N274AY

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 87,611 hrs · 12,536 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR EMERGENCY BOTTLE LOW PRESSURE. MAINTENANCE SERVICED DOOR DAMPER TO PROPER PRESSURE PER AMM 52-22-00-600-801A.

Part: FIRE BOTTLE — DISCHARGED (LAVATORY) · airframe 83,639 hrs · 12,011 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY L11 FIRE EXTINGUISHER DISCHARGED. MAINTENANCE REPLACED LAVATORY L11 FIRE EXTINGUISHER BOTTLE PER AMM 26-25-41 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 82,654 hrs · 11,871 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY POWER SUPPLY UNIT IN THE FORWARD LEFT HAND PASSENGER CABIN DOES NOT PASS THE OPERATIONAL TEST. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-400-801-A.

Part: MONITOR — MALFUNCTIONED (CABIN) · airframe 82,561 hrs · 11,859 cycles

PHL FLT 715 EN-ROUTE VCE - PHL. THE AIRCRAFT WAS NOT GROUNDED. VIDEO AT SEAT 22C INOP. PAX REPORTED SMELL AFTER UNIT SHUT DOWN. MAINTENANCE REPLACED MONITOR IAW AMM 23-32-00. OPS CK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,430 hrs · 11,724 cycles

AIRCRAFT IN BASE MAINTENANCE: BATTERY/EMERGENCY POWER SUPPLY UNIT 2L (13WL) FAULT PER TSM 33-51-00-810-802-A. REPLACED L2 EMERGENCY POWER SUPPLY BATTERY, PER AMM33-51-380-008-02,33-51-384-008-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — BINDING (L1 DOOR) · airframe 80,001 hrs · 11,545 cycles

L1 DOOR SLIDE LEVER COVER IS JAMMED. FREED THE SLIDE LEVER COVER.

Part: LEVER — BINDING (L1) · airframe 80,001 hrs · 11,545 cycles

L1 DOOR SLIDE LEVER COVER IS JAMMED, LATCH NEEDS ADJUSTMENT, ICE DRAWER WILL NOT CLOSE. FREED THE L1 DOOR SLIDE LEVER COVER. REPLACED THE LATCH. INSTALLED 7-18 THE ICE DRAWER ON TRACK.

Part: STRINGER — CRACKED (FRAME 53.8) · airframe 79,937 hrs · 11,531 cycles

CRACK INDICATION ON STRINGER 14L, FRAME 53.8. PERFORMED A TIME LIMITED REPAIR ON THE STRINGER IAW EA 278562.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,937 hrs · 11,531 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON STRINGER ( L- PROFILE ) LOCATED BETWEEN FR 53.5 TO FR 53.5A AND STRINGER 15 RIGHT IN PASSENGER CABIN. REPLACED STRINGER PER SRM 51-72-11 AND DRAWING F53370020.

Part: STRINGER — CRACKED (FRAME 53.8) · airframe 79,937 hrs · 11,531 cycles

A CRACK INDICATION FOUND ON STRINGER 14R, FRAME 53.8. PERFORMED A TIME LIMITED REPAIR IAW EA 278561.

Part: RUDDER — CORRODED (ZONE 300) · airframe 79,134 hrs · 11,410 cycles

AIRCRAFT WAS GROUNDED. SIGNS OF CORROSION ON TRAILING EDGE OF RUDDER 50 INCHES ABOVE BASE OF RUDDER. REPAIRED RUDDER PER SRM 55-41-19-300-002, FIGURE 20102.

Part: RUDDER — CORRODED (ZONE 300) · airframe 79,134 hrs · 11,410 cycles

AIRCRAFT WAS GROUNDED. SIGNS OF CORROSION ON TRAILING EDGE OF RUDDER 15 1/2 FEET ABOVE BASE OF RUDDER. REPAIRED RUDDER PER SRM 55-41-19-300-002, FIGURE 20102.

Part: RELAY — STUCK (ZONE 200) · airframe 78,817 hrs · 11,370 cycles

AIRCRAFT WAS GROUNDED. PILOT: UPON ARRIVING AT AIRCRAFT, FOUND BATTERIES OFF WITH APU OFF ELT SWITCH OFF WITH EMERGENCY LIGHTS ON. MAINTENANCE CYCLED POWER BETWEEN GROUND AND APU, RELEASED (RESET) STUCK RELAY AND PERFORMED EMERGENCY LIGHTS TEST PER AMM 33-51-00-710-801A. AS A PRECAUTION, MAINTENANCE REPLACED RELAY 26XE PER AMM 33-51-02.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 78,400 hrs · 11,316 cycles

FOUND THE R3 DOOR BOTTLE BELOW 1783 PSI. ACCOMPLISHED SERVICING OF THE R3 DOOR ASSIST BOTTLE.

Part: LIGHT — BROKEN (CABIN) · airframe 78,136 hrs · 11,285 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 24G BROKEN. REPLACED EMERGENCY LIGHT AT SEAT 24G.

Part: LENS — BROKEN (CABIN) · airframe 77,970 hrs · 11,264 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS BROKEN AT ROW 11G. REPLACED LIGHT ASSEMBLY AT 11G.

Part: LENS — BROKEN (CABIN) · airframe 77,970 hrs · 11,264 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS BROKEN AT ROW 6A. REPLACED LIGHT ASSEMBLY AT 6A.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 77,710 hrs · 11,233 cycles

EXIT SIGN LENS MISSING AFT LEFT BY LAVATORY L73. REPLACED THE LENS.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 76,813 hrs · 11,120 cycles

WHILE ACCOMPLISHING JOB CARD 33C20033004, MAINTENANCE FOUND EMERGENCY LIGHTS AT SEATS 7H TO BE INOPERATIVE. CONNECTORS LOOSE, RECONNECTED AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 76,813 hrs · 11,120 cycles

WHILE ACCOMPLISHING JOB CARD 33C20033004, MAINTENANCE FOUND EMERGENCY LIGHTS AT SEATS 4ATO BE INOPERATIVE. FOUND THE CONNECTORS LOOSE, RECONNECTED AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKED.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 75,437 hrs · 10,901 cycles

AIRCRAFT IN BASE MAINTENANCE. DAMAGED EMERGENCY EXIT LIGHT LENS AT L3 DOOR. REPAIRED EXIT SIGN AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — FAULTED (ESCAPE SLIDE) · airframe 75,245 hrs · 10,869 cycles

L3 DOOR ESCAPE SLIDE EMERGENCY LIGHT FAULT INDICATED DURING EMERGENCY POWER SUPPLY UNIT OPERATIONAL CHECK. MAINTENANCE REPLACED THE THE SLIDE.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

EMERGENCY LIGHTS FAULTED DURING OPS TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

AIRCRAFT IN BASE MAINTENANCE. FAULTED DURING EMERGENCY LIGHTS OP'S TEST, EMERGENCY POWER SUPPLY UNIT AT 1R (12WL). REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

EMERGENCY LIGHTS FAULTED DURING OPS TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

EMERGENCY LIGHTS FAULTED DURING OPS TEST. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

EMERGENCY LIGHTS FAULTED DURING OPS TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,240 hrs · 10,869 cycles

EMERGENCY LIGHTS FAULTED DURING OPS TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY.

Part: SLIDE — FAULTED (L3 DOOR) · airframe 75,240 hrs · 10,869 cycles

AIRCRAFT WAS NOT GROUNDED: DURING A19 CHECK, L3 ESCAPE SLIDE FAULT INDICATED IN CIDS. REPLACED SLIDE PACK ON L3 PER JOB CARD 33L80025001.

Part: SIGN — BROKEN (CABIN) · airframe 75,115 hrs · 10,848 cycles

AIRCRAFT WAS NOT GROUNDED. BROKEN EXIT SIGN AT DOOR 3R. REPLACED EXIT SIGN AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR SLIDE) · airframe 74,665 hrs · 10,782 cycles

R4 DOOR INDICATES DOOR ARMED WHEN ARMIMG LEVER IS NOT FULLY ENGAGED. MAINTENANCE REMOVED DEBRIS FROM GIRT BAR AT DOOR 4R, ARMED AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 52-13-22.

Part: COVER — MISSING (CABIN) · airframe 74,234 hrs · 10,722 cycles

EMERGENCY EXIT LIGHT COVER MISSING IN AFT GALLEY. INSTALLED LIGHT COVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COVER — JAMMED (L1 DOOR) · airframe 74,194 hrs · 10,717 cycles

1 LEFT DOOR ARMING COVER WON’T COME DOWN. COVER FOUND JAMMED BEYOND END STOP COVER RELEASED AND NOW OPS OK IAW AMM 52 10 00. THE AIRCRAFT WAS NOT GROUNDED.

