 74 AT RIGHT BUTTLINE -Y1456 MINUS 4 INCHES PER SRM 51-72-11.

Part: SUPPORT BRACKET — DAMAGED (FUSELAGE) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON RIGHT HAND SIDE UPPER BELLY FAIRING SUPPORT BRACKET BETWEEN FR 40.1 AND 40.2 ON LOWER FUSELAGE. REPLACED SUPPORT BRACKET PER SRM 51-72-11 AND DRAWING F53321310.

Part: SEAT TRACK — CORRODED (FRAMES 30-37) · corrosion level 2 · airframe 76,510 hrs · 10,657 cycles

CORRODED SEAT TRACK +Y450 IN PASSENGER CABIN FROM FRAMES 30 TO 37. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 231GF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009, FIGURE 20109 IRM REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 241E BETWEEN FR. 31 TO FR. 33 AT LEFT BUTTLINE Y2462 TO LEFT BUTTLINE Y1959. REPLACED FLOOR PANEL 241E BETWEEN FR. 31 TO FR. 33 AT LEFT BUTTLINE Y2462 TO LEFT BUTTLINE Y1959 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251DF BETWEEN FR 37 AND FR 37.4 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y1456. REPLACED FLOOR PANEL 251DF BETWEEN FR 37 AND FR 37.4 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y1456 PER A330 SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 241GF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 241GF BETWEEN FR 33 TO FR 37 AT LEFT BUTTLINE Y450 TO LEFT BUTTLINE Y953 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION FOUND ON FLOOR PANEL 221BF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 970 REVISION G, AND DRAWING F53671114.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF FLOOR PANEL 251JF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251C BETWEEN FR 37 TO FR 37.4 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 251C BETWEEN FR 37 TO FR 37.4 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 221E BETWEEN FR. 14 TO FR. 17 AT LEFT BUTTLINE Y953 TO RIGHT BUTTLINE -Y953. REPLACED FLOOR PANEL 221E BETWEEN FR. 14 TO FR. 17 AT LEFT BUTTLINE Y953 TO RIGHT BUTTLINE -Y953 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251 EF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (FRAMES 33-37) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 241FF BETWEEN FR 33 TO FR 37 AT RIGHT BUTTLINE -450 TO LEFT BUTTLINE Y450. REPLACED FLOOR PANEL 241FF BETWEEN FR 33 TO FR 37 AT RIGHT BUTTLINE -450 TO LEFT BUTTLINE Y450 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 222JF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251N BETWEEN FR 39 AND FR 39.2 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953. REPLACED FLOOR PANEL 251N BETWEEN FR 39 AND FR 39.2 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y953 PER SRM 53-02-00-300-009 FIGURE 2010 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251Y BETWEEN FR. 40 TO FR. 42 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y954. REPLACED FLOOR PANEL 251Y BETWEEN FR. 40 TO FR. 42 AT LEFT BUTTLINE Y1456 TO LEFT BUTTLINE Y954 PER SRM 53-02-00-300-009 FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261MF IN PASSENGER CABIN. REPLACED FLOOR PANEL REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251BF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM REVISION G.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261JF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251DG. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009 FIGURE 20109 IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 251FG IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 262HF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-009.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (FRAMES 26-31) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 231EG BETWEEN FR 26.4 TO FR 31 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462. REPLACED FLOOR PANEL 231EG BETWEEN FR 26.4 TO FR 31 AT LEFT BUTTLINE Y1959 TO LEFT BUTTLINE Y2462 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (FRAMES 14-17) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER FLOOR PANEL 221JF BETWEEN FR 14 TO FR 17 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456. REPLACED FLOOR PANEL 221JF BETWEEN FR 14 TO FR 17 AT LEFT BUTTLINE Y953 TO LEFT BUTTLINE Y1456 PER A330 SRM 53-02-00-300-009 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATION FOUND ON FLOOR PANEL 221AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, FIGURE 20109, IRM 9701, REVISION G, AND DRAWING F53671115.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 76,510 hrs · 10,657 cycles

DELAMINATED TOP LAYER OF FLOOR PANEL 222DF IN PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 76,510 hrs · 10,657 cycles

LOWER SKIN ON FLAP DEBONDED BETWEEN RIB 8 TO RIB 9. REPAIRED THE SKIN ON THE FLAP IAW EA 275555.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 76,067 hrs · 10,603 cycles

EMERGENCY LIGHT FAILED AN OPS TEST. REPLACED EPSU.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 76,067 hrs · 10,603 cycles

EMERGENCY LIGHT FAILED AN OPS TEST. FAULTED ESPU 11WL, BATTERY FAULT. REPLACED THE BATTERY.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHT) · airframe 76,067 hrs · 10,603 cycles

EMERGENCY LIGHT FAILED OPS TEST. REPLACED THE WIRE HARNESS.

Part: LENS — MISSING (CABIN) · airframe 75,734 hrs · 10,563 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT COVER PLATE ON RIGHT SIDE OF LAV L73 IS MISSING. REPLACED EMERGENCY LIGHT LENS COVER.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 75,224 hrs · 10,501 cycles

AIRCRAFT WAS NOT GROUNDED. 1L SLIDE DIFFICULT TO ARM. REMOVED DEBRIS FROM 1L DOOR.

Part: OVEN — ODOR (MID GALLEY) · airframe 74,880 hrs · 10,457 cycles

RIGHT SIDE OVEN IN THE MID GALLEY IS VERY SLOW TO HEAT AND HAS A VERY STRONG CHEMICAL ODOR WHILE HEATING. CHEMICAL ODOR WAS VERY STRONG. REPLACED THE OVEN IAW AMM 25-35-19.

Part: LIGHT — INOPERATIVE (SEAT 11B) · airframe 74,276 hrs · 10,381 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 11B. REPAIRED EMERGENCY LIGHT ASSY.

Part: GIRT BAR — DIRTY (L4 DOOR SLIDE) · airframe 73,918 hrs · 10,335 cycles

L4 DOOR MECHANISM WILL NOT ARM. MOVES HALFWAY AND BINDS. INSPECTED DOOR AND FOUND DEBRIS IN GIRT BAR FLOOR FITTING. REMOVED DEBRIS FROM GIRT BAR FITTING.

Part: LAMP — SHORTED (GALLEY) · airframe 73,841 hrs · 10,323 cycles

AIRCRAFT WAS GROUNDED. WHILE TROUBLE SHOOTING FORWARD GALLEY CHILLER, FOUND BURN MARKS / ARCING BEHIND FORWARD GALLEY CIRCUIT BREAKER PANEL. FOUND GALLEY 115V OUTLET POWER INDICATOR LAMP SHORTED TO GROUND. REPLACED LAMP ASSEMBLY PER CMM 25-32-04. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,068 hrs · 10,193 cycles

AIRCRAFT IN BASE MAINTENANCE. INOPERABLE FLASHLIGHT AT 3L DOOR (UPPER FLASHLIGHT). REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: ENGINE — VIBRATION (LEFT) · airframe 72,464 hrs · 10,102 cycles

DURING CLIMB, THE CREW REPORTED THAT THE NR 1 ENGINE WAS VIBRATING AND HAD A HIGH EGT AND INTERMITTENT FIRE WARNING. POWER WAS REDUCED TO IDLE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. ACFT GROUND. REPLACED THE LEFT ENGINE.

Part: DOOR — OBSTRUCTED (R3) · airframe 71,873 hrs · 10,013 cycles

R3 DOOR WILL NOT FULLY OPEN. ADJUSTED THE R3 DOOR UPPER PLASTIC TRIM AND OPENED AND CLOSED DOOR MULTIPLE TIMES, OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — DAMAGED (L1 DOOR SLIDE) · airframe 71,402 hrs · 9,955 cycles

EMERGENCY POWER SUPPLY UNIT WILL NOT TEST AT L1 DOOR. ACCOMPLISHED TSM 33-41-00-810-818-A, AND FOUND GROUND SIGNAL ON PIN C REQUIRING SLIDE CHANGE OF L1 DOOR. REPLACED THE SLIDE AND ACCOMPLISHED A SATISFACTORY OPS CHECK OF THE SLIDE AND EMERGENCY POWER SUPPLY UNIT IAW JOB CARD 33L00025001 AND AMM 33-51-0-710-801-A.

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 71,258 hrs · 9,937 cycles

ECAM FUEL LEFT PUMP 1 LOW PRESSURE. MAINTENANCE PERFORMED TSM 28-21-00-810-852A AND FOUND NO CIRCUIT BREAKERS TRIPPED AND NO DEFECTS NOTED DURING AN OPERATIONAL CHECK OF THE PUMPS. REPLACED FUEL PUMP PRESSURE SWITCH IAW AMM 28-21-15 AND ACCOMPLISHED A SATISFACTORY LEAK & OP CHECK IAW AMM 28-21-15.

