N271AY
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
293 reports on file, 2007-05-04 – 2019-12-23.
Part: ADC — FAULTED · airframe 87,132 hrs · 13,180 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS F/O AIR DATA COMPUTER FAILED ON TAKEOFF ROLL CAME BACK SHORTLY AFTER. MAINTENANCE REPORTS PFR REPORTED ADM6 (19FP6) IAW TSM 34-10-00-810-851-A. REPLACED ADM6 IAW AMM 34-11-17. SYS TEST CHECKED GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,097 hrs · 13,175 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM MCDU SHOWS EPSU 3L (15WL) / DEU B (300RH5) IN PASSENGER CABIN. REPLACED EPSU 3L(15WL) IN PASSENGER CABIN IAW AMM 33-51-38-400-801-A AND PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-801-A. TEST IS OK.
Part: ACTUATOR — NO TEST (R3 DOOR) · airframe 13,175 hrs · 87,097 cycles
AIRCRAFT IN BASE MAINTENANCE: DAMPING EFFECT AT EMERGENCY EXIT DOOR 3R DID NOT PASS TEST. REPLACED DOOR DAMPER (ACTUATOR) PER AMM 52-22-14-400-801-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: ACTUATOR — NO TEST (EMERGENCY EXIT) · airframe 13,175 hrs · 87,097 cycles
AIRCRAFT IN BASE MAINTENANCE: DAMPING EFFECT AT EMERGENCY EXIT DOOR 3L DID NOT PASS TEST. REPLACED DOOR DAMPER (ACTUATOR) PER AMM 52-22-14-400-801-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: LOCK — NO TEST (DOOR SLIDE) · airframe 13,175 hrs · 87,097 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS DONT PASS OPERATIONAL TEST CHECK OF ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION (4DH) FWD CHANNEL IN FWD AVIONIC COMPARTMENT. REPLACED HEATED SLIDE FITTING 6DH IAW AMM 30-46-11-400-801-A. PERFORMED OPERATIONAL CHECK OF THE ESCAPE-SLIDE LOCKING MECHANISM ICE-PROTECTION IAW AMM 30-46-00-710-801-A STEP 1 THRU 3C AND 4A(2), TEST IS OK.
Part: THROTTLE — SURGES · airframe 86,809 hrs · 13,123 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS WHEN ENGAGED WITH AP1 THE AUTO THROTTLES SURGED(BETWEEN 1.1 & CLIMB MAINTAINED ALTITUDE FL 350 & AIRSPEED MACH .82 THE ENTIRE TIME. SWITCHED TO AP2 AUTO THROTTLES WORKED FINE. MAINTENANCE PERFORMED AFS BITE CHECK IAW AMM 22-96-00-740-810A TEST OK. NO AIRMAN AND NO POST FLIGHT REPORT. AIRCRAFT OK FOR CONTINUED SERVICE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 86,174 hrs · 13,042 cycles
AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS EMERGENCY LIGHT BATTERIES FAIL TEST WHILE ACCOMPLISHING JOB CARD 33C20033002. REMOVED AND REPLACED ALL 8 BATTERIES WITH FULLY CHARGED UNITS IAW AMM 33-51-00. OPS CHECK NORMAL.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 84,492 hrs · 12,835 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 3A EMERGENCY LIGHT INOPERABLE. MAINTENANCE REINSTALLED WIRING PIN CONNECTOR AT SEAT 3A CONNECTOR 5450VC7 PER AWM 33-51-21.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 84,492 hrs · 12,835 cycles
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 3L REPORTED INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AT DOOR 3L AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 84,265 hrs · 12,806 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS SMOKE LAVATORY SMOKE ECAM WITH MASTER WARNING AND CRC FOR 3 SECONDS. LAV 11 AND LAC 33 SHOWED RED LIGHT FLASH OVER DOOR, OCCUPIED AT THE TIME. NO SMOKE SMELLED OR SEEN .TRASH CAN WAS INSPECTED. NOTHING FOUND. MAINTENANCE ACCOMPLISHED A330 TSM TASK 26-17-00-810-812-A REV 67, NO FAULTS FOUND. CONFIRMED OK FOR SERVICE.
Part: BATTERY — WEAK (FLASHLIGHT) · airframe 83,616 hrs · 12,709 cycles
CAPTAIN`S EMERGENCY FLASHLIGHT BATTERY WAS WEAK. MAINTENANCE REPLACED THE BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: CIRCUIT BREAKER — FAILED (COFFEEMAKER) · airframe 83,415 hrs · 12,673 cycles
ODOR OF SMOKE IN THE COCKPIT, FWD CABIN, AND CENTER GALLEY. DESCRIBED AS BURNING PLASTIC. COMPLETED JC 33L00021001. FOUND THE SOURCE OF THE ODOR TO BE THE MID-GALLEY COFFEE MAKER CIRCUIT BREAKER OVERHEATED AND TRIPPED. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE CIRCUIT BREAKER IAW AMM 20-46-10. REMOVED AND REPLACED THE COFFEEMAKER IAW AMM 25-35-15. OPS CHECKED GOOD.
Earlier reports · 2007–2018 · 281 reports
2018
Part: CONTROL UNIT — NO TEST (ZONE 100) · airframe 83,415 hrs · 12,672 cycles
HEAT CONTROL UNIT 10DH FAILED TO TEST. MAINTENANCE REPLACED THE CONTROL UNIT IAW JC 33-0533-8-0007/001, AND PERFORMED A SATISFACTORY OPS CHECK.
Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 83,415 hrs · 12,672 cycles
FLIGHT ATTENDANT FLASHLIGHT LED DOES NOT FLASH. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-02.
Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 82,108 hrs · 12,503 cycles
DURING INITIAL TAKE OFF, EXPERIENCED TWO VIOLENT COMPRESSOR STALLS ON THE RIGHT ENGINE. REJECTED TAKE OFF AND RETURNED BACK TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED ENGINE IAW 33L40071001.
Part: OVEN — ODOR (GALLEY) · airframe 82,108 hrs · 12,503 cycles
MID-GALLEY OVEN NR 2 HAD ELECTRICAL BURNING ODOR. REPLACED THE NR 2 OVEN IAW AMM 25-35-19-0401. OPS CHECKED SATISFACTORY.