Part: FLOORBEAM — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON CABIN FLOORBEAM AT FRAME 37 AND Y863. REPLACED FLOOREAM IAW EA 263885A.

Part: FITTING — FAILED (L4 DOOR) · airframe 74,110 hrs · 10,705 cycles

L4 DOOR FORWARD HEATED SLIDE LOCK MECHANISM (23DH) FAILED BITE TEST. REPLACED L4 DOOR FORWARD HEATED SLIDE LOCK MECHANISM (23DH) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECKS PER AMM 30-46-11-04, 30-46-00 & 52-11-00.

Part: DOOR SILL — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN DOOR SILL PLATE BETWEEN FRAMES 73A AND 75 AT Y2462 , STRINGER 26L. REPLACED THE DOOR SILL PLATE IAW SRM 51-73-11 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 71-73) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 71 & 73 AT Y2462. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 70-72) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN SEAT TRACK AT -Y1959 BETWEEN FRAMES 70 TO 72. REPLACED SEAT TRACK IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FRAME 32-33) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON SEAT TRACK AT Y1456 BETWEEN FRAMES 32 AND 33. REPLACED SEAT TRACK IAW SRM 53-00-15 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 31-37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON SEAT TRACK BETWEEN FRAME 31 AND 37.5 AT Y953. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FITTING — CORRODED (FRAME 16) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FORWARD CABIN CROSSBEAM FITTING. LANDING ASSEMBLY BETWEEN Y953 AND Y1450 AT FRAME 16. REPLACED THE FITTING IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FORWARD CABIN CROSSBEAM FITTING AT FR 16 BETWEEN Y1450 AND Y1959. REPLACED THE FITTING IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FORWARD CABIN CROSSBEAM FITTING AT FR 16A BETWEEN Y1450 AND Y1959. REPLACED THE FITTING IAW SRM 51-42-11.

Part: STIFFENER — CRACKED (FRAME 12) · airframe 74,110 hrs · 10,705 cycles

CRACKED STIFFENER AT FRAME 12A AND STRINGER 26L. REPLACED THE STIFFENER IAW SRM 51-42-11.

Part: CROSSBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FORWARD CABIN CROSSBEAM FITTING BETWEEN Y953 AND Y1450 AT FRAME 16A. REPLACED THE FITTING IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 71-72) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 71 AND 72 AT Y1446. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN DOOR SILL PLATE AT STRINGER 25L BETWEEN FRAMES 73A AND FR 75A. REPLACED SILL PLATE IAW SRM 51-73-11 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 69-72) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT Y794.3 BETWEEN FRAMES 69 AND 72. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 AND 53-41-15.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FORWARD CABIN FLOOR SUPPORT AT -Y1450 BETWEEN FRAMES 16 AND 17. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON OUTBOARD SEAT TRACK BETWEEN FRAMES 35 AND 36 AT Y1456. REPLACED THE SEAT TRACK IAW SRM 53-00-15 & 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 74) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOORBEAM, AT Y1137.1 AND FRAME 74. REPLACED THE FLOORBEAM IAW SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FRAME 74) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON FLOORBEAM AT -Y1137.1 AND FRAME 74. REPLACED THE FLOORBEAM IAW SRM 53-41-14.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT FRAME 75 AND -Y450. REPLACED FLOOR SUPPORT IAW SRM 53-41-14-201 FIG 211.

Part: SEAT TRACK — CORRODED (FRAMES 30-33) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON SEAT TRACK AT -Y2462 BETWEEN FRAMES 30 AND 33. REPLACED THE SEAT TRACK IAW SRM 53-00-15-101 & 51-42-11

Part: SEAT TRACK — CORRODED (FRAMES 33-35) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON SEAT TRACK AT -Y953 BETWEEN FRAMES 31 AND 37. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 71) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT FRAMES 71 AND -Y1456. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND 51-44-11.

Part: SEAT TRACK — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON SEAT TRACK AT -Y450 BETWEEN FRAMES 18.5 AND 19.5. REPLACED SEAT TRACK IAW SRM 53-00-15.

Part: DOOR SILL — CORRODED (FRAMES 73-75) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN DOOR SILL PROFILE BETWEEN FR73A AND FR75 AT Y2462. REPLACED DOOR SILL PROFILE IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CHAFED (FRAMES 16-17) · airframe 74,110 hrs · 10,705 cycles

FORWARD CABIN FLOOR SUPPORT CHAFED AT -Y1959 BETWEEN FRAMES 16 AND 17. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 71-73) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 71 AND 73, -Y2462. REPLACED THE FLOOR SUPPORT IAW SRM 51-74-00,SRM 51-42-11, AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 70-72) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y794.3 BETWEEN FRAMES 70 AND 72. REPLACED FLOOR SUPPORT IAW SRM 53-41-14 FIG 104 & 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT SIDE PASSENGER CABIN FLOORBEAM AT FR 73 AND -Y1137. REPLACED FLOORBEAM PER SRM 53-41-14, SRM 51-42-11, AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON CABIN FLOORBEAM UPPER SURFACE AT FRAME 37 BETWEEN Y450 AND Y953. REPLACED THE FLOORBEAM IAW SRM 53-00-14-201 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73A-76) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 73A & 76 AT Y2462. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73A) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON AFT CABIN SEAT TRACK AT FRAME 73A AND Y2462. REPAIRED THE SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 80-82) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT PASSENGER CABIN FLOOR SUPOPRT BETWEEN FRAMES 80 TO 82 AT -Y470. REPLACED FLOOR SUPPORT IAW SRM 53-41-14 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 80-82) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT PASSENGER CABIN FLOOR SUPPORT BETWEEN FRAMES 80 AND 82 AT -Y450. REPLACED CABIN FLOOR SUPPORT SRM 53-41-14 AND 51-42-11.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 74,110 hrs · 10,705 cycles

AFT CABIN FLOOR PANEL 272GF DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT SIDE SEAT TRACK AT FRAME 33 AND -Y1959. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11, AND SRM 53-21-15.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 73 AND 74 AT -Y1220. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON LEFT SIDE CABIN SEAT TRACK AT FRAME 37 AND Y450. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11, AND SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT SIDE SEAT TRACK AT FRAME 37-37.4 AND -Y450. REPLACED THE SEAT TRACK IAW SRM 53-21-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT SIDE CABIN SEAT TRACK AT FRAME 17 AND -Y450. REPLACED THE SEAT TRACK IAW SRM 53-11-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON LEFT SIDE CABIN SEAT TRACK AT FRAME 37.1, Y450. REPLACED THE SEAT TRACK IAW SRM 53-21-15 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 72-75) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT AFT CABIN SEAT TRACK.BETWEEN FRAMES 72 AND 75, -Y450. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 51-42-11, AND SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON LEFT AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 73 AND 74 AT Y1244. REPLACED FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11, AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON LEFT AFT CABIN FLOORBEAM AT FRAME 73 TO 73A BETWEEN Y1456 AND Y1959. REPLACED THE FLOORBEAM IAW SRM 51-74-11 AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON RIGHT SIDE CABIN SEAT TRACK AT FRAME 37 AND -Y450. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

CORROSION ON LEFT AFT CABIN FLOOR SUPPORT FROM FRAMES 75 TO 76 AT Y381. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11, AND SRM 51-44-11.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 74,110 hrs · 10,705 cycles

CABIN FLOOR PANEL 251BF HAS CORNER EDGE DISBONDED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,110 hrs · 10,705 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON AFT CABIN BEAM, LONGERON BETWEEN FRAME 75 AND FRAME 76. REPLACED BEAM, LONGERON IAW SRM 53-41-14, FIG 101, 51-42-11.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 74,110 hrs · 10,705 cycles

FORWARD CARGO FLOOR PANEL 132PF HAS CRACK. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 73,855 hrs · 10,671 cycles

EXIT SIGN LENS AT L3 DOOR FOUND BROKEN AND CAME OFF. REPLACED THE LENS AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 73,619 hrs · 10,643 cycles

OVERHEAD EXIT SIGN LENS COVER AT 3R IS LOOSE. REPLACED EXIT SIGN ASSEMBLY AT 3R AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-17.

Part: LENS — OUT OF ADJUST (CABIN) · airframe 73,261 hrs · 10,598 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR NOT SEATED RIGHT WHEN CLOSED. LIGHT LENS ADJUSTED ABOVE 3R DOOR BY OPENING AND CLOSING DOOR. DOOR INDICATION, LENS NORMAL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 72,421 hrs · 10,496 cycles

AIRCRAFT WAS GNDED. AFT GALLEY FLOOR PANEL 272GF HAS LARGE SOFT SPOT AREA, BETWEEN GALLEY CART 5 - 16 & ATTENDANT SEAT. REPAIRED FLOOR PANEL IAW EA 259828 & SRM 53-02-00-201 PARAGRAPH 5H.