Part: CHILLER — ODOR (LAVATORY) · airframe 71,249 hrs · 9,936 cycles

FLIGHT CREW REPORTED HOT ODOR LIKE MELTING PLASTIC OR WIRE COMING FROM AFT GALLEY. MAINTENANCE REPLACED THE AFT CHILLER IAW AMM 25-35-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 9,788 hrs · 70,048 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS FAILED THE OPERATIONAL CHECK ACCOMPLISHED BY JC 33C22033002 VIA MCDU. R & R EMER LIGHT BATTERY PACK ABOVE R3 DOOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,038 hrs · 9,787 cycles

AIRCRAFT WAS NOT GNDED. R4 DOOR EMER EXIT LIGHT BATTERY FAIL BATTERY CHECK ON CARD 33C22033002. REPLACED BATTERY ON EMER POWER SUPPLY UNIT 18WL AT THE R4 DOOR AREA IAW AMM 33-51-38. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CHECK VALVE — DEFECTIVE (ZONE 400) · airframe 69,571 hrs · 9,725 cycles

AIRCRAFT WAS GNDED. NR 2 ENG STALLS, FIVE HRS INTO FLT, HAD BEEN AT FL400, REC MAX 409 FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING AGAIN. ACCOMPLISHED ENG STALL, NOT DISPLAYED ON ECAM, QRH PROCEDURE WHILE DESCENDING TO FL300. AT FL300 BOTH ENG INDICATIONS WERE NORMAL & STABLE. REPLACED THE NR 2 ENG FUEL PUMP, FUEL DIFFERENTIAL PRESS SWITCH & FUEL METERING UNIT IAW AMM 73-11-11 & 73-21-12. THE NR 2 ENG LT & RT 8TH STAGE CHECK VLVS WERE FOUND TO BE FAULTY & WERE REPLACED IAW AMM 36-11-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PRESSURE SWITCH — DEFECTIVE (NR 2 ENGINE) · airframe 69,571 hrs · 9,725 cycles

AIRCRAFT WAS GNDED. NR 2 ENG STALLS. FIVE HRS INTO FLT, HAD BEEN AT FL400, REC MAX 409 FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING AGAIN.. ACCOMPLISHED ENG STALL, NOT DISPLAYED ON ECAM, QRH PROCEDURE WHILE DESCENDING TO FL300. AT FL300 BOTH ENG INDICATIONS WERE NORMAL & STABLE. CONTINUED & REPLACED THE NR 2 ENG FUEL PUMP, FUEL DIFFERENTIAL PRESS SWITCH & FUEL METERING UNIT IAW AMM 73-11-11 & 73-21-12. THE NR 2 ENG L & RT 8TH STAGE CHECK VLVS WERE FOUND TO BE FAULTY & WERE REPLACED IAW AMM 36-11-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 69,571 hrs · 9,725 cycles

AIRCRAFT WAS GNDED. NR 2 ENG STALLS, 5 HRS INTO FLT, HAD BEEN AT FL 400, REC MAX 409, FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING AGAIN. ACCOMPLISHED ENG STALL, NOT DISPLAYED ON ECAM, QRH PROCEDURE WHILE DESCENDING TO FL300. AT FL300 BOTH ENG INDICATIONS WERE NORMAL & STABLE. REPLACED THE NR 2 ENG FUEL PUMP, FUEL DIFFERENTIAL PRESS SWITCH & FUEL METERING UNT IAW AMM 73-11-11 & 73-21-12. THE NR 2 ENG LT & RT 8TH STAGE CHECK VLVS WERE FOUND TO BE FAULTY & WERE REPLACED IAW AMM 36-11-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CHECK VALVE — DEFECTIVE (ZONE 400) · airframe 69,571 hrs · 9,725 cycles

AIRCRAFT WAS GNDED. NR 2 ENG STALLS, FIVE HRS INTO FLT HAD BEEN AT FL400, REC MAX 409 FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING AGAIN. ACCOMPLISHED ENG STALL, NOT DISPLAYED ON ECAM, QRH PROCEDURE WHILE DESCENDING TO FL300, AT FL300 BOTH ENG INDICATIONS WERE NORMAL & STABLE. REPLACED THE NR 2 ENG FUEL PUMP, FUEL DIFFERENTIAL PRESS SWITCH & FUEL METERING UNIT IAW AMM 73-11-11 & 73-21-12. THE NR 2 ENG LT & RT 8TH STAGE CHECK VLVS WERE FOUND TO BE FAULTY & WERE REPLACED IAW AMM 36-11-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: METERING UNIT — DEFECTIVE (NR 2 ENGINE) · airframe 69,571 hrs · 9,725 cycles

AIRCRAFT WAS GNDED. NR 2 ENG STALLS, FIVE HRS INTO FLT, HAD BEEN AT FL400, REC MAX 409 FOR ABOUT 5 MIN WITH NO TURB & GOT NUMEROUS NR 2 ENG STALL ECAM WARNINGS. ENG WOULD GO TO IDLE, ECAM WARNING WOULD DISAPPEAR & ENG WOULD ACCELERATE TRIGGERING THE WARNING AGAIN. ACCOMPLISHED ENG STALL, NOT DISPLAYED ON ECAM, QRH PROCEDURE WHILE DESCENDING TO FL 300. AT FL 300 BOTH ENG INDICATIONS WERE NORMAL & STABLE. WE CONTINUED & REPLACED THE NR 2 ENG FUEL PUMP, FUEL DIFFERENTIAL PRESS SWITCH & FUEL METERING UNIT IAW AMM 73-11-11 & 73-21-12. THE NR 2 ENG LT & RT 8TH STAGE CHECK VLVS WERE FOUND TO BE FAULTY & WERE REPLACED IAW AMM 36-11-41. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LENS — MISSING (CABIN) · airframe 68,988 hrs · 9,581 cycles

AIRCRAFT IN BASE MX. SEAT 16AB IS MISSING COVER FOR EMER LIGHT, EMER LIGHT WORKS. R & R ROW 16AB EMER LIGHT IAW CMM 25-23-54. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801-A01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,979 hrs · 9,578 cycles

AIRCRAFT WAS IN BASE MX. SEAT 4H EMER LIGHT INOPERATIVE. R & R EMER LIGHT IN SEAT 4H IAW SEAT CMM 25-02-38. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 35-51-00-710-803-A.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 66,276 hrs · 9,171 cycles

DOOR 3R, EMER CYLINDER PRESS IN THE YELLOW BAND. SERVICED DOOR 3R EMER CYLINDER.

Part: WIRE HARNESS — UNSECURE (CABIN) · airframe 65,886 hrs · 9,114 cycles

ROW 31, SEAT GH, EMER LIGHT WONT ILLUMINATE. SECURED WIRES GOING TO SEAT 31GH.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 65,487 hrs · 9,058 cycles

R3 DOOR ASSIST AT TOP OF YELLOW BAND. SERVICED R3 DOOR ASSIST IAW 52-22-00.

Part: STRUT — LOW (NLG) · airframe 65,169 hrs · 9,012 cycles

BOTH TAKEOFFS TODAY, THE NOSE GEAR WOULD NOT CYCLE UP. HAD TO LOWER GEAR & THEN RETRACT THEM A SECOND TIME, WORKED SECOND TIME. ACCOMPLISHED FULL SERVICE OF NOSE LANDING GEAR STRUT. ALSO ACCOMPLISHED TWO SUCCESSFUL EXTENSIONS & RETRACTIONS. OPERATIONS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 65,148 hrs · 9,008 cycles

CIDS PANEL SAYS CHECK DOOR PRESS 3R. SERVICED 3R DOOR ASSIST BOTTLE. LEAK CHECK OK. OK FOR SERVICE.

Part: O-RING — LEAKING (APU) · airframe 65,055 hrs · 8,992 cycles

THE CABIN CREW NOTICED FUMES IN THE GALLEY, ACFT RT, & BOTH AISLES LT & RT OF ACFT STARTING AT ROW 1 & BECOMING STRONGER AT ROWS 8 - 12. THE FLIGHT DECK CREW CAME INTO THE CABIN & VERIFIED THE ODORS. SEVERAL CABIN CREW MEMBERS USED PORTABLE OXYGEN AS NECESSARY. NO PAX COMPLAINTS WERE RECEIVED. THE PACKS WERE PLACED ON HI FLOW WHICH CAUSED THE FUMES TO DIMINISH. THE FUMES REAPPEARED ON APPROACH BELOW 6,000 FEET. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. DETERMINED THE APU TO BE THE CAUSE. THE APU WAS PLACED ON MEL DEFERRAL. REPLACED AN O RING AT THE APU OIL PUMP MODULE.

Part: WIRE — BROKEN (CABIN) · airframe 64,817 hrs · 8,932 cycles

SEAT EMER LIGHT AT SEAT 1A INOPERATIVE. REPAIRED BROKEN WIRE GOING TO EMER LIGHT AT SEAT 1A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,809 hrs · 8,931 cycles

SEAT 1R SEAT EMER LIGHT INOPERATIVE. REPLACED SEAT 1R SEAT EMER LIGHT ASSEMBLY AT SEAT.

Part: ACTUATOR — LOW PRESSURE (R3 DOOR) · airframe 64,676 hrs · 8,896 cycles

R3 EMER DOOR ASSIST DAMPER PRESS READS IN YELLOW BAND. CHARGED R3 EMER DOOR ASSIST WITH NITROGEN IAW AMM 52-10-00-600-802-A.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,466 hrs · 8,849 cycles

C2 CHECK DELAMINATION ON FLOOR PANEL 162EF BETWEEN FRAME 69 TO 73 & BETWEEN -Y1246 TO 0. REPLACED FLOOR PANEL 162EF IAW SRM 53-02-00 PARA 5I FIG 211.

Part: LIGHT — INOPERATIVE (CABIN)

LAVATORY L33, L11, L62, L61 & L74 EMER LIGHT INOPERATIVE. R & R EMER LIGHT. OKAY FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 64,344 hrs · 8,821 cycles

DURING DAILY CHECK, DOOR 3R DAMPER & EMER CYLINDER FOUND IN THE YELLOW BAND. SERVICED THE 3R DOOR DAMPER & EMER CYLINDER.