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 80,865 hrs · 12,357 cycles
DURING A A03 CHECK, EMERGENCY LIGHT TEST, ACTIVE CLASS 1 FAULT CIDS 1 335100 EXIT SIGNS/EMERGENCY POWER SUPPLY UNIT 3L 15WL. REPLACED THE POWER SUPPLY IAW AMM 33-51-38, AND PERFORMED SATISFACTORY OPS CHECK. THE AIRCRAFT WAS GROUNDED
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 80,865 hrs · 12,357 cycles
DURING A A03 CHECK, EMERGENCY LIGHT TEST, ACTIVE CLASS 1 FAULT CIDS 1335100 EXIT SIGNS, EMERGENCY POWER SUPPLY UNIT 3R 16WL. REPLACED THE POWER SUPPLY IAW AMM 33-51-38, AND PERFORMED SATISFACTORY OPS CHECK. THE AIRCRAFT WAS GROUNDED
Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 80,590 hrs · 12,323 cycles
R3 EXIT SIGN HANGING DOWN. REPLACED THE EXIT SIGN HOUSING IAW 33-51-17.
Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 80,513 hrs · 12,313 cycles
EXIT SIGN ON THE L3 DOOR WAS FOUND BROKEN. REPLACED THE SIGN IAW AMM 33-51-00-710-804-A.
Part: LIGHT — DETACHED (CABIN) · airframe 80,216 hrs · 12,273 cycles
EMERGENCY EXIT LIGHT AT L3 JUMP SEAT. HANGING BY WIRES ONLY. REPLACED THE EMERGENCY EXIT SIGN IAW AMM 33-51-17. OPS CHECKED GOOD.
Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 79,918 hrs · 12,231 cycles
L4 DOOR ARMING KNOB WILL NOT MOVE FULLY TO THE ARMED POSITION. REMOVED DEBRIS FROM GIRT BAR SLIDER.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 79,871 hrs · 12,224 cycles
AIRCRAFT WAS NOT GROUNDED. R1 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED R1 DOOR FLIGHT ATTENDANT FLASHLIGHT.
Part: PIN — CORRODED (ACTUATOR) · airframe 79,769 hrs · 12,209 cycles
CORRODED ACTUATOR LOWER ARM FITTING PIN. REPLACED THE PIN IAW AMM 27-44-51-400-801-A.
Part: STRINGER — CRACKED (FRAME 53) · airframe 79,769 hrs · 12,209 cycles
CRACK INDICATION FOUND ON STRINGER 14R AND 1.125 INCHES AFT OF FRAME 53, AT TORSION BOX RUN-OUT R3 DOOR. REPLACED THE STRINGER SRM 51-72-11, AND DRAWING F53370147.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,769 hrs · 12,209 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED STRINGER 15 RIGHT HAND, AT FR 53.5. REPLACED PER SRM 51-72-11 AND DRAWING F53370020.
Part: ARMING LEVER — DIRTY (R3 DOOR) · airframe 79,635 hrs · 12,186 cycles
R3 DOOR SLIDE WILL NOT DISARM. CLEANED AND LUBRICATED THE R3 SLIDE ARMING LEVER.
2017
Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 79,057 hrs · 12,104 cycles
EXIT SIGN AT THE L3 DOOR FELL OFF. ATTACHED THE SIGN
Part: FILTER — CONTAMINATED (HYD SYSTEM) · airframe 77,659 hrs · 11,927 cycles
DURING INITIAL BRAKE APPLICATION BRAKES APPLY, RELEASE, THEN GRAB. SUSPECT GREEN HYDRAULICS SYSTEM CONTAMINATION. REPLACED GREEN AUX PUMP LP FILTER.
Part: INDICATOR — CONTAMINATED (HYD SYSTEM) · airframe 77,659 hrs · 11,927 cycles
DURING INITIAL BRAKE APPLICATION BRAKES APPLY, RELEASE, THEN GRAB. SUSPECT GREEN HYDRAULICS SYSTEM CONTAMINATION. REPLACED LP DIFFERENTIAL PRESSURE INDICATOR. AIRCRAFT WAS GROUNDED.
Part: DOOR FRAME — DIRTY (R2 DOORWAY) · airframe 77,636 hrs · 11,923 cycles
R2 DOOR WOULD NOT ARM. REMOVED DEBRIS FROM DOOR FRAME.
Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 77,498 hrs · 11,907 cycles
R2 DOOR ARMING HANDLE WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR.
Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 77,176 hrs · 11,867 cycles
EXIT SIGN COVER AT THE R3 DOOR DETACHED. REIINSTALLED EXIT SIGN COVER.
Part: ACTUATOR — FAILED (FUEL TRANSFER) · airframe 77,040 hrs · 11,851 cycles
ECAM FUEL TANK TRANSFER FAULT, ZFW / ZFCG DISAGREE.. AIRCRAFT WAS GROUNDED. REPLACED FUEL TRIM PIPE ISOLATION VALVE ACTUATOR IAW AMM 28-27-53. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 76,948 hrs · 11,839 cycles
EMERGENCY LIGHT ROW 40 SEAT B INOPERATIVE. REPLACED THE LAMP. FOUND POS AND GROUND TERMINALS CROSSED. REINSTALLED.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 76,226 hrs · 11,747 cycles
EPSU BATTERY 11WL AT POSITION 1L FAILED EPSU TEST IAW J/C 33C22033002. REPLACED THE BATTERY. AIRCRAFT WAS GROUNDED.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 76,226 hrs · 11,747 cycles
EPSU BATTERY 17WL AT POSITION L4 FAILED EPSU TEST IAW J/C 33C22033002. REPLACED THE BATTERY 17WL. AIRCRAFT WAS GROUNDED.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 76,226 hrs · 11,747 cycles
EPSU BATTERY 16WL AT POSITION R3 FAILED EPSU TEST IAW J/C 33C22033002. REPLACED THE BATTERY. AIRCRAFT WAS GROUNDED.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 76,226 hrs · 11,747 cycles
EPSU BATTERY 12WL FAILED EPSU TEST IAW J/C 33C22033002. REPLACED EPSU BATTERY 12WL. AIRCRAFT WAS GROUNDED.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 76,141 hrs · 11,735 cycles
EMERGENCY EXIT SIGN FELL OFF THE L3 DOOR. ATTACHED THE EMERGENCY SIGN COVER.