Part: SIGN — UNSECURE (CABIN) · airframe 72,120 hrs · 10,453 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN AT 3R HAS FALLEN OFF. SECURED EXIT SIGN AT 3R & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — PARTIAL DEPLOY (L2 DOOR) · airframe 71,659 hrs · 10,358 cycles

AIRCRAFT WAS GNDED. 2L DOOR WAS OPENED SLIGHTLY WITH THE DOOR SLIDE ARMED, PARTIAL DEPLOYMENT. REPLACED L2 DOOR SLIDE IAW AMM 25-62-41-400.

Part: COVER — MISSING (CABIN) · airframe 71,594 hrs · 10,343 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT COVER MISSING MID GALLEY ACFT RT. INSTALLED EMER LIGHT COVER IN MID GALLEY.

Part: LENS — MISSING (CABIN) · airframe 71,550 hrs · 10,332 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT SEAT 16B MISSING LENS. REPLACED MISSING LENS.

Part: SENSE LINE — DEFECTIVE (NR 1 ENGINE) · airframe 71,490 hrs · 10,319 cycles

AIRCRAFT WAS GNDED. ENG NR 1 DID NOT DEVELOP TAKEOFF POWER MAS EPR 1.4, RESULTING IN THE CREW ABORTING THE TAKEOFF & RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. REPLACED THE P4.95 SENSE LINE IAW MM 77-10-00. SATISFACTORY OPERATIONAL & POWER ASSURANCE CHECKS WERE ACCOMPLISHED.

Part: SHADE — DIRTY (L1 DOOR) · airframe 71,085 hrs · 10,246 cycles

AIRCRAFT WAS NOT GNDED. 1L DOOR WINDOW SHADE IS STUCK. CLEANED 1L DOOR WINDOW SHADE TRACK. OPERATIONS CHECKED SATISFACTORY.

Part: BATTERY — FAILED (CABIN) · airframe 70,952 hrs · 10,223 cycles

EMERGENCY BATTERY 12WL FAILED BATTERY CAPACITY CHECK. REF JC 33C20033002. REPLACED EMERGENCY BATTERY 12WL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW MM 33-51-3.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,709 hrs · 10,176 cycles

C1 CHECK, RT WING INBD FLAP DELAMINATED AT THE OTBD TE, UPPER & LOWER SURFACE. REPAIRED IAW EA 255261 & SRM 57-54-00-201.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 70,709 hrs · 10,176 cycles

CLASS SEAT 5H & 6H EMER LIGHTS INOPERATIVE. REPLACED LIGHT WIRE HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 35-51-00-710-84-A-01.

Part: CONTROL UNIT — FAILED (ZONE 100)

SLIDE FITTING HEATER CONTROL UNIT, 10DH FAILED OPERATIONAL TEST. REPLACED HEATER CONTROL UNIT. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 30-46-34 & 30-46-00.

Part: BRAKE — OVERHEATED (LT MLG) · airframe 70,030 hrs · 10,077 cycles

FLIGHT 787 EN-ROUTE, LT SIDE BRAKES OVERHEATED AFTER TAKEOFF. DROPPED LG IAW ECAM. TEMP GOT UP TO 325 DEGREES. RT SIDE UNAFFECTED. INSPECTED LT GEAR BRAKES, NO FAULTS OR DEFECTS NOTED. BRAKE TEMPS ARE WITHIN ALLOWABLE LIMITS IAW TSM 32-42-00-810-818-A.

Part: HOOK AND LOOP — UNSECURE (EVAC SLIDE) · airframe 69,947 hrs · 10,066 cycles

1R SLIDE WILL NOT ARM. SECURED VELCRO ON BOTTOM OF SLIDE PACK, DOOR ARMING NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A A CHECK JC 33C22033002, FAULTED EPSU 1R, 2L, 2R, 3L, 4L & 3R. REPLACED BATTERY PACKS AT 1R, 2L, 1L, 2R, 3L, 4L & 3R IAW AMM 33-51-38-400-802A.

Part: FITTING — FAULTY (ZONE 800) · airframe 68,586 hrs · 9,879 cycles

WHILE COMPLYING WITH JC 33T2103001, OPERATIONS CHECK ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION, FOUND THAT THE LIGHT ON CONTROL UNIT DID NOT TEST. R & R R1 DOOR AFT SLIDE FITTING 8DH IAW AMM 30-46-11-400-801A.

Part: ROD END — CORRODED (RT MLG) · corrosion level 2 · airframe 66,635 hrs · 9,534 cycles

GEAR CHANGE RT MLG SHORTENING MECHANISM ADJUSTABLE LINK LOWER ROD END SPLIT BEARING & ATTACH PIN CORRODED. R & R ROD END BEARING ASSEMBLY IAW AMM 32-11-13-400-801A.

Part: LENS — DETACHED (CABIN) · airframe 64,695 hrs · 9,286 cycles

EXIT PANEL 2L OFF. MX REPLACED EMERGENCY LENS DOOR 2L.

Part: COVER — MISSING (CABIN) · airframe 64,282 hrs · 9,233 cycles

3L DOOR EXIT LIGHT COVER MISSING. REPLACED EXIT LIGHT COVER AT 3L DOOR, OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 63,691 hrs · 9,150 cycles

LAVATORY L54 EMERGENCY LIGHT WALL LENS, RED, MISSING. INSTALLED MISSING LIGHT LENS, OPERATIONAL CHECK IS GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 63,457 hrs · 9,121 cycles

DOOR 2L AFT FACING OVERHEAD EXIT SIGN WILL NOT STAY IN PLACE. SECURED EXIT SIGN AT 2L, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,170 hrs · 8,940 cycles

DURING EPSU CAP TEST L2 & R4 BATTERIES FAULTED. R & R BATTERIES AT L2 & R4 POSITION EPSU'S.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

DURING C2 CHECK, A 5 INCH CRACK IN FLOOR PANEL 152UG BETWEEN FRAMES 53.6 TO 54 & BETWEEN -Y953 & -Y1456. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 5I , FIG. 211 & AMM 53-00-00-020-52A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 251VF BETWEEN FRAMES 39.2 TO 40 & Y1959 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 252GF BETWEEN FRAMES 37.4 TO 39 & -Y450 TO -Y953. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 251EF BETWEEN FRAMES 37 TO 37.4 & Y1959 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 231YF BETWEEN FRAMES 26.3 TO 26.1 & Y1456 TO Y1959. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 231TF BETWEEN FRAMES 25 TO 26.1 & Y1456 TO Y1959. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK - DELAMINATION ON FLOOR PANEL 262FH BETWEEN FRAMES 62 TO 65 & -Y953 TO -Y1959. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION FOUND ON FLOOR PANEL 232MF BETWEEN FRAMES 22 TO 25 & -Y953 TO -Y1456. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION FOUND ON FLOOR PANEL 232HF BETWEEN FRAMES 19 TO 22 & -Y1456 TO -Y1959. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 261ZF BETWEEN FRAMES 57.1 TO 58 & Y1959 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 251CF BETWEEN FRAMES 37 TO 37.4 & Y953 TO Y1456. REPLACED FLOOR PANEL 251CF IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION FOUND ON FLOOR PANEL 261UG BETWEEN FRAMES 65 TO 69 & Y1959 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION FOUND ON FLOOR PANEL 252KF BETWEEN FRAMES 37.4 TO 39 & -Y1959 TO -Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION FOUND ON FLOOR PANEL 251MG BETWEEN FRAMES 47 TO FR51 & Y1959 TO Y2462. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 211.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 61,846 hrs · 8,888 cycles

C2 CHECK, DELAMINATION ON FLOOR PANEL 262JF BETWEEN FRAMES 53.7 TO 53.9 & -Y953 TO -Y1456. REPLACED FLOOR PANEL NR IAW SRM 53-02-00, FIG 211.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 61,705 hrs · 8,870 cycles

COVER PLATE ON EMERGENCY LIGHT IS MISSING L73. MX INSTALLED MISSING COVER OPS CHECKED GOOD.

Part: COVER — DETACHED (ZONE 200) · airframe 61,291 hrs · 8,818 cycles

MISSING COVER EMERGENCY LIGHT AT POSITION AFT BULKHEAD WALL NEAR SEAT 25F WIRES EXPOSED. MX FOUND COVER DETACHED, CHECKED FOR INTEGRITY, AND REPOSITIONED CORRECTLY. OPS ARE NORMAL.