Part: SWITCH — LOOSE (COCKPIT SEAT) · airframe 63,576 hrs · 8,727 cycles

REGARDING MEL ON FIRST OFFICER`S ELEC SEAT CONTROLS, ELEC VERTICAL CONTROL ON FIRST OFFICER'S SEAT INOPERATIVE. DURING CLIMB OUT SEAT STARTED MOVING BACKWARDS ON ITS OWN, PROBABLY DUE TO FORCE ON ELEC SWITCH, VERY LOOSE, RECOMMEND DISABLE SWITCH. REPLACED HORIZONTAL ELEC SWITCH ON FIRST OFFICER`S SEAT ASSEMBLY. OPERATIONS CHECKED GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 61,895 hrs · 8,515 cycles

FLIGHT 787, CDG - CLT LOST BLUE HYD SYS PRESS & QTY, CONTINUING TO CLT. DECLARED AN EMERGENCY & THE FLIGHT LANDED UNEVENTFULLY. R & R THE NR 1 ENG BLUE SYS HYD PUMP.

Part: ROLLER — STUCK (L4 DOOR) · airframe 61,792 hrs · 8,502 cycles

DOOR 4L STUCK IN HALF OPEN & CLOSED POSITION. RELEASED SPRING ROLLER ON FWD FRAME HALFWAY ON DOOR GUIDE FOUND OVER LATCH PLATE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 61,775 hrs · 8,500 cycles

FORWARD MEGA PHONE. R & R FWD MEGA PHONE.

Part: DEU — FAULTY (ZONE 200) · airframe 61,668 hrs · 8,486 cycles

CLT 3L SLIDE BOTTLE & DOOR REPORT LOW ON CIDS PANEL. REPLACED DEU 300RH5.

Part: MONITOR — FAULTY (CABIN) · airframe 61,226 hrs · 8,428 cycles

23F IFE INOPERATIVE. REPLACED MONITOR AT SEAT 23F.

Part: INTERFACE UNIT — INOPERATIVE (CABIN) · airframe 61,226 hrs · 8,428 cycles

SEAT 11H MONITOR SMOKED AFTER INSTALLATION. R & R ACFT INTERFACE.

Part: MONITOR — FAULTY (CABIN) · airframe 61,227 hrs · 8,428 cycles

IFE 15H SMOKING. REPLACED MONITOR AT SEAT 15H, OPERATIONAL CHECK IS SATISFACTORY.

Part: MONITOR — FAULTY (CABIN) · airframe 61,226 hrs · 8,428 cycles

SMOKE REPORTED COMING FROM MONITOR AT 11H. REPLACED MONITOR AT SEAT 11H, OPERATIONAL CHECK IS SATISFACTORY.

Part: PIN — NOT SEATED (EMERGENCY LIGHTS) · airframe 61,131 hrs · 8,414 cycles

SEAT 6A EMERGENCY LIGHT INOPERATIVE. RESEATED PUSHED PIN AT SEAT CONNECTOR. OPERATIONAL CHECK IS SATISFACTORY.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 61,131 hrs · 8,414 cycles

ELEC FLASH FROM BEHIND THE CAPPUCCINO MAKER. STRONG ELEC SMELL WHICH DISSIPATED AFTER A FEW MINUTES, MID GALLEY 4. REPLACED COFFEEMAKER NR 1, NR 2 & NR 3 ESPRESSO MAKERS.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 60,735 hrs · 8,356 cycles

1R CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK FAILED BATTERY TEST. R & R 1R CABIN EMERGENCY LIGHTING, EMERGENCY POWER SUPPLY UNIT.

Part: COVER — MISSING (CABIN) · airframe 58,570 hrs · 8,064 cycles

EMERGENCY LIGHT COVER MISSING, FWD GALLEY AT CART 2-9 POSITION. (LT EDGE OF GALLEY FACING AFT ABOUT 12' OFF FLOOR).

Part: COVER — LOOSE (L4 DOOR) · airframe 58,167 hrs · 8,014 cycles

L4 DOOR JAMMED, WILL NOT OPEN, WILL NOT CLOSE. MX FOUND COVERS LOOSE. COVERS ATTACHED AND OPEN/CLOSE FUNCTION SATISFACTORY FOR SERVICE.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 57,916 hrs · 7,979 cycles

INFLIGHT LOSS OF O2 (CREW) LANDED WITH 375 PSI. SERVICED. MX FOUND CAPT O2 MASK LEAKING. SWAPPED TO FIRST OBSERVER SEAT. REMOVED, SERVICED AND REINSTALLED CREW O2 BOTTLE. LEAK CHECK CARRIED OUT. NO FAULTS, ACFT OK FOR CONTINUED SERVICE. CAPTAIN'S MASK REMOVED AND REPLACED.

Part: DOOR — JAMMED (CABIN) · airframe 57,916 hrs · 7,979 cycles

ENTRY DOOR 4L WAS STUCK NEITHER FULLY OPEN NOR FULLY CLOSED, JAMMED. MX UNJAMMED PAX DOOR 4L AND ACCOMPLISHED DOOR INSPECTION. NO DAMAGE NOTED.

Part: SIGN — DETACHED (CABIN) · airframe 57,210 hrs · 7,891 cycles

EXIT SIGN ACFT RT NEAR 2R DOOR CAME OFF. REPLACED EXIT SIGN COVER AS REQUIRED.

Part: SOCKET — UNSECURE (CABIN) · airframe 56,836 hrs · 7,841 cycles

21B-INSEAT EMERGENCY EXIT LED SOCKET FELL FROM POSTION, SOCKET ON CENTER PEDISTAL. MAINTENANCE RE-INSTALLED EMERGENCY LED SOCKET AT SEAT 21B. OPERATIONAL CHECK IS GOOD.

Part: LENS — MISSING (CABIN) · airframe 56,787 hrs · 7,835 cycles

LENS COVER FOR EMERGENCY LIGHT AT LAV L53 IS MISSING. MAINTENANCE INSTALLED LENS EMERGENCY COVER AT LAV L53.

Part: COVER — DETACHED (CABIN) · airframe 56,585 hrs · 7,808 cycles

THE 3L EXIT COVER HAS FALLEN OFF. MAINTENANCE SECURED 3L EXIT COVER.

Part: LENS — DETACHED (EXIT SIGN) · airframe 56,396 hrs · 7,782 cycles

EXIT SIGN AT 3R FELL OFF. MAINTENANCE RE-INSTALLED LENS. OK FOR SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 55,454 hrs · 7,652 cycles

PHL - EMERGENCY LIGHT AT THE 2R DOOR FLICKERS ON TAKEOFF. MAINTENANCE REPLACED CEILING EMERGENCY LIGHT ASSY.

Part: COVER — MISSING (CABIN) · airframe 53,630 hrs · 7,415 cycles

EMERGENCY LENS COVER MISSING AT 4R DOOR. MAINTENANCE INSTALLED COVER, FOUND IN OVERHEAD BIN.

Part: COVER — MISSING (CABIN) · airframe 53,331 hrs · 7,376 cycles

EMERGENCY LIGHT ON L74 COVER PANEL A/C RIGHT. MAINTENANCE REPLACED L74 EMERGENCY LIGHT COVER, CHECKS NORMAL.

Part: SIGN — MISSING (CABIN) · airframe 52,374 hrs · 7,253 cycles

EXIT SIGN 3L DOOR IS MISSING/BROKEN. MAINTENANCE REPLACED EXIT SIGN FOR 3L DOOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,236 hrs · 7,236 cycles

EMERGENCY LIGHT BATTERY 3R (16WL) FAILED TEST (J/C 33C20033002 CAPACITY CHECK). REMOVED & REPLACED BATTERY 16WL.

Part: COVER — LOOSE (EXIT SIGN) · airframe 52,229 hrs · 7,235 cycles

L2 OVERHEAD EXIT LIGHT (AISLE) PLASTIC COVER DOES NOT STAY ATTACHED TO LIGHT FIXTURE. MAINTENANCE RE-SECURED PLASTIC COVER OF L2 EXIT SIGN INTO ITS LIGHT ASSEMBLY. OPERATIONAL CHECK IS OKAY.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 51,971 hrs · 7,201 cycles

THE R3 DOOR EXIT SIGN MISSING. MAINTENANCE REPLACED EXIT SIGN.

Part: ATTACH FITTING — DEFECTIVE (GIRT BAR) · airframe 51,327 hrs · 7,115 cycles

WHILE OPENING L1 DOOR, OBSERVED REAR PORTION OF GIRT BAR SLIDE NOT ENGAGED IN TRACK, HANGING FROM BOTTOM OF DOOR. MAINTENANCE REASSEMBLED GIRT BAR ATTACH FITTING CORRECTLY. L1 DOOR SLIDE ASSEMBLY OPERATES PROPERLY.

Part: REGULATOR — LEAKING (APU) · airframe 50,578 hrs · 7,022 cycles

FLIGHT 733, LGW-CLT - MALODOROUS SMELL ON APPROACH, ZONE C & AFT GALLEY AREA. MAINTENANCE PERFORMED CABIN AIR QUALITY JOB CARD 33L00021001. FOUND APU LEAKING OIL INTO AIR INLET, REMOVED AND REPLACED APU OIL TEMPERATURE COOLER REGULATOR. EXTENSIVE ENGINE RUNS & REPLACEMENT OF RECIRC FILTERS ACCOMPLISHED, NO UNUSUAL ODORS NOTED.