Part: MECHANISM — OUT OF ADJUST (R2 DOOR) · airframe 75,985 hrs · 11,712 cycles
AIRCRAFT WAS NOT GROUNDED. R DOOR WILL NOT STAY ARMED. ADJUSTED DOOR R2 ARMING MECHANISM.
Part: ACTUATOR — FAILED (R2 DOOR) · airframe 75,952 hrs · 11,707 cycles
R2 DOOR ASSIST ACTUATOR FIRING MECHANISM MALFUNCTIONED. REMOVED AND REPLACED R2 DOOR ASSIST ACTUATOR.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,756 hrs · 11,664 cycles
FLIGHT ATTENDANT JUMPSEAT 3L EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 75,496 hrs · 11,616 cycles
FLIGHT ATTENDANT PANEL 1R DOOR READS LOW PRESSURE. MAINTENANCE SERVICED R1 DOOR DAMPER ASSIST IAW AMM 52-10-00.
Part: ELEC CONNECTOR — UNSECURE (PROXIMITY SENSOR) · airframe 75,404 hrs · 11,596 cycles
FLIGHT CREW REPORTED ISSUE AT 3000 FEET WHEN NOSE GEAR FAILED TO EXTEND. ATTEMPLTED TO EXTEND GEAR TWICE WITH SAME RESULTS. ACCOMPLISHED MANUAL LANDING GEAR EXTENSION ON APPROACH, AN EMERGENCY WAS DECLARED. LANDING GEAR NOT LOCKED, NOSE WHEEL RED INDICATION. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND DOWNLOCK PROXIMITY SENSOR 20GA2 ELECTRICAL CONNNECTOR LOOSE AND NOT LOCKED. SECURED THE CONNECTOR IAW MM 32-31-00 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 75,372 hrs · 11,592 cycles
BROKEN TABS ON WHITE EXIT SIGN AT L3 DOOR TOP OF LENS. MAINTENANCE REPLACED THE SIGN AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
2016
Part: CONTACT — DAMAGED (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
L4 DOOR EXIT SIGN HOUSING HAS MISSING CONTACT INSULATION. REPLACED EXIT SIGN HOUSING IAW AMM 33-51-16.
Part: CONTACT — DAMAGED (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
R4 DOOR EXIT SIGN HOUSING MISSING CONTACT INSULATION. REPLACED EXIT SIGN IAW 35-51-16 AND AMM 34-51-16.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
EXIT SIGN INSTALLED IN THE RIGHT AFT CEILING, BEFORE GALLEY NR 5 AND ABOVE R4 DOOR INOPERABLE. REPLACED THE POWER SUPPLY UNIT IAW 33-51-38.
Part: CONNECTOR — LOOSE (CABIN) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. BROKEN CONNECTOR ON EMERGENCY LIGHT AISLE PATH AT SEAT 5A. FOUND CONNECTION TO BE LOOSE, RESEATED CONNECTOR/CONTACT PER ESPM 20-48-00 AND ACCOMPLISHED CHECK PER AMM 33-51-00.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACK ON FORWARD CABIN LEFT HAND SIDE STIFFENER AT FR12A. REPLACED STIFFENER PER EO 5315U155.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. DOOR 2L EMERGENCY EXIT SIGNS, DOOR AND OVERHEAD PATHWAY SIGN, INOPERABLE DURING OPERATIONS CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND AMM 33-51-00.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACK ON FORWARD CABIN RIGHT HAND SIDE STIFFENER AT FR12A. REPLACED STIFFENER PER EO 5315U155 .
Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 75,233 hrs · 11,563 cycles
CRACK ON FORWARD CARGO DOOR INNER SKIN. REPAIRED THE SKIN IAW EA 265196.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
DAMAGED MID CABIN EMERGENCY LIGHT CABLE 706WL. REPLACED CONNECTOR BACKSHELL.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 75,233 hrs · 11,563 cycles
FORWARD ECONOMY CLASS EMERGENCY LIGHT HAS A BROKEN WIRE HARNESS AT FIN 701WL19, CLOSE TO SEAT 13AB. REPLACED THE WIRE HARNESS IAW DRAWING F92393044, CONNECTED TO SEAT AND TESTED.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 75,233 hrs · 11,563 cycles
FORWARD ECONOMY CLASS EMERGENCY LIGHT HAS BROKEN WIRE HARNESS AT FIN 701WL13, CLOSE TO SEAT 8AB. REPLACED THE WIRE HARNESS IA. PER JOB CARD 33C20025106.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
FORWARD ECONOMY CLASS EMERGENCY LIGHT HAS BROKEN HARNESS AT FIN 701WL14, CLOSE TO SEAT 8GH. REPLACED WIRE HARNESS IAW DRAWING F92393044 AND CONNECTED TO SEAT AND TESTED.
Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
BROKEN EMERGENCY LIGHT HARNESS AT SEATS 32AB, 35GH. REPLACED THE WIRE HARNESS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 75,233 hrs · 11,563 cycles
BROKEN EMERGENCY LIGHT WIRE HARNESS AT SEAT 40GH. REPLACED LIGHT WIRE HARNESS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON BEAM AT -Y1447.8 AND FR 78. REPLACED LONGERON BEAM PER SRM 51-74-00, SRM 53-41-14-103 AND SRM 51-23-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT Y1447.8 AND FR 78. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT Y0 AND FR 71. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT Y450 AND FR 80. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT Y1137.1 AND FR 78. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LONGERON FLOORBEAM AT -Y450 AND FR 78. REPLACED BEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN CROSSBEAM, 9" AFT OF FR75 BETWEEN Y1137.1 AND 1447.8. REPLACED CROSSBEAM PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN CROSSBEAM BETWEEN Y450 AND Y794.3 AT FR 75A. REPLACED CROSSBEAM PER A330 SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT AT -Y794.3 AND FR 78. REPLACED FLOOR SUPPORT PER SRM 53-41-14, SRM 51-42-11 AND SRM 51-44-11.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR PROFILE Z ANGLE AT FR80 AND -Y450. REPLACED FLOOR PROFILE Z ANGLE PER SRM 51-42-11.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN UPPER CHORD AT Y2462 BETWEEN FR 71 AND FR 73A. REPLACED UPPER CHORD PER SRM 51-42-11, SRM 53-00-15, AND SRM 51-44-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOORBEAM AT -Y450 AND FR 80. REPLACED FLOORBEAM PER SRM 51-42-11, SRM 51-73-11 AND SRM 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y450 AND FR 17. REPLACED SEAT TRACK PER SRM 53-11-15 AND SRM 51-42-11.
Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORRODED SHIM AT STRINGER L=1.90", W=0.70", D=0.50". REPLACED IAW SRM-51-44-11 AND 51-42-11
Part: PROFILE — CORRODED (FUSELAGE) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON PROFILE Z ASSEMBLY, FLOOR ANGLE AT NUT PLATE HOLES AT, -Y2462 AND FR 75A. REPLACED PROFILE Z ASSEMBLY PER SRM 53-41-14-10 AND SRM 51-42-11.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN CROSS BEAM AT -Y1447.8 AND FR 76. REPLACED CROSS BEAM PER SRM 53-41-14-101 AND SRM 51-42-11.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN CROSS BEAM AT -Y1447.8 AND FR 73A. REPLACED CROSS BEAM PER SRM 53-41-14-101 AND SRM 51-42-11.
Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORRODED PROFILE Z, L=1.70",W=0.80",D=0.080". REPLACED WITH IDENTICAL PART IAW SRM 51-42-11 AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN FLOOR SUPPORT AT -Y953 AND FR 15. REPLACED FLOOR SUPPORT PER SRM 53-11-15 AND SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORRODED FLOORBEAM, L=2.10",W=1.80",D=O.080". REPLACED WITH IDENTICAL PART IAW SRM 51-42-11 AND 51-44-11.
Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORRODED PROFILE Z, L=1.10",W=0.90",D=0.08",REPLACED WITH IDENTICAL PART IAW SRM 51-44-11 AND 51-42-11.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORRODED BEAM ASSEMBLY, L=4.0" W= 2" D= 0.055". REPLACED WITH IDENTICAL PART IAW SRM 51-44-11 AND 51-42-11.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. LONGERON BEAM CORRODED L=1.5",W=0.8", D=1.5" . REPLACED WITH IDENTICAL PART IAW SRM 51-42-11 AND 51-44-11.
Part: COVER — CORRODED (FRAME 16) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
COVER PLATE HAS AREA OF CORROSION. FABRICATED AND INSTALLED NEW COVER PLATE. SRM 53-11-14, SRM 51-42-11, SRM 51-44-11
Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
CORROSION ON SEAT TRACK AT FRAME 74 AND Y450. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11 AND 51-44-11.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 75,233 hrs · 11,563 cycles
BROKEN EMERGENCY LIGHT, SEAT HARNESS. REPLACED WIRE HARNESS ASSEMBLY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: FLOORBEAM — CORRODED (FRAME 78) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOORBEAM CORRODED. REMOVED CORRODED AREA AND INSTALLED A REPAIR ANGLE IAW SRM 53-00-14-201 FIG 202.
Part: WIRE HARNESS — DAMAGED (ZONE 200 - FUSE) · airframe 75,233 hrs · 11,563 cycles
BROKEN EMERGENCY LIGHT, SEAT WIRE HARNESS. REPLACED THE WIRE HARNESS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 75,233 hrs · 11,563 cycles
BROKEN EMERGENCY LIGHT SEAT WIRE HARNESS AT 36 AB. REPLACED THE WIRE HARNESS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: FLOORBEAM — CORRODED (FRAME 78) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOORBEAM CORRODED. REMOVED THE CORRODED AREA, FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM 53-00-14-201 FIG 202.
Part: FLOORBEAM — CORRODED (FRAME 76) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOORBEAM CORRODED. REPLACED THE FLOORBEAM IAW SRM 53-41-14, SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11, AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 73) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11, AND SRM 51-44-11.
Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11, AND SRM 51-44-11.
Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SEAT TRACK HAS A CORRODED AREA. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11, AND SRM 51-44-11.
Part: SHIM — CORRODED (FRAME 74) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SHIM CORRODED. THE SHIM WAS REPLACED IAW SRM.
Part: SEAT TRACK — CORRODED (FRAME 37) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-00-15, SRM 41-42-11, AND SRM 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 78) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOOR SUPPORT HAS CORROSION. REPLACED THE FLOOR SUPPORT
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LONGERON BEAM AT FR 76 AND +Y1447. REPLACED LONGERON BEAM PER SRM 53-41-14, SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 73) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, SRM 51-42-11,AND SRM 51-44-11.
Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
SEAT TRACK CORRODED. REPLACED THE SEAT TRACK SECTION IAW SRM 53-00-15, SRM 51-42-11, AND SRM 51-55-11.
Part: SEAT TRACK — CORRODED (FRAMES 30-33) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
CORROSION ON SEAT TRACK AT -Y953 BETWEEN FRAMES 30 AND 33. REPLACED THE SEAT TRACK IAW SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE, CORROSION ON FLOOR SUPPORT AT FR 43 AND -Y2462. REPLACED FLOOR SUPPORT PER SRM 53-00-15,SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAMES 30-33) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
CORROSION ON THE SEAT TRACK AT -Y953 BETWEEN FRAMES 30 AND 33. REPLACED THE SEAT TRACK IAW SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAMES 31-37) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
CORROSION ON MIDDLE CABIN SEAT TRACK AT -Y953 BETWEEN FRAMES 31 AND 37. REPLACED THE SEAT TRACK IAW SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAMES 33-37) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
CORROSION ON MIDDLE CABIN SEAT TRACK AT Y1552 BETWEEN FRAMES 33 AND 37. REPLACED THE SEAT TRACK IAW SRM 51-42-11.
Part: CONTACT — LOOSE (EXIT SIGN) · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. LOOSE CONTACT WIRES FOR EXIT SIGN 26WL AT DR 4R. REPLACED CONTACTS ON EXIT SIGN PER ESPM 20-48-20 AND INSTALLED EXIT LIGHT AND TESTED PER CARDS 33C27025028 AND 33C22033001.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,233 hrs · 11,563 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y450 BETWEEN FR 17 AND FR 18. REPLACED SEAT TRACK PER SRM 51-42-11.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 74,601 hrs · 11,485 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD F/A FLASHLIGHT 1A NOT CHARGED. R & R FORWARD F/A FLASHLIGHT 1A, FLASHLIGHT IAW AMM 25-65-00.