Part: ATTACH FITTING — CORRODED (RT NACELLE) · airframe 61,084 hrs · 8,792 cycles

DROP-IN -CORROSION ON RT PYLON FRONT MOUNT PYRAMID FITTING AT NAC RIB 1. REPAIRED RT PYLON FRONT MOUNT PYRAMID FITTING AT NAC RIB IAW EA 105047.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,023 hrs · 8,654 cycles

CIDS 1 BAT/EPSU 1L (11WL) FAULT. MX R & R 1L EMERGENCY LIGHT BATTERY.

Part: SLIDE RAFT — FAULTY (R1 DOOR) · airframe 60,030 hrs · 8,655 cycles

CIDS ESCAPE SLIDE LT SW/EPSU 1R (12WL) FAULT. R & R 1R ESCAPE FACILITIES. OP'S CHECKS NORMAL.

Part: SLIDE RAFT — FAULTY (R1 DOOR) · airframe 60,023 hrs · 8,654 cycles

CIDS ESCAPE SLIDE LT SW/EPSU 1R (12WL) FAULT. MX R & R 1R ESCAPE FACILITIES. OPS CHECK IS NORMAL.

Part: DAMPER — LOW PRESSURE (L3 DOOR) · airframe 59,572 hrs · 8,595 cycles

CUSTOMER CARE VISIT - DOOR 3L DOOR DAMPER REQUIRES SERVICING. SERVICED DOOR 3L DOOR DAMPER & EMERGENCY OPERATION CYCLINDER IAW A330 AMM 52-22-00-600-801-A.

Part: DAMPER — LOW PRESSURE (R3 DOOR) · airframe 59,572 hrs · 8,595 cycles

CUSTOMER CARE VISIT - DOOR 3R DOOR DAMPER REQUIRES SERVICING. SERVICED DOOR 3R DOOR DAMPER & EMERGENCY OPERATION CYCLINDER IAW A330 AMM 52-22-00-600-801-A.

Part: LENS — WRONG PART (CABIN)

CLT - SEAT MOUNTED ESCAPE PATH LIGHTING SEATS 25B AND 25G REQUIRES RED LENSE (CURRENTLY CLEAR). INSTALLED NEW RED LENSES ON EMERGENCY LIGHTING AT GALLEY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,864 hrs · 8,501 cycles

FOUND ON DAILY CHECK L1 DOOR F/A SEAT, EMERGENCY FLASHLIGHT DOES NOT PASS TEST LIGHT CHECK. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT THE FA/L1 DOOR POSITION.

Part: LENS — MISSING (CABIN) · airframe 58,771 hrs · 8,486 cycles

2 EMERGENCY LIGHT LENS FOUND MISSING AT ROW 25. MAINTENANCE REPLACED LENS AS REQUIRED.

Part: SLIDING WINDOW — BURNED (COCKPIT)

LEFT SLIDING WINDOW HAS A BURNED AREA ON THE FWD EDGE OF THE BUS BAR. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SLIDING WINDOW PANE.

Part: COMPUTER — MALFUNCTIONED (WINDOW HEAT)

AT CRUISE, FL400, AT MAXIMUM DIFFERENCE A BANG WAS HEARD AND THE CAPTAIN'S WINDSHIELD CRACKED ALL OVER . IT APPEARS TO BE THE OUTER PANEL. ECAM MSG 'A ICE L WSHLD HEAT'. MAINTENANCE REPLACED THE WINDOW HEAT COMPUTER AND THE CAPTAIN'S WINDSHIELD.

Part: TIRE — LOW PRESSURE (NLG) · airframe 58,079 hrs · 8,390 cycles

FLIGHT 740, PHL-MAD - ECAM INDICATION OF WHEEL TIRE LOW PRESSURE. MAINTENANCE AND DISPATCH DICUSSED AND HAD CFR MEET FLIGHT IN MAD. FLIGHT LANDED WITHOUT INCIDENT AND WAS TOWED TO GATE. MAINTENANCE FOUND NOSE WHEEL N2 WITH 40 PSI. REMOVED NOSE WHEEL N1 AND N2.

Part: SIGN — DETACHED (CABIN) · airframe 57,124 hrs · 8,252 cycles

EXIT SIGN AT DOOR 3L FELL OFF. MAINTENANCE RE-FITTED EXIT SIGN.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 56,129 hrs · 8,123 cycles

EMERGENCY LIGHT ON AT 3L DOOR. MAINTENANCE CYCLED CIDS 1&2. 3L EMERGENCY LIGHT OPERATIONAL CHECK OK.

Part: EPSU — INOPERATIVE (CABIN) · airframe 55,811 hrs · 8,079 cycles

EPSU AT DOOR 4L WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED EPSU AND BATTERY 17WL AT DOOR 4L.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,609 hrs · 7,926 cycles

C1 CHECK - L3 DOOR EMERGENCY EXIT SIGN LENS MISSING. REPLACED L3 DOOR EMERGENCY EXIT SIGN LENS IAW AMM 33-51-13.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,609 hrs · 7,926 cycles

C1 CHECK - L2 DOOR CEILING EMERGENCY EXIT SIGN MISSING AFT LENS. REPLACED MISSING LENS IAW AMM 33-51-16.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 54,609 hrs · 7,926 cycles

C1 CHECK - L4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L4 DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-802-A.

Part: ANGLE — DAMAGED (ZONE 100) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK, BASED ON REPORTS OF FUEL LEAKS, RIB1/FR 42 OUTER ANGLE REPAIRED IAW EA 103588.

Part: ANGLE — DAMAGED (ZONE 100) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK, BASED ON REPORTS OF FUEL LEAKS, RIB 1/FR 42 OUTER ANGLE REPLACED IAW EA 103588.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - 5 INCH LONG CRACK IN FLOORBEAM AT FR63 BETWEEN -Y1318 TO -Y2540. REPLACED FLOOR BEAM AT FR63 BETWEEN -Y1318 TO -Y2540 IAW A330 SRM 53-41-14 FIG 203 & 51-42-11.

Part: BEAM — CRACKED (ZONE 100) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - 6 INCH LONG CRACK IN BEAM ASSEMBLY BETWEEN FR62 TO FR63, -Y1727. REPLACED BEAM ASSEMBLY IAW A330 SRM 51-42-11.

Part: FLANGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON DUCT ASSEMBLY FLANGE BETWEEN FR46 TO FR47, Y254. REPLACED DUCT ASSEMBLY FLANGE BETWEEN FR46 TO FR47, Y254 IAW A330 SRM 51-74-00 & 51-42-11.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - DOOR ASSIST BOTTLES L1 AND L3 AND SERVICING. SERVICED DOOR ASSIST BOTTLE ON DOOR L1 IAW A330 AMM 52-10-00-600-802-A.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - DOOR ASSIST BOTTLES L1 AND L3 AND SERVICING. SERVICED DOOR ASSIST BOTTLE ON DOOR L3 IAW A330 AMM 52-22-00-600-801-A.

Part: FRAME — CORRODED (FAIRING) · corrosion level 2 · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLANGE (BELLY FAIRING FRAME) AT FR39, Y1095. REPLACED FLANGE (BELLY FAIRING FRAME) AT FR39, Y1095 IAW A330 SRM 53-35-14 FIG 104 & 51-42-11.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FRAME LOWER CHORD (BELLY FAIRING) AT FR40 BETWEEN -Y432 TO Y=0. REPAIRED FRAME LOWER CHORD (BELLY FAIRING) AT FR40 BETWEEN -Y432 TO Y=0. IAW A330 SRM 53-35-14 FIG 104 & 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT BETWEEN FR46 TO FR47, Y87. REPLACED FAIRING SUPPORT BETWEEN FR46 TO FR47, Y87 IAW A330 SRM 53-35-14 FIG 104.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 APPROX 3.875 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 APPROX 2.125 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON LEFT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 APPROX 4.125 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 APPROX 3 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 7 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 5 APPROX 3.875 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 5 IAW EO 5511U056.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - MOISTURE INGRESSION ON RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 6 APPROX 4.25 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR SKIN UPPER SURFACE AT ELEVATOR RIB 6 IAW EO 5511U056.

Part: LINKAGE — LACK OF LUBE (EMERGENCY EXIT) · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - EMERGENCY EXIT DOOR 3R FAILED OPERATIONAL CHECK OF THE INTERLOCK MECHANISM. TROUBLESHOOTING DETERMINED PROBLEM WAS STICKING LINKAGE. CLEANED & LUBRICATED LINKAGE IAW A330 AMM 12-22-52. OPS CHECKED INTERLOCK MECHANISM IAW JOB CARD 33C84452001. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,605 hrs · 7,924 cycles

C1 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR30 TO FR36, -Y450. REPLACED SEAT TRACK BETWEEN FR30 TO FR36, -Y450 IAW A330 SRM 53-00-15 FIG 101 SHT 2, 51-44-11 & 51-42-11.