Part: COVER — MISSING (CABIN) · airframe 50,256 hrs · 6,982 cycles

CLT - EXIT LIGHT COVER AT DOOR 1L DOOR, COVER IS IN COCKPIT ON THE PEDESTAL. MAINTENANCE RE-INSTALLED EXIT LIGHT COVER AT 1L DOOR, CHECKS OK.

Part: OVEN — INOPERATIVE (GALLEY) · airframe 50,256 hrs · 6,982 cycles

CLT - NR 1 OVEN TEMP LIGHT COMES ON MID GALLEY AND HAS STRONG ODOR. MAINTENANCE REPLACED THE MID GALLEY OVEN NR 1 POSITION. OPERATIONAL AND LEAK CHECKS ARE SATISFACTORY PER TASK 25-35-19-991-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,212 hrs · 6,975 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR42, Y450. REPLACED SEAT TRACK BETWEEN FR41 TO FR42, Y450 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,212 hrs · 6,975 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR42, -Y450. REPLACED SEAT TRACK BETWEEN FR41 TO FR42, -Y450 IAW A330 SRM 51-42-11.

Part: ANGLE — CRACKED (RT WING) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CRACKS ON RIGHT WING ANGLE AT FASTENER HOLES NUMBERS 7, 8, 10, FR42, RIB 1. REPLACED RIGHT WING ANGLE AT FR42, RIB 1 IAW EA 103364.

Part: ANGLE — CRACKED (LT WING) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CRACKS ON LEFT WING ANGLE AT FASTENER HOLES NUMBERS 7, 8, 10, FR42, RIB 1. REPLACED LEFT WING ANGLE AT FR42, RIB 1 IAW EA 103364.

Part: SIGN — BROKEN (CABIN) · airframe 50,203 hrs · 6,871 cycles

S2 CHECK - BROKEN EMERGENCY EXIT SIGN OVER R2 DOOR. REPLACED EMERGENCY EXIT SIGN OVER R2 DOOR IAW A330 AMM 33-51-17.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LIQUID INGRESS ON LT ELEVATOR BETWEEN RIB 18 TO RIB 19 AT 32ND TRAILING EDGE FASTENER. REPAIRED LT ELEVATOR BETWEEN RIB 18 TO RIB 19 AT 32ND TRAILING EDGE FASTENER IAW A330 SRM 55-22-11AND EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LIQUID INGRESS ON LT ELEVATOR BETWEEN RIB 6 TO RIB 7 AT 17TH TRAILING EDGE FASTENER. REPAIRED LT ELEVATOR BETWEEN RIB 6 TO RIB 7 AT 17TH TRAILING EDGE FASTENER IAW A330 SRM 55-22-11AND EO 5511U056.

Part: SLIDE RAFT — UNSERVICEABLE (L1 DOOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - SLIDE RAFT BAD FROM STOCK, NOT PACKED PROPERLY, BULGES AT CENTER BOTTOM AND BACK TO L1 DOOR FACING WILL NOT MOUNT PROPERLY DRAGS FLOOR SILL. REPLACED L1 DOOR SLIDE RAFT IAW A330 AMM 25-62-41.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LIQUID INGRESS ON LT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 40TH TRAILING EDGE FASTENER. REPAIRED LT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 40TH TRAILING EDGE FASTENER IAW A330 SRM 55-22-11AND EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LIQUID INGRESS ON RT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 38TH TRAILING EDGE FASTENER. REPAIRED RT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 38TH TRAILING EDGE FASTENER IAW A330 SRM 55-22-11AND EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LIQUID INGRESS ON LT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 37TH TRAILING EDGE FASTENER. REPAIRED LT ELEVATOR BETWEEN RIB 19 TO RIB 20 AT 37TH TRAILING EDGE FASTENER IAW A330 SRM 55-22-11AND EO 5511U056.

Part: SLIDE RAFT — OUT OF ADJUST (L2 DOOR) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DURING INSTALLATION OF L2 SLIDE PACK P/N 7A1539-045 S/N AUO417 DISCOVERED THE PARACHUTE PIN TRIGGER/CABLE ASSY AS PACKED HAS TENSION UNCHARACTERISTIC OF ADJACENT INSTALLATIONS AND UNABLE TO CONFIRM ACCEPTABILITY VIA AMM 25-62-41. REPLACED L2 SLIDE RAFT IAW A330 AMM 25-62-41, OPS & SYSTEM CHECK GOOD IAW A330 AMM 25-62-41 & 52-71-00.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN R4 DOOR EMERGENCY EXIT SIDE SIGN LENS MISSING. INSTALLED CABIN R4 DOOR EMERGENCY EXIT SIDE SIGN LENS IAW A330 AMM 33-50-00.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN LEFT EMERGENCY DOOR EXIT SIDE SIGN LENS MISSING. INSTALLED CABIN LEFT EMERGENCY DOOR EXIT SIDE SIGN LENS IAW A330 AMM 33-50-00.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - EMERGENCY LIGHTS AT SEAT 40HG INOPERATIVE. RESEATED THE CONNECTOR FOR THE EMERGENCY LIGHTS AT SEAT 40HG IAW A330 AMM 33-51-12.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - EMERGENCY LIGHTS AT ROW 39 LEFT SIDE INOPERATIVE. RESEATED THE CONNECTOR FOR THE EMERGENCY LIGHTS AT ROW 39 LEFT SIDE IAW A330 AMM 33-51-11.

Part: DOOR FRAME — CRACKED (R4 DOOR) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CRACK ON R4 DOOR LOWER CORNER FRAME ASSEMBLY DOOR BEAM NR 8 AT FR75A. REPLACED LOWER CORNER FRAME ASSEMBLY IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 271NF HAS AREA OF DISBOND BETWEEN FR 75 AND FR 78 AT Y1447.8. REPAIRED CABIN FLOOR PANEL 271NF BETWEEN FR 75 AND FR 78 AT Y1447.8 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 271PF HAS AREA OF DISBOND BETWEEN FR 78 AND FR 80 AT Y450. REPAIRED CABIN FLOOR PANEL 271PF BETWEEN FR 78 AND FR 80 AT Y450 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 251RF HAS AREA OF DISBOND AT FR 39 AND Y1185. REPAIRED CABIN FLOOR PANEL 251RF AT FR 39 AND Y1185 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 271HF HAS AREA OF DISBOND BETWEEN FR 75 AND FR 78 AT Y381. REPAIRED CABIN FLOOR PANEL 271HF BETWEEN FR 75 AND FR 78 AT Y381 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 272QF HAS AREA OF DISBOND BETWEEN FR 78 AND FR 80 AT Y1447.8. REPAIRED CABIN FLOOR PANEL 272QF BETWEEN FR 78 AND FR 80 AT Y1447.8 IAW A330 SRM 53-02-00.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - ON LEFT WHEEL WELL FAIRING AT FLAP CARRIAGE FR53.2, BETWEEN S32L TO S37L. REPAIRED FAIRING AT FLAP CARRIAGE FR53.2, BETWEEN S32L TO S37L IAW A330 SRM 53-35-14.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 231XF BETWEEN FR26.1 TO FR26.4, Y987. REPAIRED FLOOR PANEL 231XF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 232LF BETWEEN FR22 TO FR25, -Y795. REPAIRED FLOOR PANEL 232LF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 232ZF BETWEEN FR26.1 TO FR28, -Y1975. REPAIRED FLOOR PANEL 232ZF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 231VF BETWEEN FR26.1 TO FR28, Y=0. REPAIRED FLOOR PANEL 231VF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 223RF HAS AREA OF DELAMINATION BETWEEN FR 25 AND FR 26.1 AT +Y790. REPAIRED CABIN FLOOR PANEL 223RF BETWEEN FR 25 AND FR 26.1 AT +Y790 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 232PF BETWEEN FR22 TO FR25, Y1975. REPAIRED FLOOR PANEL 232PF A330 IAW AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 261TG HAS AREA OF DISBOND BETWEEN FR 65 AND FR 69 AT +Y1382. REPAIRED CABIN FLOOR PANEL 261TG BETWEEN FR 65 AND FR 69 AT +Y1382 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 232HF HAS AREA OF DISBOND BETWEEN FR 19 AND FR 22 AT Y1580. REPAIRED CABIN FLOOR PANEL 232HF BETWEEN FR 19 AND FR 22 AT Y1580 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 260GG HAS AREA OF DISBOND BETWEEN FR 60 AND FR 62 AT Y790. REPAIRED CABIN FLOOR PANEL 260GG BETWEEN FR 60 AND FR 62 AT Y790 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 232GF HAS AREA OF DISBOND BETWEEN FR 19 AND FR 22 AT -Y987. REPAIRED CABIN FLOOR PANEL 232GF BETWEEN FR 19 AND FR 22 AT -Y987 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED FLOOR PANEL 241KF BETWEEN FR34 TO FR35, BETWEEN Y1975. REPAIRED FLOOR PANEL 241KF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 252XG BETWEEN FR 53.2 TO FR53.4, -Y1777. REPAIRED FLOOR PANEL 252XG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED FLOOR PANEL 231NF BETWEEN FR22 TO FR25, Y1382. REPAIRED FLOOR PANEL 231NF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 261MG HAS AREA OF DISBOND BETWEEN FR 62 AND FR 65 AT Y790. REPAIRED CABIN FLOOR PANEL 261MG BETWEEN FR 62 AND FR 65 AT Y790 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 231CF BETWEEN FR17 TO FR19, Y1382. REPAIRED FLOOR PANEL 231CF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED FLOOR PANEL 231TF BETWEEN FR25 TO FR26.1 Y1382. REPAIRED FLOOR PANEL 231TF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 232DG HAS AREA OF DISBOND BETWEEN FR 26.1 AND FR 31 AT -Y1975. REPAIRED CABIN FLOOR PANEL 232DG BETWEEN FR 26.1 AND FR 31 AT -Y1975 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED FLOOR PANEL 232DF BETWEEN FR17 TO FR19, -Y1382. REPAIRED FLOOR PANEL 232DF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED FLOOR PANEL 232MF BETWEEN FR22 TO FR25, -Y987. REPAIRED FLOOR PANEL 232MF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON FLOOR PANEL 261KF BETWEEN FR53 TO FR55, Y=0. REPAIRED FLOOR PANEL 261KF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON FLOOR PANEL 261AF BETWEEN FR53.4 TO FR53.6, Y=0. REPAIRED FLOOR PANEL 261AF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON FLOOR PANEL 261EF BETWEEN FR53.4 TO FR53.9, Y1975. REPAIRED FLOOR PANEL 261EF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