Part: SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 74,360 hrs · 11,455 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT FUEL PUMP 2 LOW PRESSURE. REPLACED LT FUEL PUMP L2 PUSH BUTTON SWITCH, 64QA1 IAW SPM 20-45-10 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.
Part: GIRT BAR — OBSTRUCTED (ZONE 800) · airframe 73,369 hrs · 11,334 cycles
AIRCRAFT WAS NOT GROUNDED. ACFT 2R DOOR EMERGENCY SLIDE ON DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR ATTACH BRACKETS MOUNTED ON THE FLOOR AND ACCOMPLISHED A SATISFACTORY OPS CHECK.
Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 73,162 hrs · 11,305 cycles
AIRCRAFT WAS NOT GNDED. 2L DOOR HARD TO ARM & DISARM. FOUND THE 2L DOOR GIRT BAR BEING OBSTRUCTED, PAPER, REMOVED THE OBSTRUCTION & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-35-00.
Part: BATTERY — FAILED (CABIN) · airframe 72,667 hrs · 11,245 cycles
AIRCRAFT WAS GNDED. DURING A-16 CHECK, 3R EMER POWER SUPPLY UNIT FAILED BATTERY CAPACITY TEST. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.
Part: BATTERY — FAILED (CABIN) · airframe 72,667 hrs · 11,245 cycles
AIRCRAFT WAS GNDED. DURING A-16 CHECK, 4L EMER POWER SUPPLY UNIT FAILED BATTERY CAPACITY TEST. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.
Part: BATTERY — FAILED (CABIN) · airframe 72,667 hrs · 11,245 cycles
AIRCRAFT WAS GNDED. DURING A-16 CHECK, 4R EMER POWER SUPPLY UNIT FAILED BATTERY CAPACITY TEST. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.
Part: PUMP — LOW PRESSURE (FUEL SYSTEM) · airframe 72,285 hrs · 11,192 cycles
FUEL TRIM TANK PUMP HAD LOW PRESSURE. REPLACED TRIM TANK TRANSFER PUMP & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK.
Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 71,940 hrs · 11,124 cycles
AIRCRAFT WAS GNDED. MID GALLEY HAS A DELAMINATED FLOORBOARD 242HF. REPLACED FLOORBOARD IAW AMM 25-28-42.
Part: COVER — BROKEN (EXIT SIGN) · airframe 71,690 hrs · 11,070 cycles
AIRCRAFT WAS NOT GNDED. EXIT SIGN COVER AT 2R BROKEN OFF. REPLACED EMER EXIT SIGN COVER IAW AMM 33-51-17.
2015
Part: WIRE HARNESS — BROKEN (CABIN) · airframe 71,227 hrs · 10,981 cycles
AIRCRAFT IN BASE MAINTENANCE. EMER LIGHT HARNESS IN SEAT A2 HAS BROKEN TERMINAL. R & R EMER LIGHT HARNESS IAW CMM 25-02-38. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-801.
Part: BEAM — CORRODED (FUSELAGE) · airframe 71,227 hrs · 10,981 cycles
AIRCRAFT IN BASE MX. CORROSION ON LONGERON BEAM, BETWEEN FRAME 75 & 78 AT -Y380. REPLACED LONGERON BEAM IAW SRM 51-42-11.
Part: BEAM — CORRODED (FUSELAGE) · airframe 71,227 hrs · 10,981 cycles
AIRCRAFT IN BASE MX. CORROSION ON LONGERON BEAM, BETWEEN FRAME 75 & 78 AT +Y380. REPLACED LONGERON BEAM IAW SRM 51-42-11.
Part: SIGN — BROKEN (CABIN) · airframe 70,475 hrs · 10,873 cycles
DOOR 2L EMER EXIT SIGN BROKEN AT ATTACHMENT POINT. REPLACED LENS ASSEMBLY IAW AMM 33-51-17. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 69,023 hrs · 10,679 cycles
R3 DOOR SHOWS OPEN AMBER ECAM INDICATION WHEN CLOSED. CIDS SHOWS R3 LOW BOTTLE PRESS. SERVICED THE R3 DOOR ASSIST BOTTLE.
Part: COVER — UNSECURE (CABIN) · airframe 68,785 hrs · 10,648 cycles
EXIT LIGHT COVER HAS COME OFF DOOR 4R. RE-INSTALLED EXIT LIGHT COVER AT DOOR 4R.
Part: LENS — MISSING (CABIN) · airframe 68,544 hrs · 10,608 cycles
L74 EMER LIGHT MISSING. REPLACED THE L74 EMER LIGHT LENS.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,236 hrs · 10,566 cycles
EMERGENCY POWER SUPPLY UNIT 15WL BATTERY FAIL INDICATION. REPLACED EPSU 15WL BATTERY IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,235 hrs · 10,565 cycles
EMERGENCY POWER SUPPLY UNIT 17WL BATTERY FAIL INDICATION. REPLACED EPSU 17WL BATTERY IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,236 hrs · 10,566 cycles
RON CHECK, EPSU 12WL BATTERY FAIL INDICATION. REPLACED EPSU BATTERY 12WL IAW AMM 33-51-38-000-801A. OPERATIONAL CHECKED GOOD.
Part: DIAPHRAGM — FAULTY (L2 DOOR) · airframe 68,079 hrs · 10,545 cycles
DOOR 2L DOOR ASSIST PRESS READS ZERO. REPLACED PERCUSSION MECHANISM DIAPHRAGM IAW AMM 52-10-00.
Part: FITTING — FAULTY (ZONE 200) · airframe 68,079 hrs · 10,545 cycles
HEATED SLIDE FITTING AT DOOR R3 FAILED TEST. REPLACED R3 DOOR HEATED SLIDE FITTING IAW AMM 30-46-11.
Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 67,493 hrs · 10,398 cycles
FAP INDICATES CHECK SLIDE PRESS 1L DOOR. REPLACED THE L1 DOOR ESCAPE SLIDE.
Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 67,473 hrs · 10,390 cycles
LOW PRESS WARNING ON CIDS PANEL FOR 3R DOOR. SERVICED 3R DOOR ASSIST BOTTLE, MSG CLEARED. LEAK CHECKED OK.
Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 67,465 hrs · 10,387 cycles
3R DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED 3R DOOR ASSIST BOTTLE.