Part: GUST LOCK — JAMMED (L1 DOOR) · airframe 53,809 hrs · 7,816 cycles

FRA - 1L DOOR RELEASE BUTTON STUCK IN DOWN POSITION. UNJAMMED 1L DOOR GUST LOCK, OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,593 hrs · 7,787 cycles

PHL - EMERGENCY FLOOR LIGHTS BY SEATS 16B INOP. MAINTENANCE REPLACED LENS EMERG LT SEAT 16AB, CHECKS OK.

Part: COVER — DETACHED (CABIN) · airframe 53,400 hrs · 7,761 cycles

FCO EMERGENCY LIGHT COVER SEAT 9B NEEDS RE-ATTACHING. POSITION 9B EMERGENCY LIGHT COVER RE-SECURED. POSITION 9B EMERGENCY LIGHT COVER RE-SECURED.

Part: LENS — DAMAGED (CABIN) · airframe 53,357 hrs · 7,756 cycles

PHL - FLOOR LEVEL EMERGENCY LIGHT LENS COVER AT SEAT 16B NEEDS TO BE REPLACED. MAINTENANCE RE-INSTALLED EMERGENCY LENS AT ROW 16 LEFT AS REQUIRED.

Part: STOP FITTING — OUT OF ADJUST (L2 DOOR) · airframe 53,007 hrs · 7,710 cycles

PHL - THE L2 ENTRY DOOR ASSIST CYLINDER FAILED TO DEPLOY DURING OPERATIONAL CHECK PER JC 33L20025001 (ESCAPE SLIDE/RAFT OPERATIONAL CHECK). MAINTENANCE TROUBLESHOT AND FOUND ADJUSTMENT OF DOOR L2 DAMPER AND EMERGENCY OPERATION CYLINDER RELEASE LEVER STOP OUT OF RIG. ADJUSTED LEVER STOP AS REQUIRED. PERFORMED SATISFACTORY OPERATIONAL CHECK. REMOVED SLIDE AND INSTALLED SERVICEABLE SLIDE PER AMM 25-62-41.

Part: COVER — MISSING (CABIN) · airframe 52,857 hrs · 7,691 cycles

EMERGENCY LIGHT COVER AT 16B DOES NOT STAY ATTACHED. FOUND EMERGENCY LIGHT COVER AT 19B MISSING NOT 16B. REPLACED LIGHT COVER AT 19B. PFMD EMERGENCY LIGHT CHECK. ALL EMERGENCY LIGHTS OPS CHECK OK.

Part: COVER — DETACHED (CABIN) · airframe 52,840 hrs · 7,689 cycles

FRA - EMERGENCY LIGHT COVER AT 19B DOES NOT STAY ATTACHED. MAINTENANCE REPLACED LIGHT COVER AT 19B. PERFORMED EMERGENCY LIGHT CHECK, ALL EMERGENCY LIGHTS OPERATIONAL CHECK IS OKAY.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 52,840 hrs · 7,689 cycles

FRA - ON DAILY CHECK FOUND 3L DOOR PRESSURE BOTTLE PRESSURE IN YELLOW. MAINTENANCE SERVICED 3L DOOR PRESSURE BOTTLE PER AMM 52-22-00-600-801-0. OKAY FOR SERVICE.

Part: WIRE — SHORTED (CABIN) · airframe 52,655 hrs · 7,666 cycles

FRA - EMERGENCY LIGHTS LOCATED AT SEATS 9, 13, 19, 23, 25, 28, 33 AND 38 RT SIDE INOP FLT 705. MFF CLT MAINTENANCE FOUND SHORTED WIRE AT SEAT 19R, WHICH BLEW FUSE IN EPSU 16WL. REPAIRED WIRING AT SEAT 19R. REF ESPM20-53-21. REPLACED EPSU 16WL, TESTED GOOD. REF M/M 33-51-38. REPAIRED BROKEN WIRES AT SEATS 25R AND 38R. EMERG LTS AT SEATS TEST GOOD. REF EPSU 20-53-21. EMERG LTS FOR A/C TEST GOOD. REF M/M 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,402 hrs · 7,633 cycles

PHL - EMER LIGHTS INOP AT SEATS G9, G13, G19, G22, G23, G28, AND G33 LAV NR 54 (RED), LAV NR 61 AND AT R4 ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED EPSU'S AT 3R (16WL) AND 4L (17WL) IAW AMM 33-51-38-400. OPS CHECK GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 52,402 hrs · 7,633 cycles

PHL - EMER LIGHTS INOP AT SEATS G9, G13, G19, G22, G23, G28, AND G33 LAV NR 54 (RED), LAV NR 61 AND AT R4 ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED EPSU'S AT 3R (16WL) AND 4L (17WL) IAW AMM 33-51-38-400. OPS CHECK GOOD.

Part: BAFFLE — BURNED (GALLEY) · airframe 52,362 hrs · 7,628 cycles

FLIGHT 721, FCO - CLT - FWD GALLEY RT SIDE OVEN HAS BURNED PLASTIC IN BACK PRODUCING FOUL ODOR IN CABIN DURING FLIGHT. MAINTENANCE REPLACED BAFFLE PLATE & CHECKS GOOD.

Part: EPSU — FAULTY (CABIN) · airframe 52,131 hrs · 7,599 cycles

PHL - EPSU AT DOOR 3R SHOWS UNIT FAULT. MAINTENANCE REPLACED EPSU AND BATTERY PER AMM 33-51-38-400-801. OP'S CHECK OK.

Part: COVER — MISSING (CABIN) · airframe 51,188 hrs · 7,481 cycles

COVER FOR EMERGENCY LIGHT ON BULHEAD ROW 23 A/C LEFT IS MISSING. MAINTENANCE INSTALLED MISSING EMERGENCY LIGHT COVER AT ROW 23 A/C LEFT.

Part: ANGLE — CRACKED (CENTER TANK) · airframe 50,175 hrs · 7,351 cycles

CLT - RON - WHILE TROUBLESHOOTING THE CENTER TANK DRY BAY LEAK ISSUE TWO CRACKS WHERE FOUND ON THE OUTER CHORD VERTICAL ANGLE AT FR 42, RIB 1 LEFT SIDE, NR 7 & NR 8 FASTENER HOLES. REPLACED OUTER CHORD VERTICAL ANGLE AT FR 42, RIB 1 LEFT SIDE, NR 7 & NR 8 FASTENER HOLES IAW ENGINEERING AUTHORIZATION 102915.

Part: FITTING — DAMAGED (CENTER TANK) · airframe 50,175 hrs · 7,351 cycles

CLT - RON - WHILE TROUBLESHOOTING THE CENTER TANK DRY BAY LEAK ISSUE ELONGATED FASTENER HOLES WHERE FOUND ON THE INNER FITTING AT FR 42, RIB 1 LEFT HAND SIDE, HOLES NR 7 & NR 8. REPAIRED FASTNER HOLES ON THE INNER FITTING AT FR 42, RIB 1 LEFT SIDE, HOLES NR 7 & NR 8 IAW ENGINEERING AUTHORIZATION 102915.

Part: FASTENER — LOOSE (CENTER WING) · airframe 50,165 hrs · 7,350 cycles

FRA - TRACES OF FUEL HAVE BEEN FOUND IN THE CENTER WING DRY BAY OF A330-300 AIRCRAFT AT RIB 1. AS A RESULT OF THIS AN INSPECTION WAS PERFORMED ON THIS AIRCRAFT & FASTENERS WERE FOUND LOOSE & LEAKING AT FR42 LEFT & RIGHT SIDES AT RIB 1. ALSO A CRACK INDICATION WAS NOTED ON THE VERTICAL ANGLE AT RIB 1 ON THE LEFT SIDE. THE VERTICAL ANGLE WAS REPAIRED IAW EA 102897 & 102915. THE BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 102863C.

Part: EPSU — FAULTY (CABIN)

CLT - PERFORMED TROUBLESHOOTING OF EPSU 16WL. MAINTENANCE FOUND EPSU 16WL AT FAULT FOR EMERGENCY LIGHTS ON NUMEROUS ROWS. MAINTENANCE REPLACED EPSU 16WL.

Part: WIRE — CUT (CABIN)

CLT - PERFORM TROUBLESHOOTING OF EPSU 16WL. FOUND WIRE CUT AND TAPED AT SEAT 38R. RECONNECTED WIRES.

Part: EPSU — FAILED (CABIN)

PHL - DURING CHECK, FOUND SOME EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED NUMBER THREE R EPSU AND BATTERY.