C11 CHECK - DISBONDING ON FLOOR PANEL 252WG BETWEEN FR53.2 TO FR53.6, -Y987. REPAIRED FLOOR PANEL 252WG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CRACK ON FLOOR PANEL 261JH BETWEEN FR53.4 TO FR53.9, Y1925. REPAIRED FLOOR PANEL 261JH IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 231LF HAS AREA OF DISBOND BETWEEN FR 22 AND FR 25 AT Y592. REPAIRED CABIN FLOOR PANEL 231LF BETWEEN FR 22 AND FR 25 AT Y592 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 211EF HAS AREA OF DISBOND BETWEEN FR 1 AND FR 11A AT Y0. REPAIRED CABIN FLOOR PANEL 211EF BETWEEN FR 1 AND FR 11A AT Y0 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262CF BETWEEN FR53.4 TO FR53.7, -Y1185. REPAIRED FLOOR PANEL 262CF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 231YF BETWEEN FR26.1 TO FR28, Y1530. REPAIRED FLOOR PANEL 231YF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 242LF BETWEEN FR33 TO FR35A, -Y2462. REPLACED FLOOR PANEL 242LF IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 261QG BETWEEN FR62 TO FR65, Y1777. REPAIRED FLOOR PANEL 261QG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 261ZF HAS AREA OF DISBOND BETWEEN FR 57.1 AND FR 58 AT Y1975. REPAIRED CABIN FLOOR PANEL 261ZF AT BETWEEN FR 57.1 AND FR 58 AT Y1975 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CABIN FLOOR PANEL 212HF HAS AREA OF DISBOND BETWEEN FR 1 AND FR 11A AT -Y592. REPAIRED CABIN FLOOR PANEL 212HF BETWEEN FR 1 AND FR 11A AT -Y592 IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 232NF BETWEEN FR22 TO FR25, -Y1382. REPAIRED FLOOR PANEL 232NF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEEN FR 37.4 AND FR 40 AT -Y1959. REPLACED SEAT TRACK BETWEEEN FR 37.4 AND FR 40 AT -Y1959 IAW A330 SRM 51-42-11, 51-72-11 AND EA 134552. UPON FURTHER EVALUATION CORROSION WAS FOUND TO BE LEVEL 2.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

C11 CHECK - DISBONDING ON FLOOR PANEL 271PF BETWEEN FR78 TO FR80, -Y450. REPLACED FLOOR PANEL 271PF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - BALL MAT PANEL 151AG CRACKED AT FR 63 AND +Y1193.8. REPAIRED BALL MAT PANEL 151AG AT FR 63 AND +Y1193.8 IAW CMM 25-59-65.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

ON S2 CHECK, FOUND LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR 40.3 TO 41, -Y953. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 261DH BETWEEN FR53.6 TO FR53.7, Y1580. REPAIRED FLOOR PANEL 261DH IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION AROUND INSERTS OF FLOOR PANEL 271MF BETWEEN FR75 TO FR78 & BETWEEN -Y450 TO Y450. REPLACED FLOOR PANEL 271MF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 271FF BETWEEN FR73 TO FR75 & BETWEEN -Y450 TO Y450. REPLACED FLOOR PANEL 271FF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER & LOWER SURFACE OF FLOOR PANEL 272KF BETWEEN FR73 TO FR75, -Y1959. REPAIRED FLOOR PANEL 272KF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION AROUND INSERTS OF FLOOR PANEL 241GF BETWEEN FR31 TO FR33 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 241GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