2014
Part: CONNECTOR — LOOSE (CABIN) · airframe 65,701 hrs · 10,110 cycles
SEAT MOUNTED EMER EXIT LIGHT SEAT 16GH INOPERATIVE. MAINTENANCE RESECURED LOOSE CANON PLUG.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 64,798 hrs · 9,990 cycles
FORWARD EMER FLASHLIGHT AT L1 DOOR INOPERATIVE. MX REPLACED FLASHLIGHT BATTERY AT L1 DOOR FWD JUMP SEAT, SECURED AS REQUIRED OPERATES OK.
Part: DUCT CLAMP — LOOSE (AC BAY) · airframe 64,766 hrs · 9,986 cycles
SHORTLY AFTER TAKEOFF & PASSING THROUGH 10,000' AGL, THE CREW EXPERIENCED A LOW FREQUENCY BUFFETING THAT INCREASED WITH ACFT SPEED. THE VIBRATION WENT AWAY WHEN THE POWER WAS REDUCED. THERE WERE NO INDICATION ISSUES. AFTER DECIDING TO RETURN TO ATH FOR MX, THE CREW EXPERIENCED A SIMILAR BUFFETING SOUND WHILE IN A HOLD & IN LANDING CONFIGURATION. THE ISSUE OCCURRED AT BOTH LOW & HIGH SPEEDS. THE FLIGHT LANDED WITHOUT INCIDENT WITH EMER EQUIPMENT STANDING BY. MX FOUND ON THE RT AIR CONDITIONING BAY CLAMP LOOSE ON RT & PACK HEAT EXCHANGER OUTLET DUCT PORT. DUCT CONNECTED & PROPERLY SECURED.
Part: VIDEO DISPLAY — SMOKE (CABIN)
VIDEO SCREEN SEAT 9C STARTED SMOKING, FLIGHT ATTENDANT TURNED IT OFF. NOT HOT BUT SMOKE SMELL. ACCOMPLISHED OPERATIONAL CHECK OF VIDEO 9C, NO SMOKE NOR ANY SMELL NOTED, OK FOR SERVICE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,496 hrs · 9,806 cycles
3R DOOR FLASHLIGHT IS NOT FLASHING. MX INSTALLED NEW BATTERY IN FLASHLIGHT AT 3R, CHECKED GOOD.
Part: MONITOR — SMOKE (CABIN) · airframe 63,274 hrs · 9,767 cycles
10C VIDEO MONITOR SMOKES WHEN ON. MX REPLACED VIDEO MONITOR 10C & SEB ROW 10 C, D, E, F.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK CORROSION ON SEAT TRACK BETWEEN FRAME 62 TO FRAME 68, Y 1959. REPLACED SEAT TRACK BETWEEN FRAME 62 TO FRAME 68, Y 1959 IAW A330 SRM 53-00-15, FIG 204 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 151PF BETWEEN FRAME 58 TO FRAME 60 BETWEEN Y 805 TO Y 1470. REPLACED FLOOR PANEL 151PF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 152QF BETWEEN FRAME 58 TO FRAME 60 & BETWEEN Y 805 TO Y 1470. REPLACED FLOOR PANEL 152QF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262FH BETWEEN FRAME 62 TO FRAME 65 BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 262FH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262DH BETWEEN FRAME 58 TO FRAME 60 BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 262DH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK CORROSION ON SEAT TRACK BETWEEN FRAME 37 TO FRAME 37.2, Y 450. REPLACED SEAT TRACK BETWEEN FRAME 37 TO FRAME 37.2, Y 450 IAW A330 SRM 53-00-15, FIG 101 & 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK CORROSION ON SEAT TRACK BETWEEN FRAME 58 TO FRAME 62 & Y 1959. REPLACED SEAT TRACK BETWEEN FRAME 58 TO FRAME 62 & Y 1959 IAW A330 SRM 53-00-15, FIG 101 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262MG BETWEEN FRAME 62 TO FRAME 65, BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 262MG IAW A330 SRM 53-02-00, PARA 5I, FIG 211.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251AF BETWEEN FRAME 37 TO FRAME 37.4, BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 251AF IAW A320 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261NH BETWEEN FRAME 67 TO FRAME 69, BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261NH IAW A320 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251GF BETWEEN FRAME 37.4 TO FRAME 39, BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251GF IAW A320 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261WG BETWEEN FRAME 69 TO FRAME 71, BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261WG IAW A320 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 252JF BETWEEN FRAME 37.2 TO FRAME 39 & BETWEEN Y 1450 TO Y 1959. REPLACED FLOOR PANEL 252JF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251HG BETWEEN FRAME 47 TO FRAME 51 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251HG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261FG BETWEEN FRAME 60 TO FRAME 62 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261FG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251SG BETWEEN FRAME 51 TO FRAME 53.2 & BETWEEN Y 1959 TO Y 2462. REPLACED FLOOR PANEL 251SG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251MF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251MF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261VF BETWEEN FRAME 57.1 TO FRAME 58 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261VF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262JF BETWEEN FRAME 53.7 TO FRAME 53.9 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 262JF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261DH BETWEEN FRAME 58 TO FRAME 60 & BETWEEN Y 953 TO Y 1959. REPLACED FLOOR PANEL 261DH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251DF BETWEEN FRAME 27 TO FRAME 37.4 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 251DF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 261AG BETWEEN FRAME 58 TO FRAME 60 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 261AG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262LF BETWEEN FRAME 53.9 TO FRAME 55 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 262LF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
DELAMINATION ON FLOOR PANEL 251WF BETWEEN FRAME 40 TO FRAME 45 & BETWEEN Y 450 TO -Y 450. REPLACED FLOOR PANEL 251WF IAW SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251XF BETWEEN FRAME 40 TO FRAME 42 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251XF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 252RG BETWEEN FRAME 51 TO FRAME 53.2 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 252RG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 252MF BETWEEN FRAME 39 TO FRAME 39.2 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 252MF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251CG BETWEEN FRAME 44 TO FRAME 47 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 251CG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251NG BETWEEN FRAME 53 TO FRAME 53.2 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 251NG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251RG BETWEEN FRAME 51 TO FRAME 53.2 & BETWEEN Y 1456 TO Y 1959. REPLACED FLOOR PANEL 251RG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 251GG BETWEEN FRAME 47 TO FRAME 51 & BETWEEN Y 450 TO Y 450. REPLACED FLOOR PANEL 251GG IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 231EF BETWEEN FRAME 19 TO FRAME 22 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 231EF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 232ZF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 2462 TO Y 1959. REPLACED FLOOR PANEL 232ZF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 231LF BETWEEN FRAME 22 TO FRAME 25 & BETWEEN Y 450 TO Y 953. REPLACED FLOOR PANEL 231LF IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,234 hrs · 9,755 cycles
C2 CHECK DELAMINATION ON FLOOR PANEL 262JH BETWEEN FRAME 53.7 TO FRAME 53.9 & BETWEEN Y 1552.5 TO Y 1959. REPLACED FLOOR PANEL 262JH IAW A330 SRM 53-02-00, FIG 211 & 51-42-11.