Part: FUSE — FAILED (POWER SUPPLY)

PHL - FOUND EMERGENCY LIGHTS OUT ON SEATS 9G, 13G, 19G, 23G, 28G, AND 33G. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT THE R3 DOOR. PRELIMINARY INSPECTION - PERFORMED FUNCTIONAL TEST/INSPECTION AND VERIFIED DISCREPANCY. TROUBLESHOOTING REVEALED FUSE F6 ON PCB A3 WAS OPEN. REMOVED AND RE-SOLDERED WEAK CONNECTIONS UNDERNEATH CONVERTER U12, RE-INSTALLED U12. REPLACED LISTED PART(S) (FUSE 4A 250 TR5T19372-4A, MPN 779-435-73). UNIT ASSEMBLED, CLEANED, AND PASSED FUNCTIONAL TEST.

Part: DAMPER — FAILED (EMERGENCY EXIT) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - EES - RIGHT EMERGENCY EXIT DOOR DAMPER & EMERGENCY OPERATION CYLINDER FAILED ON DAMPING CHECK. REPLACED RIGHT EMERGENCY EXIT DOOR 3R DAMPER IAW A330 AMM 52-22-14-40-801.

Part: DAMPER — FAILED (EMERGENCY EXIT) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - EES - LEFT EMERGENCY EXIT DOOR DAMPER & EMERGENCY OPERATION CYLINDER FAILED ON DAMPING CHECK. REPLACED LEFT EMERGENCY EXIT DOOR 3L DAMPER IAW A330 AMM 52-22-14-40-801.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON NR 1 ENGINE FORWARD PYRAMID MOUNT FITTING ATTACH HOLES (4 EACH) & MATING SURFACES. REPAIRED NR 1 ENGINE FORWARD PYRAMID MOUNT FITTING IAW EA 134306.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON NR 2 ENGINE FORWARD PYRAMID MOUNT FITTING ATTACH HOLES (4 EACH) & MATING SURFACES. REPAIRED NR 2 ENGINE FORWARD PYRAMID MOUNT FITTING IAW EA 134308.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM AT FR80, Y450. REPAIRED CABIN FLOOR STRUCTURE CROSSBEAM AT FR80, Y450 IAW EA 34313.

Part: RIB — CRACKED (ZONE 400) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CRACKED RIB FRAME AT FR 7264. REPLACED RIB FRAME AT FR 7264 AW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT OUTBOARD FLANGE AND CROWN FR.19 Y-450. REPAIRED SEAT TRACK AT OUTBOARD FLANGE AND CROWN FR 19 Y-450 IAW A330 SRM 51-74-00 AND A330 SRM 53-00-01 FIG 101 AND A330 SRM 53-00-15 FIG 204.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 26.4,- Y1959. REPLACED SEAT TRACK BETWEEN FR 26.4,- Y1959 IAW A330 SRM 53-00-15 FIG 202, A330 SRM 53-00-15 FIG 101, A330 SRM 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 19,- Y953. REPLACED SEAT TRACK AT FR 19,- Y953 IAW A330 SRM 51-74-00, A330 SRM 53-00-15 FIG 101, A330 SRM 53-30-15 FIG 204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT SEAL PROFILE AT FR80, -Y450. REPLACED FLOOR SUPPORT SEAL PROFILE AT FR80, -Y450 IAW A330 SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - NR 6298288 - DELAMINATION ON FLOOR PANEL NR 272HF BETWEEN FR73 TO FR75. REPLACED FLOOR PANEL NR 272HF BETWEEN FR73 TO FR75 IAW SRM 53-02-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSEL) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOORBEAM BETWEEN FR75 TO FR76, Y450. REPLACED LONGERON FLOORBEAM BETWEEN FR75 TO FR76, Y450 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - NR 6279473 - CORROSION ON FLOOR SUPPORT AT FR30, Y0. REPLACED FLOOR SUPPORT AT FR30, Y0 IAW A330 SRM 51-74-00, 53-31-15, 53-00-14, 51-70-10, 51-21-11, 51-23-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT PROFILE 9 INCHES AFT OF FR80, -Y450. REPLACED FLOOR SUPPORT PROFILE 9 INCHES AFT OF FR80, -Y450 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOORBEAM 9 INCHES AFT OF FR80, Y450. REPLACED LONGERON FLOORBEAM 9 INCHES AFT OF FR80, Y450 IAW A330 SRM 53-41-14, 51-42-11, 51-44-11 & 51-75-12.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOORBEAM 12 INCHES FORWARD OF FR76 TO FR76, Y1447.8. REPLACED LONGERON FLOORBEAM 12 INCHES FORWARD OF FR76 TO FR76, Y1447.8 IAW A330 SRM 53-21-14, 53-41-14, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK AT FR41, -Y450. REPLACED CABIN SEAT TRACK AT FR41, -Y450 IAW A330 SRM 53-31-15, 51-42-11, 53-74-00 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION SEAT TRACK 8 INCHES AFT OF FR73 (TRACK YB &1). REPLACED SEAT TRACK 8 INCHES AFT OF FR73 (TRACK YB &1) IAW A330 SRM 53-00-15, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR33 TO FR37, Y953. REPLACED MAIN CABIN SEAT TRACK BETWEEN FR33 TO FR37, Y953 IAW A330 SRM 51-74-00, 53-00-15, 51-72-11, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - NR 6298121 - CRACKED FLOOR SUPPORT BETWEEN FR7 TO FR10. REPLACED FLOOR SUPPORT BETWEEN FR7 TO FR10 IAW A330 SRM 51-44-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR37, Y450. REPLACED MAIN CABIN SEAT TRACK AT FR37, Y450 IAW A330 SRM 53-00-15, 51-74-00, 51-42-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN FR42 TO FR43, -Y450. REPLACED CABIN SEAT TRACK BETWEEN FR42 TO FR43, -Y450 IAW A330 SRM 51-72-11, 53-31-15 & 51-10-00.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - 2 HEATED FLOOR PANELS CORRODED AT R2 DOOR BETWEEN FR33 TO FR35A & BETWEEN -Y2462 TO -Y1456. REPLACED 2 HEATED FLOOR PANELS AT R2 DOOR BETWEEN FR33 TO FR35A & BETWEEN -Y2462 TO -Y1456 IAW TYPICAL REPAIR 53-02-01.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGERON BEAM BETWEEN FR 73 TO FR 76, Y0. REPLACED LONGERON BEAM BETWEEN FR 73 TO FR 76, Y0 IAW A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN FR70 TO FR72, -Y450. REPLACED CABIN SEAT TRACK BETWEEN FR70 TO FR72, -Y450 IAW A330 SRM 51-74-00, 53-00-15, 51-42-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR 57.2 - FR 57.3,- Y450. REPLACED SEAT TRACK BETWEEN FR 57.2 -FR 57.3,- Y450 IAW A330 SRM 51-42-11, A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN FR38 TO FR39, -Y2462. REPLACED SEAT TRACK BETWEEN FR38 TO FR39, -Y2462 IAW A330 SRM 53-31-15, 51-74-00 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK 10 INCHES AFT OF FR53.4, -Y2462. REPLACED SEAT TRACK 10 INCHES AFT OF FR53.4, -Y2462 IAW A330 SRM 53-31-15, 51-21-11 & 51-75-12.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOOR BEAM AT FR73, Y1456. REPLACED LONGERON FLOORBEAM AT FR73, Y1456 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 4,837 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 60,- Y1959. REPLACED SEAT TRACK BETWEEN FR 60,- Y1959 IAW A330 SRM 51-42-11, A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK AT FR 60,- Y1959. REPLACED SEAT TRACK BETWEEN FR 60,- Y1959 IAW A330 SRM 51-42-11, A330 SRM 53-00-15.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL NR 261VF BETWEEN FR57.1 TO FR58, -Y450. REPLACED FLOOR PANEL NR 261VF BETWEEN FR57.1 TO FR58, -Y450 IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - EXFOLIATION CORROSION ON SEAT TRACK AT FR 35,- Y2462. REPLACED SEAT TRACK AT FR 35,- Y2462 IAW A330 SRM 51-74-00, A330 SRM 53-00-15 FIG 101 D-D, A330 SRM 51-44-11, A330 SRM 53-00-15, A330 SRM 51-42-11, A330 SRM 51-75-12.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGERON BEAM AT FR73, -Y1137.1. REPLACED LONGERON BEAM AT FR73, -Y1137.1 IAW A330 SRM 51-74-00, A330 SRM 53-00-15 FIG 102, A330 SRM 51-72-12, A330 SRM 51-23-12, A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR 33 AND FR 34,- Y1456. REPLACED SEAT TRACK BETWEEN FR 33 AND FR 34,- Y1456 IAW A330 SRM 51-42-11, A330 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK 10 INCHES FORWARD OF FR37.4, Y450. REPLACED SEAT TRACK 10 INCHES FORWARD OF FR37.4, Y450 IAW 53-00-15, 51-42-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN 6 INCHES FORWARD OF FR68 TO FR70, -Y450. REPLACED CABIN SEAT TRACK BETWEEN 6 INCHES FORWARD OF FR68 TO FR70, -Y450 IAW A330 SRM 51-74-00, 53-00-15, 51-42-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR 31 AND FR 33,- Y1959. REPLACED SEAT TRACK BETWEEN FR 31 AND FR 33,- Y1959 IAW A330 SRM 51-42-11, A330 SRM 53-00-15 FIG 101, A330 SRM 51-23-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK AT FR44, -Y450. REPLACED CABIN SEAT TRACK AT FR44, -Y450 IAW A330 SRM 53-31-15, 51-72-11 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN 10 INCHES FORWARD OF FR55 TO FR57.1, -Y450. REPLACED CABIN SEAT TRACK BETWEEN 10 INCHES FORWARD OF FR55 TO FR57.1, -Y450 IAW A330 SRM 53-00-15, 51-42-11 & 51-74-11.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON HEATED FLOOR PANEL AT R1 DOOR AT FR14A, -Y1959. REPLACED HEATED FLOOR PANEL AT R1 DOOR AT FR14A, -Y1959 IAW TYPICAL REPAIR 53-02-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR57.4 TO FR59, Y450. REPLACED SEAT TRACK BETWEEN FR57.4 TO FR59, Y450 IAW A330 SRM 51-42-11 & 51-32-11.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON THE LONGERON BEAM BETWEEN FR 74 TO FR 76, -Y1137.1. REPLACED LONGERON BEAM BETWEEN FR 74 TO FR 76, -Y1137.1 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR34 TO FR35, -Y1456. REPLACED SEAT TRACK BETWEEN FR34 TO FR35, -Y1456 IAW A330 SRM 53-00-15, 51-42-11 & 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - NR 6298258 - DELAMINATION ON FLOOR PANEL NR 251ZF BETWEEN FR40.1 TO FR43 & BETWEEN Y1456 TO Y1959. REPLACED FLOOR PANEL NR 251ZF BETWEEN FR40.1 TO FR43 & BETWEEN Y1456 TO Y1959 IAW SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION MAIN CABIN SEAT TRACK BETWEEN FR72 TO FR75, Y450. REPLACED MAIN CABIN SEAT TRACK BETWEEN FR72 TO FR75, Y450 IAW A330 SRM 53-00-15, 51-42-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSEL) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOORBEAM BETWEEN FR75 TO FR79, -Y1450. REPLACED LONGERON FLOORBEAM BETWEEN FR75 TO FR79, -Y1450 IAW A330 SRM 51-72-11 & 51-75-12.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CRACK ON CABIN FLOOR PROFILE Z-ASSEMBLY STRUCTURE 12 INCHES FORWARD OF FR16 TO FR16 AT R-4 DOOR & 19 INCHES OUTBOARD OF -Y1447.8. REPLACED CABIN FLOOR PROFILE Z-ASSEMBLY IAW A330 SRM 51-42-11, 51-44-11, 51-75-12 & 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM 5 INCHES FORWARD OF FR76, -Y1447. REPLACED FLOORBEAM IAW A330 SRM 51-74-00, 53-41-14, 51-72-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION MAIN CABIN SEAT TRACK CROWN & OUTBD FLANGE FRAME BETWEEN FR18.5 TO FR19.5, Y450. REPLACED MAIN CABIN SEAT TRACK BETWEEN FR18.5 TO FR19.5, Y450 IAW A330 SRM 53-00-15, 51-74-00 & 53-00-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR15A TO FR17, -Y953. REPLACED SEAT TRACK BETWEEN FR15A TO FR17, -Y953 IAW SRM 53-11-15 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSEL) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON FLOORBEAM UPPER CHORD BETWEEN FR73 TO FR75, Y1959. REPLACED LONGERON FLOORBEAM UPPER CHORD BETWEEN FR73 TO FR75, Y1959 IAW SRM 53-00-13, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK 4 INCHES FORWARD OF FR59, -Y1959. REPLACED SEAT TRACK 4 INCHES FORWARD OF FR59, -Y1959 IAW A330 SRM 51-42-11, 51-44-11 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR SUPPORT BETWEEN FR 34 TO 35, Y0. REPLACED CABIN FLOOR SUPPORT BETWEEN FR 34 TO 35, Y0 IAW A330 SRM 51-74-00, A330 SRM 51-42-11, A330 SRM 51-44-11.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - MAIN CABIN FLOOR PANEL 272KF HAS CORROSION BETWEEN FR72 TO FR76, S25R. REPLACED MAIN CABIN HEATED FLOOR PANEL 272KF BETWEEN FR72 TO FR76, S25R IAW A330 SRM 51-21-00 & TYPICAL REPAIR 53-02-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGERON FLOORBEAM BETWEEN FR74 TO FR80, Y794.3. REPLACED LONGERON FLOORBEAM BETWEEN FR74 TO FR80, Y794.3 IAW A330 SRM 53-14-14, 51-42-11, 51-72-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR17 TO FR15A, -Y450. REPLACED SEAT TRACK BETWEEN FR17 TO FR15A, -Y450 IAW A330 SRM 53-11-15, 51-72-11 & 51-74-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK BETWEEN FR45 TO FR46, -Y450. REPLACED CABIN SEAT TRACK BETWEEN FR45 TO FR46, -Y450 IAW A330 SRM 53-31-15, 51-72-11 & 51-42-11.