S2 CHECK - TORN AND CORRODED FLOOR PANEL 242CF BETWEEN FR30 TO FR33, BETWEEN -Y953 TO -Y1456. REPLACED FLOOR PANEL 242CF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 272AG BETWEEN FR71 TO FR73, -Y1382. REPAIRED FLOOR PANEL 272AG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 251JG BETWEEN FR47 TO FR51 Y1382. REPAIRED FLOOR PANEL 251JG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 271AG BETWEEN FR71 TO FR73 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 271AG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 261RF BETWEEN FR55 TO FR57.1, Y740. REPAIRED FLOOR PANEL 261RF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION AROUND INSERTS OF FLOOR PANEL 271HF BETWEEN FR73 TO FR75 & BETWEEN Y750 TO Y953. REPLACED FLOOR PANEL 271HF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 241BF BETWEEN FR30 TO FR33, Y592. REPAIRED FLOOR PANEL 241BF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 231BF BETWEEN FR15A TO FR19 & BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 231BF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 272HF BETWEEN FR73 TO FR75 & BETWEEN -Y453 TO -Y1456. REPLACED FLOOR PANEL 272HF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 241DF BETWEEN FR34 TO FR35, Y1975. REPAIRED FLOOR PANEL 241DF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 271GF BETWEEN FR73 TO FR75 & BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 271GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 261VG BETWEEN FR67 TO FR68, Y790. REPAIRED FLOOR PANEL 261VG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 272GF BETWEEN FR73 TO FR75 & BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 272GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 252JF BETWEEN FR37 TO FR39, -Y1580. REPAIRED FLOOR PANEL 252JF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 231HF BETWEEN FR19 TO FR22, Y1382. REPAIRED FLOOR PANEL 231HF IAW B767 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261MH BETWEEN FR65 TO FR67, Y0. REPAIRED FLOOR PANEL 261MH IAW B767 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATED FLOOR PANEL 231SF BETWEEN FR25 TO FR26.1, BETWEEN Y1185. REPAIRED FLOOR PANEL 231SF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 221ZF BETWEEN FR26.1 TO FR28, Y1975. REPAIRED FLOOR PANEL 221ZF IAW B767 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 221AF BETWEEN FR11 TO FR14, -Y1185. REPAIRED CABIN FLOOR PANEL 221AF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 251CF BETWEEN FR37 TO FR37.4, Y987. REPAIRED FLOOR PANEL 251CF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 242EF BETWEEN FR30 TO FR33, -Y1975. REPAIRED FLOOR PANEL 242EF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 251FF BETWEEN FR37 TO FR39, Y=0. REPAIRED FLOOR PANEL 251FF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 232YF BETWEEN FR26.1 TO FR28, -Y1580. REPAIRED FLOOR PANEL 232YF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 242BF BETWEEN FR31 TO FR34, -Y790. REPAIRED FLOOR PANEL 242BF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 231PF BETWEEN FR22 TO FR25, Y1975. REPAIRED FLOOR PANEL 231PF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 251TG BETWEEN FR53.2 TO FR55, Y=0. REPAIRED FLOOR PANEL 251TG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 231VF BETWEEN FR26.1 TO FR28, Y0. REPAIRED CABIN FLOOR PANEL 231VF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251CG BETWEEN FR47 TO FR51, Y1580. REPAIRED CABIN FLOOR PANEL 251CG A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 261QF BETWEEN FR55 TO FR57.1, Y=0. REPAIRED FLOOR PANEL 261QF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 251NG BETWEEN FR36 TO FR53.2, Y1975. REPAIRED FLOOR PANEL 251NG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 251HG BETWEEN FR47 TO FR51, Y790. REPAIRED FLOOR PANEL 251HG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251GF BETWEEN FR34 TO FR39, Y790. REPAIRED CABIN FLOOR PANEL 251GF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251HF BETWEEN FR37 TO FR39, Y1185. REPAIRED CABIN FLOOR PANEL 251HF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261EH BETWEEN FR60 TO FR62, Y1383. REPAIRED FLOOR PANEL 261EH IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 242DF BETWEEN FR31 TO FR34, -Y1580. REPAIRED CABIN FLOOR PANEL 242DF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251DG BETWEEN FR42 TO FR47, Y1185. REPAIRED CABIN FLOOR PANEL 251DG A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 251LF BETWEEN FR38 TO FR39.2, Y0. REPAIRED FLOOR PANEL 251LF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261GG BETWEEN FR60 TO FR62, -Y790. REPAIRED FLOOR PANEL 261GG IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 231FF BETWEEN FR19 TO FR22, Y592. REPAIRED FLOOR PANEL 231FF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED CABIN FLOOR PANEL 251AG AT FR40, Y1975. REPAIRED FLOOR PANEL 251AG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262DF BETWEEN FR53.4 TO FR53.6, -Y1185. REPAIRED FLOOR PANEL 262DF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 251HF BETWEEN FR31 TO FR39, Y1185. REPAIRED FLOOR PANEL 251HF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 241HF BETWEEN FR33 TO FR37, Y987. REPLACED FLOOR PANEL 241HF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262BF BETWEEN FR53.4 TO FR53.6, -Y790. REPAIRED FLOOR PANEL 262BF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261BF BETWEEN FR53.4 TO FR53.9, Y595. REPAIRED FLOOR PANEL 261BF IAW A330 AMM 25-28-43.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR18 TO FR19, Y450. REPLACED SEAT TRACK BETWEEN FR18 TO FR19, Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR53.4 TO FR53.6, Y1382. REPAIRED FLOOR PANEL 261DF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261LG BETWEEN FR62 TO FR63, Y=0. REPAIRED FLOOR PANEL 261LG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251QF BETWEEN FR37 TO FR53.2, Y1975. REPAIRED CABIN FLOOR PANEL 251QF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261LT BETWEEN FR57.1 TO FR58, Y1382. REPAIRED FLOOR PANEL 261LT IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261WF BETWEEN FR57.1 TO FR58, -Y790. REPAIRED FLOOR PANEL 261WF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 231MF BETWEEN FR22 TO FR25, Y1185. REPAIRED CABIN FLOOR PANEL 231MF IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 241CF BETWEEN FR30 TO FR34, Y1185. REPAIRED CABIN FLOOR PANEL 241CF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CRACK ON CABIN FLOOR PANEL 251XF AT FR40, Y1185. REPAIRED CABIN FLOOR PANEL 251XF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATED FLOOR PANEL 261FH BETWEEN FR62 TO FR65, BETWEEN Y1382. REPAIRED FLOOR PANEL 261FH IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261WG BETWEEN FR57.1 TO FR58, Y790. REPAIRED FLOOR PANEL 261WG BETWEEN FR57.1 TO FR58, Y790 IAW A330 AMM 25-28-43.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 252DG BETWEEN FR39 TO FR47, -Y953. REPAIRED FLOOR PANEL 252DG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR11 TO FR14, -Y1185. REPAIRED FLOOR PANEL 221EF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON CABIN FLOOR PANEL 231GF BETWEEN FR19 TO FR22, Y1185. REPAIRED FLOOR PANEL 231GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DISBONDED CABIN FLOOR PANEL 251BG BETWEEN FR42 TO FR47, Y=0. REPAIRED CABIN FLOOR PANEL 251BG A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATED CABIN FLOOR PANEL 222JF BETWEEN FR14 TO FR17, -Y592. REPAIRED CABIN FLOOR PANEL 222JF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 271AF BETWEEN FR71 TO FR73, Y=0. REPAIRED FLOOR PANEL 271AF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 221CF BETWEEN FR11 TO FR19, Y1975. REPAIRED FLOOR PANEL 221CF IAW B767 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 262GF BETWEEN FR53.4 TO FR53.7, BETWEEN -Y1456 TO -Y1959. REPLACED FLOOR PANEL 262GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 271CF BETWEEN FR71 TO FR73 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL 271CF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 241TF BETWEEN FR31 TO FR33, BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 241TF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 212KF BETWEEN FR10A TO FR11A, BETWEEN -Y1456 TO -Y1959. REPLACED FLOOR PANEL 212KF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252XF BETWEEN FR39 TO FR47, -Y953. REPAIRED FLOOR PANEL 252XF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATED FLOOR PANEL 232BF BETWEEN FR15A TO FR19, BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 232BF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 252CF BETWEEN FR37 TO FR37.4, -Y450. REPLACED FLOOR PANEL 252CF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATED FLOOR PANEL 242FF BETWEEN FR33 TO FR37, BETWEEN -Y450 TO Y450. REPLACED FLOOR PANEL 242FF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATED FLOOR PANEL 242GF BETWEEN FR33 TO FR37, BETWEEN -Y450 TO -Y953. REPLACED FLOOR PANEL 242GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 272BF BETWEEN FR71 TO FR73, BETWEEN -Y450 TO -Y953. REPAIRED FLOOR PANEL 272BF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252AG BETWEEN FR39 TO FR47, -Y1959. REPAIRED FLOOR PANEL 252AG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252LG BETWEEN FR47 TO FR53.2, BETWEEN -Y1959. REPAIRED FLOOR PANEL 252LG IAW A330 SRM 53-00-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR 33 AND -Y953. REPLACED SEAT TRACK AT FR 33 AND -Y953 IAW A330 SRM SRM 53-21-15, 51-42-11, 53-00-15 FIG 101, 51-44-11. UPON FURTHER EVALUATION CORROSION WAS FOUND TO BE LEVEL 2.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 261VG BETWEEN FR67 TO FR69, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 261VG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CRACKED FLOOR PANEL 261DH BETWEEN FR67 TO FR69, BETWEEN -Y450 TO Y450. REPLACED FLOOR PANEL 261DH IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATED FLOOR PANEL 241GF BETWEEN FR33 TO FR37, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 241GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 272CF BETWEEN FR71 TO FR73, BETWEEN Y953 TO Y1456. REPLACED FLOOR PANEL 272CF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 271BF BETWEEN FR71 TO FR73, BETWEEN Y450 TO Y953. REPLACED FLOOR PANEL 271BF IAW A330 SRM 53-00-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR32 TO FR37, -Y450. REPLACED SEAT TRACK BETWEEN FR32 TO FR37, -Y450 IAW A330 SRM 51-42-11 & 51-72-11.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252PG AT FR53.2, -Y953. REPAIRED FLOOR PANEL 252PG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 251PF BETWEEN FR39 TO FR39.2, Y1456. REPAIRED FLOOR PANEL 251PF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CRACKED FLOOR PANEL 262FH BETWEEN FR62 TO FR65, -Y1580. REPAIRED FLOOR PANEL 262FH IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR11 TO FR14, Y1459. REPLACED FLOOR PANEL 221DF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 252YF BETWEEN FR39 TO FR47, -Y1175. REPLACED FLOOR PANEL 252YF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATED FLOOR PANEL 251YF BETWEEN FR40 TO FR42, Y1456. REPAIRED FLOOR PANEL 251YF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 262WF BETWEEN FR55 TO FR58, AT -Y790. REPAIRED FLOOR PANEL 262WF IAW A330 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR42 TO FR47, -Y450. REPLACED SEAT TRACK BETWEEN FR42 TO FR47, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 262VG BETWEEN FR58 TO FR69, -Y790. REPAIRED FLOOR PANEL 262VG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 252SF BETWEEN FR39 TO FR47, -Y953. REPLACED FLOOR PANEL 252SF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDING ON UPPER SURFACE OF FLOOR PANEL 231CG BETWEEN FR26.4 TO FR31, Y1459. REPLACED FLOOR PANEL 231CG IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 252GF BETWEEN FR37.4 TO FR39, -Y953. REPLACED FLOOR PANEL 252GF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 261JF BETWEEN FR53.5 TO FR53.9, -Y1175. REPLACED FLOOR PANEL 261JF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252DF BETWEEN FR37 TO FR37.4, -Y1959. REPAIRED FLOOR PANEL 252DF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - UPPER SURFACE DISBONDED ON FLOOR PANEL 262HF BETWEEN FR53.5 TO FR53.9, -Y790. REPLACED FLOOR PANEL 262HF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 252EG BETWEEN FR37 TO FR47, -Y2462. REPAIRED FLOOR PANEL 252EG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 262MF BETWEEN FR53.9 TO FR55, AT -Y1185. REPAIRED FLOOR PANEL 262MF IAW A330 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 251VF BETWEEN FR39.2 TO FR40, Y1959. REPAIRED FLOOR PANEL 251VF IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 261ZG BETWEEN FR69 TO FR72, Y1577.5. REPAIRED FLOOR PANEL 261ZG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DISBONDED FLOOR PANEL 251PG BETWEEN FR51 TO FR53.2, Y953. REPAIRED FLOOR PANEL 251PG IAW A330 SRM 53-00-02.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 272KF BETWEEN FR73 TO FR75 & BETWEEN -Y1447 TO -Y794. REPLACED FLOOR PANEL 272KF IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR75 TO FR76 & BETWEEN -Y794.3 TO -Y1137.1. REPLACED FLOORBEAM BETWEEN FR75 TO FR76 & BETWEEN -Y794.3 TO -Y1137.1 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 222KF BETWEEN FR14 TO FR17, BETWEEN -Y1959 TO -Y1456. REPLACED FLOOR PANEL 222KF IAW TYPICAL REPAIR 330-5302-11-0330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR37.4 TO FR40, -Y450. REPLACED SEAT TRACK BETWEEN FR37.4 TO FR40, -Y450 IAW A330 SRM 53-31-15 FIG 103 & 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 221GF BETWEEN FR14 TO FR17 & BETWEEN Y1959 TO Y2462. REPLACED FLOOR PANEL 221GF IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 242TF BETWEEN FR33 TO FR35, -Y1456. REPLACED FLOOR PANEL 242TF IAW AIRWAYS TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 271KF BETWEEN FR73 TO FR76, Y1447.8. REPLACED FLOOR PANEL 271KF IAW AIRWAYS TYPICAL REPAIR TR330-5302-11-0330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR32 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR32 TO FR37, Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 221KF BETWEEN FR13 TO FR16, Y1959. REPLACED FLOOR PANEL 221KF IAW AIRWAYS TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 241UF BETWEEN FR33 TO FR35, Y1959. REPLACED FLOOR PANEL 241UF IAW TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - CORROSION ON FLOOR PANEL 222GF BETWEEN FR13 TO FR16, -Y1959. REPLACED FLOOR PANEL 222GF IAW AIRWAYS TYPICAL REPAIR TR330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR75, BETWEEN Y794 TO Y1137. REPLACED FLOOR PANEL BETWEEN FR73 TO FR75, BETWEEN Y794 TO Y1137 IAW TYPICAL REPAIR 330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR33 TO FR35, BETWEEN -Y953 TO -Y1959. REPLACED FLOOR PANEL BETWEEN FR33 TO FR35, BETWEEN -Y953 TO -Y1959 IAW TYPICAL REPAIR 330-5302-11-0330.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR73 TO FR75, BETWEEN -Y794.3 TO -Y1137. REPLACED FLOOR PANEL BETWEEN FR73 TO FR75, BETWEEN -Y794.3 TO -Y1137 IAW TYPICAL REPAIR 330-5302-11-0330.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR30, Y450. REPLACED SEAT TRACK AT FR30, Y450 IAW A330 SRM 51-42-11, 53-00-15.

Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CRACK ON FORWARD CARGO COMPARTMENT ROLLER TRAY AT FR25, -Y1460. REPAIRED FORWARD CARGO COMPARTMENT ROLLER TRAY AT FR25, -Y1460 IAW A330 SRM 53-00-14 FIGURE 205, SRM 51-42-11, SRM 51-44-11.

Part: LINK — CRACKED (TE FLAP) · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CRACK IN LEFT WING NR 3 FLAP TRACK REAR LINK ASSEMBLY AT WS 9184 BETWEEN RIB 13 & RIB 14. REPLACED LEFT WING NR 3 FLAP TRACK REAR LINK ASSEMBLY IAW A330 AMM 27-54-75.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR33, Y=0. REPLACED FLOOR SUPPORT AT FR33, Y=0 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

ON S2 CHECK FOUND CORROSION ON SEAT TRACK BETWEEN FR53.2 TO FR53.4, -Y953. REPLACED SEAT TRACK IAW SRM 51-42-11, 51-40-02 & 53-31-15 FIGURE 101 SHEET 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR35 AND +Y1959. REPLACED SEAT TRACK AT FR35 AND +Y1959 IAW A330 SRM 51-21-11, 51-42-11, 51-44-11, 53-00-15 FIG 101. UPON FURTHER EVALUATION CORROSION WAS FOUND TO BE LEVEL 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR74 TO FR76, -Y1477.8. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR76, -Y1477.8 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON LONGITUDINAL BEAM AT FR 71 AND -Y794.3. REPLACED LONGITUDINAL BEAM AT FR 71 AND -Y794.3 IAW A330 SRM 53-41-14.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR73 TO FR74, -Y794.3. REPLACED LONGITUDINAL BEAM BETWEEN FR73 TO FR74, -Y794.3 IAW SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,203 hrs · 6,971 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 241JF BETWEEN FR33 TO FR37, Y953. REPAIRED FLOOR PANEL 241JF IAW A330 SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

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

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON ADAPTER BETWEEN FR73 TO FR74, Y1168. REPLACED ADAPTER BETWEEN FR73 TO FR74, Y1168 IAW A330 SRM 53-41-140, 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR73, Y=0. REPLACED SEAT TRACK BETWEEN FR32 TO FR37, -Y450 IAW A330 SRM 51-42-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1137.1. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR76, -Y1137.1 IAW A330 SRM 53-41-14 FIGURE 103, SRM 51-42-11 & SRM 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

DURING S2 CHECK, FOUND CORROSION ON SEAT TRACK BETWEEN FRAME 33 TO 35, Y953. REPLACED SEAT TRACK IAW SRM 51-21-11, 51-44-11, 51-42-11 & 53-00-15 FIGURE 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR78, Y=0. REPLACED FLOOR SUPPORT AT FR78, Y=0 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON L4 DOOR SILL FLOOR COVER PLATE BETWEEN FR75 TO FR76, Y2462. REPLACED L4 DOOR SILL FLOOR COVER PLATE BETWEEN FR75 TO FR76, Y2462 IAW A330 SRM 51-42-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR73 TO FR74, Y2462. REPLACED LONGITUDINAL BEAM BETWEEN FR73 TO FR74, Y2462 IAW A330 SRM 53-41-14 FIG 103 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR74, Y794.3. REPLACED CORROSION ON FLOOR SUPPORT AT FR74, Y794.3 IAW SRM A330 53-41-14 FIGURE 103, SRM 51-42-11 & SRM 51-75-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

S2 CHECK - CORROSION ON LONGITUDINAL BEAM AT FR 73 AND -Y794.3. REPLACED ON LONGITUDINAL BEAM AT FR 73 AND -Y794.3 IAW A330 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR17 TO FR18, -Y450. REPLACED SEAT TRACK BETWEEN FR17 TO FR18, -Y450 IAW A330 SRM 51-42-11, 51-42-11 & 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR17 TO FR18, Y450. REPLACED SEAT TRACK BETWEEN FR17 TO FR18, Y450 IAW A330 SRM 53-00-15 FIG 101 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,203 hrs · 6,971 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR17, -Y953. REPLACED SEAT TRACK AT FR17, -Y953 IAW A330 SRM 53-11-15 FIG 101 & 51-42-11.

Part: LENS — LOOSE (CABIN) · airframe 49,839 hrs · 6,923 cycles

FCO - SEAT 11G - EMERGENCY EXIT LIGHT IS HANGING LOOSE FROM RECEPTACLE. SEAT-MOUNTED EMERGENCY LIGHT LENS REPLACED. P/N 25-1435-3. ALL CHECKS SATISFACTORY AT 11G SEAT.

Part: LIGHT — LOOSE (CABIN)

MAD - THE 11G EMERGENCY FLOOR LIGHT LOOSE. THE 11G EMERGENCY FLOOR LIGHT REPOSITIONED AND SECURED.

Part: HANDLE — OUT OF SEQUENCE (L4 DOOR)

CLT - PRE-FLIGHT 4L CABIN DOOR DIFFICULT TO CLOSE. DISCOVERED OPEN ABOUT 4 INCHES. DOOR JAMMED: WILL NOT OPEN OR CLOSE. FOUND DOOR OUT OF SEQUENCE. RE-SEQUENCED DOOR HANDLE. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN)

PHL - LIGHT BURNED OUT - EMER EXIT LIGHT ON TOP AT L2 DOOR. SECURED LIGHT CONNECTION. CHECKS OK.

Part: SLIDE — BINDING (R2 DOOR)

DURING A SLIDE OPERATIONAL TEST, THE R2 DOOR SLIDE DID NOT PROPERLY FUNCTION. IT WAS OBSERVED AS: "DOOR ASSIST BOTTLE DISCHARGED, BUT DOOR DID NOT OPEN FULLY. SLIDE GIRT WAS RESTRICTING DOOR FROM OPENING. SLIDE BOTTLE NEVER DISCHARGED." MAINTENANCE REPLACED THE SLIDE. VENDOR OVERHAULED EVACUATION SLIDE/RAFT.

Part: LIGHT — INOPERATIVE (CABIN)

PHL - ROW 6AB EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 6AB.

Part: CYLINDER — LOW PRESSURE (R1 DOOR)

CLT - THE R1 DOOR ASSIST OPERATIONAL CYLINDER HAS LOW BOTTLE PRESSURE. MAINTENANCE SERVICED THE R1 DOOR ASSIST EMERGENCY OPERATIONAL CYLINDER.

Part: FASTENER — LOOSE (CENTER WING) · airframe 48,079 hrs · 6,693 cycles

CLT - TRACES OF FUEL HAVE BEEN FOUND IN THE CENTER WING DRY BAY OF A330-300 AIRCRAFT AT RIB 1. AS A RESULT OF THIS AN INSPECTION WAS PERFORMED ON THIS AIRCRAFT & FASTENERS WERE FOUND LOOSE & LEAKING WITH CRACK INDICATIONS AT FR42 LEFT & RIGHT SIDE AT RIB 1. THE VERTICAL ANGLES WAS REPAIRED IAW EA 102883 & THE BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102864A.

Part: WIRE HARNESS — FAULTY (LANDING GEAR)

CLT - FLT 9225 PHL TO CLT. WHEN THE LANDING GEAR WAS LOWERED, THE CREW RECEIVED A "L/G SYS DISAGREE" ECAM WARNING. THE FLIGHT DID A GO-AROUND. ON THE SECOND APPROACH, THE LANDING GEAR EXTENDED NORMALLY, WITH NO ECAM WARNINGS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED HARNESS 1M AND 2M. ALSO, THE NLG STRUT WAS SERVICED. THE SYSTEM WAS OPERATIONALLY AND LEAK CHECKED OK.

Part: GEARBOX — MISRIGGED (NLG STEERING)

FLT 728. AFTER NORMAL LANDING, WHEN THE FLIGHT ATTEMPTED TO TURN OFF THE RUNWAY, THE CREW FELT A SHUDDERING THROUGH THE AIRCRAFT. ALSO, THE AIRCRAFT CONTINUED TO GO STRAIGHT AS THE CREW WAS MAKING THE ATTEMPT TO TURN. THE CREW STOPPED THE AIRCRAFT AND WAITED FOR A TOW TO THE GATE. THE AIRCRAFT WAS TOWED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BSCU AND SENSORS 3GC, AND 4GC. THE FAULT WAS STILL PRESENT. MAINTENANCE THEN RIGGED THE RIGHT SENSOR GEARBOX. THE NOSE WHELL STEERING DATA CHECK WAS SATISFACTORY. THE ORIGINAL BSCU WAS RE-INSTALLED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

LGW - THE FORWARD FACING CREW SEAT DOOR L1 TORCH LED WAS NOT FLASHING WITHIN 10 SECONDS. MAINTENANCE REPLACED THE TORCH BATTERY.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 46,531 hrs · 6,484 cycles

CWF - EES - C2 - R4 DOOR POWER ASSIST BOTTLE IN YELLOW BAND. CHARGED R4 DOOR POWER ASSIST BOTTLE IAW A330 AMM 52-10-00-600-802.