2013
Part: MONITOR — FAILED (SEAT 13C) · airframe 62,698 hrs · 9,675 cycles
SEAT 13C MONITOR HOT WITH SMOKE EMITTING FROM FACE OF UNIT. MAINTENANCE R & R VIDEO MONITOR AT SEAT 13C.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 62,101 hrs · 9,599 cycles
DURING EMERGENCY LIGHTING BATTERY CAPACITY CHECK AT 1L (11WL) AND BATTERY 2L (13WL) FAILED. MX R & R BATTERIES AT 1L & 2L DOORS.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 60,635 hrs · 9,409 cycles
FLASHLIGHT AT 3R INOPERATIVE. MX REPLACED FLASHLIGHT BATTERY AT 3R, CHECKS OK.
Part: FITTING — INOPERATIVE (SLIDE HEATER) · airframe 59,955 hrs · 9,322 cycles
SLIDE FITTING HEATER CONTROL UNIT FAILED TEST ON SLIDE HEATER FITTING 14DH. REMOVED AND REPLACED SLIDE HEATER FITTING 14DH IAW A330 AMM 30-46-11AND PERFORMED OPS CHECK, TEST GOOD IAW A330 AMM 30-46-00.
Part: SIGN — UNSECURE (CABIN) · airframe 59,770 hrs · 9,297 cycles
EXIT SIGN OVER DOOR 3R FELL OFF. MAINTENANCE REPLACED EXIT SIGN LENS AT 3R DOOR.
Part: ACTUATOR — MALFUNCTIONED (O2 MASK DEPLOY) · airframe 59,710 hrs · 9,288 cycles
FLT 755, ENROUTE. DURING CABIN DEPRESSURIZATION EVENT, O2 MASKS DID NOT DEPLOY AT F/A SEATS BY DOORS 1R, 4L, AND 4R, AND AT PASSENGER SEAT POSITIONS 13E/F, 13G/H, 26G/H, 29G/H, 32E/F, 32G/F, AND 33E/F. MAINTENANCE REPLACED THE SOLENOID ACTUATORS FOR SEATS AT THE AFFECTED POSITIONS. MAINTENANCE ALSO REPLACED ALL SPENT OXYGEN GENERATORS IN THE CABIN.
Part: CHECK VALVE — FAILED (RAM AIR INTAKE) · airframe 59,710 hrs · 9,288 cycles
FLT 755, EN ROUTE. AT FL380, AIRCRAFT EXPERIENCED SUDDEN CABIN DEPRESSURIZATION. RECEIVED ECAM MESSAGES "CABIN ALTITUDE", "CAB PR LO DIPR PR", AND "MAINTENANCE STATUS BMC2". INITIATED AN EMERGENCY DESCENT AND DONNED O2 MASKS. DURING EMERGENCY DESCENT, RATE OF DEPRESSURIZATION INCREASED TO NEARLY 2000 FPM. OTHER THAN A MUFFLED THUD AND EARS POPPING, THERE WAS NO OBVIOUS CAUSE INDICATED. FLIGHT LEVELED OFF TO 10,000 FT AND CONTINUED TO DESTINATION, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE EMERGENCY RAM AIR INLET CHECK VALVE AND FOUND THE VALVE MISSING ONE OF THE FLAPPER HALVES. MAINTENANCE REPLACED THE EMERGENCY RAM AIR INLET CHECK VALVE. MAINTENANCE ALSO REPLACED ALL SPENT EMERGENCY OXYGEN GENERATORS IN THE AIRCRAFT CABIN.
Part: LIGHT — DEFECTIVE (CABIN) · airframe 59,588 hrs · 9,267 cycles
THE 27H READING LIGHT WAS HOT AND APPEARED TO BE SMOKING. MAINTENANCE REPLACED 27H READING LAMP OPERATIONAL CHECK IS SATISFACTORY.
Part: PUMP — LEAKING (HYDRAULIC SYS)
FLIGHT 701, FRA-PHL -AT 1551Z ACARS MESSAGE WAS SENT NOTING A GREEN HYDRAULIC SYSTEM LEAK. WHEN MESSAGE WAS RECEIVED WE WERE WORKING WITH GREEN SYSTEM HYDRAULIC INOPERATIVE WHICH WOULD MEAN NO NOSE WHEEL STEERING. CREW WANTED THE EQUIPMENT STANDING BY IN CASE NEEDED A TOW TO GATE, EMERGENCY DECLARED ABOUT FIVE MINUTES PRIOR TO TOUCHDOWN. SAFE LANDING MADE AND AC TOWED TO THE GATE. MAINTENANCE REPLACED THE NR 1 AND NOT 2 EDP AND PERFORMED OPERATIONAL AND LEAK CHECK.
Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 58,885 hrs · 9,167 cycles
FLIGHT 701, FRA-PHL -AT 1551Z ACARS MESSAGE WAS SENT NOTING A GREEN HYDRAULIC SYSTEM LEAK. WHEN MESSAGE WAS RECEIVED WE WERE WORKING WITH GREEN SYSTEM HYDRAULIC INOPERATIVE WHICH WOULD MEAN NO NOSE WHEEL STEERING. CREW WANTED THE EQUIPMENT STANDING BY IN CASE NEEDED A TOW TO GATE, EMERGENCY DECLARED ABOUT FIVE MINUTES PRIOR TO TOUCHDOWN. SAFE LANDING MADE AND AC TOWED TO THE GATE. MAINTENANCE REPLACED THE NR 1 AND NR 2 EDP AND PERFORMED OPERATIONAL AND LEAK CHECK.