Part: PIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 - LEVEL 2 CORROSION ON PIN FLANGE AT NR 2 PYLON RIGHT INBOARD OF FORWARD PYLON TO WING ATTACH FITTING, RIB 12. REPLACED PIN FLANGE AT NR 2 PYLON RIGHT INBOARD OF FORWARD PYLON TO WING ATTACH FITTING, RIB 12 IAW A330 AMM 54-51-17.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGERON BEAM AT FR 74 TO 76, Y1447.8. REPLACED LONGERON BEAM AT FR 74 TO 76, Y1447.8 IAW A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION MAIN CABIN SEAT TRACK CROWN AND FLANGE BETWEEN FR33 TO FR34, Y450. REPLACED SEAT TRACK BETWEEN FR33 TO FR34, Y450 IAW A330 SRM 53-00-15 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION MAIN CABIN SEAT TRACK AT 7 AND 8.5 INCHES AFT OF FR36, Y450. REPLACED SEAT TRACK AT FR36, Y450 IAW A330 SRM 53-00-15, 51-42-21 & 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CABIN FLOOR SUPPORT AT FR 14, -Y953. REPAIRED FORWARD CABIN FLOOR SUPPORT AT FR 14, -Y953 IAW A330 SRM 51-21-11, A330 SRM 51-75-12, A330 SRM 53-11-14 FIG 211, A330 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR67 TO FR68, Y450. REPLACED SEAT TRACK BETWEEN FR67 TO FR68, Y450 IAW A330 SRM 53-00-15, 51-74-00 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK 2.5 INCHES FORWARD OF FR62, -Y2463. REPLACED SEAT TRACK 2.5 INCHES FORWARD OF FR62, -Y2463 IAW A330 SRM 51-74-00, 53-00-15, 51-42-11 & 51-72-11.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR CROSS BEAM AUXILLARY STRUCTURE AT, 8 INCHES AFT OF FR 73, 2 INCHES TO 14 INCHES INBOARD OF Y2462. REPAIRED CABIN FLOOR CROSS BEAM AUXILLARY STRUCTURE AT, 8 INCHES AFT OF FR 73, 2 INCHES TO 14 INCHES INBOARD OF Y2462 IAW A330 SRM 51-74-00, A330 SRM 53-00-15 FIG 101, A330 SRM 51-42-11, A330 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION MAIN CABIN SEAT TRACK FORWARD OF FR74, -YC1 OLT 3.5 INCHES. REPLACED MAIN CABIN SEAT TRACK FORWARD OF FR74, -YC1 OLT 3.5 INCHES IAW A330 SRM 53-00-15, 51-42-11, 51-44-11 & 51-72-11.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON LONGERON BEAM BETWEEN FR74 TO FR76, Y1137.1. REPLACED LONGERON BEAM BETWEEN FR74 TO FR76, Y1137.1 IAW A330 SRM 51-74-00, A330 SRM 53-41-14 FIG 103, A330 SRM 51-72-11, A330 SRM 51-44-11, A330 SRM 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION CABIN FLOOR STRUCTURE LONGERON BETWEEN FR73. 5 TO FR74, -Y1447.8. REPLACED LONGERON BETWEEN FR73. 5 TO FR74, -Y1447.8 IAW A330 SRM 51-74-00, 53-41-14, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGERON FLOORBEAM AT FR73, Y1137.1. REPLACED LONGERON FLOORBEAM AT FR73, Y1137.1 IAW SRM 53-41-14, 51-44-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK WEB LOWER SURFACE AT FR73, Y2462. REPLACED SEAT TRACK AT FR73, Y2462 IAW A330 SRM 51-42-11, 51-44-11 & 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN FR17 TO FR15A, Y450. REPLACED SEAT TRACK BETWEEN FR17 TO FR15A, Y450 IAW A330 SRM 51-74-00, 51-44-11 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR65 TO FR67, Y450. REPAIRED SEAT TRACK BETWEEN FR65 TO FR67, Y450 IAW A330 SRM 53-00-15 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LONGERON BEAM BETWEEN FR791 TO FR80, Y1447.8. REPLACED FLOOR SUPPORT BETWEEN FR791 TO FR80, Y1447.8 IAW A330 SRM 51-41-14, 51-74-00 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR STRUCTURE SUPPORT AT FR 73, Y1959. REPAIRED CABIN FLOOR STRUCTURE SUPPORT AT FR 73, Y1959 IAW A330 SRM 53-41-14 FIG 103B-B, A330 SRM 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR30 TO FR38, -Y953. REMOVED SEAT TRACK BETWEEN FR30 TO FR38, -Y953 IAW A330 SRM 53-00-15 & 51-42-11.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT WING LOWER FUEL ACCESS PANEL 642FB FASTENER HOLE LANDS. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 642FB IAW A330 SRM 57-27-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON LONGERON BEAM BETWEEN FR71 TO FR74, Y794.3. REPLACED FLOOR SUPPORT BETWEEN FR71 TO FR74, Y794.3 IAW A330 SRM 51-44-11, 53-41-14, 51-72-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,108 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LONGERON BEAM BETWEEN FR75 TO FR78, Y450. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR78, Y450 IAW SRM 51-44-11, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LONGERON BEAM BETWEEN FR74 TO FR76, -Y1447.8. REPLACED FLOOR SUPPORT BETWEEN FR74 TO FR76, -Y1447.8 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11 & 5175-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR73, Y2462. REPLACED SEAT TRACK AT FR73, Y2462 IAW A330 SRM 53-41-14 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR73 TO FR75, -Y450. REPLACED SEAT TRACK BETWEEN FR73 TO FR75, -Y450 IAW A330 SRM 51-74-00, 53-00-15 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR78 BETWEEN Y450 TO -Y450. REPLACED FLOOR SUPPORT AT FR78 BETWEEN Y450 TO -Y450 IAW A330 SRM 53-41-14 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR SUPPORT AT FR76, Y1447. REPLACED FLOOR SUPPORT AT FR76, Y1447 IAW A330 SRM 51-74-00, 51-42-11 & 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR37 TO FR36, Y450. REPLACED SEAT TRACK BETWEEN FR37 TO FR36, Y450 IAW A330 SRM 51-42-11, 51-44-11 & 51-72-11.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON T-CHANNEL FLOOR STRUCTURE BETWEEN FR71 TO FR74, -Y794.3. REPLACED T-CHANNEL FLOOR STRUCTURE BETWEEN FR71 TO FR74, -Y794.3 IAW A330 SRM 53-41-14 & 51-42-11.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 48,371 hrs · 7,105 cycles