Part: RIB — CRACKED (RT WING) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - TWO CRACKS ON RIGHT WING RIB 6 FROM AFT FUEL PIPE PASS TO UPPER AFT MOUNT BOLT HOLE AND FROM TOP OF MOUNT BOLT HOLE TO RIB 6 APERTURE. REPAIRED RIGHT WING RIB 6 IAW EO 5706U238 AND AIRWASY EA102273.

Part: PIN — CORRODED (LT MLG) · corrosion level 2 · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - LEVEL 2 PITTING CORROSION ON LEFT HAND AFT MAIN LANDING GEAR PINTLE PIN ON NUT END OF THE CHROME. REPLACED LEFT HAND AFT MAIN LANDING GEAR PINTLE PIN IAW A330 AMM 32-11-11.

Part: LINK — CORRODED (MLG) · corrosion level 2 · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - LEVEL 2 CORROSION ON LEFT HAND ADJUSTABLE LINK ASSEMBLY AFT PIN WITH CORROSION BETWEEN THREADS & CHROME ON BARREL. REPLACED LEFT HAND ADJUSTABLE LINK ASSEMBLY IAW A330 AMM 32-11-00-210 & JOB CARD 33L73032001.

Part: PIN — CORRODED (LT MLG) · corrosion level 2 · airframe 46,531 hrs · 6,484 cycles

C2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LEFT MAIN GEAR AFT PINTLE PIN. REPLACED LEFT MAIN GEAR AFT PINTLE PIN IAW SRM 32-11-00-210.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271NF BETWEEN FR75 TO FR78 & BETWEEN Y450 TO Y1447.8. REPAIRED FLOOR PANEL 271NF & BETWEEN FR75 TO FR78 BETWEEN Y450 TO Y1447.8 IAW A330 SRM 53-02-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON AUXILIARY FLOOR BEAM AT FR76, -Y1447.8. REPLACED AUXILIARY FLOORBEAM AT FR76, -Y1447.8 IAW A330 SRM 51-42-11 & 53-41-14.

Part: PIN — CORRODED (RT MLG) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON RIGHT MAIN LANGING GEAR AFT PINTLE PIN. REPLACED RIGHT MAIN LANDING GEAR AFT PINTLE PIN IAW A330 SRM 32-11-00-210.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM BETWEEN FR77 TO FR80, -Y1447.8. REPLACED LONGERON BEAM BETWEEN FR77 TO FR82, -Y1447.8 IAW A330 SRM 51-72-11.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON LOWER FUSELAGE BELLY FAIRING PANEL 193BB FORWARD SUPPORT FRAME LOWER FLANGE AT FR40 BETWEEN Y1065 TO -Y1065 & BETWEEN S56L TO S56R. REPLACED LOWER FUSELAGE BELLY FAIRING PANEL 193BB FORWARD SUPPORT FRAME IAW A330 SRM 53-00-15.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CRACK ON ATTACH FITTING AT FORWARD SIDE OF FR80/82, -Y1447.8. REPLACED ATTACH FITTING AT FORWARD SIDE OF FR80/82, -Y1447.8 IAW A330 SRM 51-72-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - EEL - PORTABLE EMERGENCY FLASHLIGHT HAS A DEAD BATTERY AT L-2 DOOR AFT PARTITION. REPLACED BATTERY IN FLASHLIGHT AT L-2 DOOR AFT PARTITION IAW A330 DME CORPORATION CMM 25-60-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - INTERGRAINULAR CORROSION ON FLOOR AUXILLARY BEAM AT FR75A BETWEEN -Y450 TO -Y794.3. REPLACED FLOOR AUXILLARY BEAM AT FR75A BETWEEN -Y450 TO -Y794.3 IAW A330 SRM 57-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR75A TO FR76, -Y1448. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR75A TO FR76, -Y1448 IAW A330 SRM 51-42-11 & 51-41-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR71 TO FR76, Y=0. REPLACED FLOOR SUPPORT BETWEEN FR71 TO FR76, Y=0 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR75, Y450. REPLACED SEAT TRACK BETWEEN FR73 TO FR75, Y450 IAW A330 SRM 51-72-11 & 53-00-15.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR76, Y1137. REPLACED LONGERON BEAM BETWEEN FR75 TO FR76, Y1137 IAW A330 SRM 51-72-11 & 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR78, Y450. REPLACED FLOORBEAM AT FR78, Y450 IAW A330 SRM 51-42-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM AT FR78, Y=0. REPLACED LONGERON BEAM AT FR78, Y=0 IAW A330 SRM 51-72-11.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON LONGERON BEAM AT FR78, -Y450. REPLACED LONGERON BEAM AT FR78, -Y450 IAW A330 SRM 51-42-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR74 TO FR75, -Y450. REPLACED SEAT TRACK BETWEEN FR72 TO FR75, -Y450 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR55 TO FR57.3, -Y450. REPLACED SEAT TRACK BETWEEN FR55 TO FR57.3, -Y450 IAW A330 SRM 53-00-15.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 46,531 hrs · 6,484 cycles

CWF - C2 - MAJOR REPAIR - CORROSION ON FLOOR LONGERON FRAME BETWEEN FR75 TO FR76, Y450. REPLACED FLOOR LONGERON FRAME BETWEEN FR75 TO FR78, Y450 IAW A330 SRM 51-42-11 & 51-72-11.

Part: GIRT BAR — DAMAGED (L2 DOOR)

PHL - THE L2 ENTRY DOOR WAS FOUND DIFFICULT TO ARM DURING A CHECK. REMOVED AND REPLACED DOOR L2 GIRT BAR ASSEMBLY.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

PHL - THE PORTABLE FLASHLIGHT AT R1 DOOR WAS NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT AT R1 DOOR.

Part: BATTERY — DISCHARGED (CABIN)

PHL - CABIN EMERGENCY LIGHTING BATTERY CAPACITY CHECK, 8 UNITS FAILED. REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERIES AS REQUIRED.

Part: MEGAPHONE — INTERMITTENT (CABIN)

PHL - THE LEFT HAND GALLEY MEGAPHONE WAS INTERMITTENT. MEGAPHONE WAS REPLACED.

Part: BOLT — SHEARED (L4 DOOR)

L4 DOOR ASSIST SNUBBER BOLD SHEARED. MAINTENANCE REPLACED BOLT ASSY.

Part: BATTERY — DISCHARGED (CABIN)

AFT LEFT EPSU BATTERY FAILS JOB CARD. MAINTENANCE REPLACED BATTERY AFT LEFT EPSU.

Part: GIRT BAR — BENT (L1 DOOR)

FRA - THE L1 DOOR WILL CLOSE, BUT THE EMERGENCY SLIDE WILL NOT ARM. MAINTENANCE STRAIGHTENED OUT THE BENT GIRT BAR ON DOOR L1.

Part: BATTERY PACK — DIRTY (CABIN) · airframe 38,858 hrs · 5,459 cycles

BFM - C1 - EES - MAIN CABIN DOOR 4L FAILS EMERGENCY POWER SUPPLY TEST. RESEATED & CLEANED BATTERY PACK CONTACTS IAW A330 AMM 33-51-38.

Part: INLET — ERODED (NR 2 COWLING) · airframe 41,783 hrs · 6,901 cycles

BFM - C1 - MAJOR REPAIR - NR 2 ENGINE INLET COWL ERODED AT ALUMINUM LIP COMPOSITE SECTION. CLEANED & PREPPED AREA, BONDED SEALER & REPAIR MATERIALS.

Part: FAIRING — CORRODED (FUSELAGE) · airframe 38,856 hrs · 5,458 cycles

BFM - C1 - MAJOR REPAIR - SEVERAL SPOTS OF CORROSION ON FUSELAGE LOWER SECTION BELLY FAIRING AT FR44. REPAIRED FUSELAGE LOWER SECTION BELLY FAIRING AT FR44 IAW A330 SRM 51-42-11.

Part: ATTACH FITTING — CORRODED (LT PYLON) · airframe 38,545 hrs · 5,414 cycles

PHL - ENGINE CHANGE - MAJOR REPAIR - EXFOLIATION OF CADMIUM COATING ON MATING SURFACE OF LEFT PYLON TO ENGINE ATTACH FITTING MATING SURFACE. REPAIRED CADMIUM COATING ON MATING SURFACE OF LEFT PYLON TO ENGINE ATTACH FITTING MATING SURFACE IAW A320 AMM 20-2015-05.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 32,862 hrs · 4,651 cycles

BFM - MAJOR REPAIR - C2 CHECK - NR 6048974, CORROSION ON SEAT TRACK, BS 4470/FR 55 - BS 4842/FR 58, -Y450. REPLACED SEAT TRACK, BS 4470/FR 55 - BS 4842/FR 58, -Y450 IAW A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 32,862 hrs · 4,651 cycles

BFM - MAJOR REPAIR - C2 CHECK - NR 6048975, CORROSION ON SEAT TRACK, BS 4842/FR 58 - BS 5372/FR 68, -Y450. REPLACED SEAT TRACK, BS 4842/FR 58 - BS 5372/FR 68, -Y450 IAW A330 SRM 53-41-15.