BFM - S2 - MAJOR REPAIR - NR 6279756 - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR78, -Y450. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR78, -Y450 IAW SRM 51-42-11 & 51-44-11.

Part: EPSU — FAILED (EMERGENCY LIGHTS)

EPSU AND BATTERY FAILED TEST. REMOVED AND REPLACED EPSU, FIN 16WL, AND BATTERY. INSTALLED SELF-ADHESIVE STRIPS IAW SIL 3214-33-05/02. REMOVED AND RE-SOLDERED WEAK CONNECTIONS UNDERNEATH CONVERTER U12, RE-INSTALLED U12. UNIT ASSEMBLED, CLEANED, AND PASSED FUNCTIONAL TEST.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAD - FOUND CAPTAIN'S FLASHLIGHT RED LED NOT BLINKING. REMOVED AND REPLACED BATTERY.

Part: BATTERY — FAULTY (CABIN)

PHL - R3 EPSU BATT FAULT ON EPSU TEST. REMOVED AND REPLACED R3 EPSU BATT.

Part: O-RING — DAMAGED (MEGAPHONE)

PHL - FOUND THE FORWARD MEGAPHONE BATTERY COMPARTMENT O-RING DAMAGED. REPLACED MEGAPHONE.

Part: MEGAPHONE — INOPERATIVE (CABIN)

FRA - THE AFT MEGAPHONE WAS FOUND INOPERATIVE. THE AFT MEGAPHONE WAS REPLACED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

LHR - THE CAPTAIN’S FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CAPTAIN’S FLASHLIGHT BATTERY. OPERATIONALLY CHECKS OK. (S)

Part: ADIRU — FAULTY (NR 3)

PHL - FLT 704 - CLT TO FRA - PRIOR TO COAST OUT, RECEIVED 'NAV IR3 FAULT'. FLIGHT COULD NOT CONTINUE ETOPS PER PROCEDURES. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADIRU NUMBER 3. OPERATIONALLY CHECKS OK.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON BODY FAIRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2. REPLACED BODY FAIRING SUPPORT STRUCTURE BRACKET, BS 2948 / FR 39.2 IAW A330 SRM 53-35-14 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5054 /FR 62. REPAIRED CABIN SEAT TRACK BS 4842 / FR 58 - BS 5054 /FR 62 IAW A330 SRM 53-00-15, 51-44-11 AND 51-42-11. *SUPP* AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 3940 / FR 53.1, -Y450. REPAIRED CABIN SEAT TRACK, BS 3940 / FR 53.1, -Y450 IAW A330 SRM 53-31-15 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4789 / FR 57.4 - BS 4842 / FR 58, -Y450. REPAIRED CABIN SEAT TRACK, BS 4789 / FR 57.4 - BS 4842 / FR 58, -Y450 IAW A330 SRM 53-31-15 AND 51-23-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, -Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB 3990 / FR 53.2, -Y2820, WL -Z1650 I/A/W A330 SRM 53-35-14 AND 51-44-11. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5478 / FR 70, +Y450. REPAIRED CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5478 / FR 70, +Y450 IAW A330 SRM 53-31-15, 53-00-15 AND 51-42-00. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: WEB — CRACKED (FUSELAGE) · airframe 35,007 hrs · 5,286 cycles

BFM - MAJOR REPAIR - C2 CHECK - CRACK ON AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650. REPAIRED AFT BELLY FAIRING SUPPORT STRUCTURE WEB, BS 3990 / FR 53.2, +Y2820, WL -Z1650 IAW A330 SRM 53-35-14. AIRCRAFT MANUFACTURER AND MODEL WAS CHANGED FROM BOEING 767201ER TO AIRBUS A330323.

Part: COMPUTER — FAILED (DOOR WARNING) · airframe 34,204 hrs · 5,173 cycles

FLIGHT 1071, PHL-SJU: FLIGHT RETURNED TO PHL DUE TO AN AFT CARGO DOOR OPEN INDICATION. UPDATED 8/3/07: MAINTENANCE REPLACED THE PROXIMITY SENSOR COMPUTER. NO FURTHER FAULTS.

Part: PROXIMITY SENSOR — INOPERATIVE (CARGO DOOR) · airframe 34,204 hrs · 5,173 cycles

FLIGHT 1071: FLIGHT RETURNED TO DEPARTURE DUE TO AN AFT CARGO DOOR OPEN INDICATION. MAINTENANCE REPLACED PROXIMITY SENSOR 28MJ.

Part: EPSU — FAULTY (EMERGENCY LIGHT)

PHL - EPSU 2R (14 WL) FAILS EMERGENCY LIGHT OPERATIONAL CHECK CARD J7-210-2414, BITE TEST OF 14WL FAULTS UNIT, INTERIOR AND EXTERIOR LIGHTS. MAINTENANCE REMOVED AND REPLACED EPSU, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 17 INOPERATIVE AND WITH INCORRECT BULBS INSTALLED. INSTALLED AND RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,696 hrs · 4,542 cycles

FLOOR LEVEL EMERGENCY LIGHTING AT SEAT 17B INOPERATIVE. MAINTENANCE RE-INSTALLED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 17B. NO FURTHER DIFFICULTIES.