2012
Part: SKIN — GOUGED (FUSELAGE) · airframe 58,510 hrs · 9,118 cycles
RON VISIT - TWO ADJACENT GOUGES ON FUSELAGE SKIN AT FR70, S48R. REPAIRED FUSELAGE SKIN AT FR70, S48R IAW A330 53-00-11 FIG 234. IT WAS DETERMINED THAT GOUGES WERE CAUSED DUE TO SEPARATION OF THE AFT WATER SERVICE PANEL FROM THE AIRCRAFT.
Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 57,040 hrs · 8,919 cycles
FLIGHT 720, CLT - FCO - AT 80 KTS, "CABIN PRESS 1&2 FAULT," ABORTED TAKEOFF AT 100 KTS. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE CONTROLLER 2.
Part: SIGN — UNSECURE (CABIN) · airframe 56,567 hrs · 8,857 cycles
LAV AT 3L, FORWARD SIDE OF EXIT SIGN HAS FALLEN OFF, FLIGHT ATTENDANT PUT IT BACK BUT IT IS NOT SECURE. MAINTENANCE RE-SECURED EXIT SIGN AT 3L, OK FOR SERVICE.
Part: TERMINAL — UNCONTROLLABLE (CABIN) · airframe 56,340 hrs · 8,828 cycles
FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL SMELL FROM MID CABIN IFE. MAINTENANCE INSPECTED IFE CONSOLE FOR HOT OR BURNED RELAY, PLUGS AND WIRING WITH NO FAULTS FOUND. REMOVED AND REPLACED THE CREW TERMINAL, AT SEAT 7F DC ZONE TERMINATOR BOX AND POWER SUPPLY MODULE.
Part: LENS — MISSING (CABIN) · airframe 56,243 hrs · 8,816 cycles
EMERGENCY LIGHT COVER IN LAV L74 IS MISSING. MAINTENANCE REPLACED LENS AT L74.
Part: WIRE — PINCHED (CABIN) · airframe 55,697 hrs · 8,744 cycles
EMERGENCY LIGHT AC LEFT BY 3L DOOR AND OVERHEAD INOPERATIVE. MAINTENANCE FOUND PINCHED WIRE BEHIND PANEL 3L DOOR REPAIRED. OPERATIONAL CHECK IS GOOD.
Part: SKIN — SATURATED (RT ELEVATOR) · airframe 55,637 hrs · 8,732 cycles
C1 CHECK - 7 AREAS OF MOISTURE INGRESSION ON RIGHT ELEVATOR UPPER SURFACE AT ELEV RIBS 3, 5, 8, 10 & 11 FROM 2.875 TO 4.625 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW EO 5511U056, APPENDEX B- CASE 5.
Part: SKIN — SATURATED (LT ELEVATOR) · airframe 55,637 hrs · 8,732 cycles
C1 CHECK - TRAPPED WATER IN UPPER SURFACE OF LEFT ELEVATOR AT ELEV STA 6663 & 7143, ELEVATOR RIB 9. REPAIRED UPPER SURFACE OF LEFT ELEVATOR IAW EO 55110056, APPENDEX B CASE 5.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 55,637 hrs · 8,732 cycles
C1 CHECK - CRACK ON FLOOR PANEL BETWEEN FR57.1 TO FR58 & BETWEEN -Y2091.1 TO -Y693. REPAIRED FLOOR PANEL BETWEEN FR57.1 TO FR58, BETWEEN -Y2091.1 TO -Y693 IAW A330 AMM 25-50-00, 25-52-00-000-801A.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 55,637 hrs · 8,732 cycles
C1 CHECK - DELAMINATION ON FLOOR PANEL 232JF BETWEEN FR19 TO FR22 & BETWEEN -Y1959 TO -Y2462. REPLACED FLOOR PANEL 232JF IAW A330 SRM 53-02-00.
Part: DAMPER — MISINSTALLED (R4 DOOR) · airframe 55,637 hrs · 8,732 cycles
C1 CHECK - TELESCOPIC ROD ON R4 DOOR 843 DAMPER INSTALLED INCORRECTLY (UPSIDE DOWN). CORRECTLY RE-INSTALLED TELESCOPIC ROD ON R4 DOOR 843 DAMPER IAW A330 AMM 52-13-14. CHARGED DOOR DAMPER AND EMERGENCY CYLINDER IAW A330 AMM 52-10-00.
Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 54,985 hrs · 8,644 cycles
FLOOR LIGHTING ON THE SIDE OF SEAT 4G CLEAR LENS COVER IS OFF. MAINTENANCE SECURED LENS COVER, OPS TEST OF EMERGENCY LIGHTS CARRIED OUT SEAT 4G, OPERATED CORRECTLY.
2011
Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 54,203 hrs · 8,546 cycles
3R DOOR DOOR CROSS ISLE EMERGENCY LIGHT HAS WRONG LENSE. REMOVED AND REPLACED LENS. OPS CHECKED GOOD.
Part: SIGN — UNSECURE (CABIN) · airframe 52,983 hrs · 8,391 cycles
FRA - DOOR 3L EXIT SIGN FALLS OFF. MAINTENANCE INSTALLED 3L EXIT SIGN, OK FOR SERVICE.
Part: EPSU — INOPERATIVE (CABIN) · airframe 52,926 hrs · 8,384 cycles
CLT - EXIT LIGHT AT 3L BURNT OUT. RELEASED ON MEL. PHL - REPLACED L3 EMERGENCY EXIT DOOR EPSU PER AMM 33-51-38.
Part: STRUCTURE — CRACKED (LT WING) · airframe 52,827 hrs · 8,370 cycles
RON - LEFT WING CHORD IS CRACKED AT BOLT HOLES 7, 8 AND 10 LOCATED AT RIB 1 FR 42. REPLACED LEFT WING CHORD AT RIB 1 FR 42 IAW EA 103336.
Part: OVEN — FAULTY (GALLEY) · airframe 52,660 hrs · 8,348 cycles
FRA - FLT 704 CLT TO FRA. OVEN NR 1 IN ENVOY GALLEY PRODUCING AN ELECTRIC SMELL WHILE COOKING. CIRCUIT BREAKER PULLED TO DE-ACTIVATE. MAINTENANCE REMOVED AND REPLACED OVEN, OPS CHECK GOOD.
Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 52,385 hrs · 8,312 cycles
MAN - DOOR 3R ASSIST BOTTLE PX REQUIRES REPLENISHING. DOOR 3R ASSIST BOTTLE RECHARGED WITH NITROGEN.
Part: POWER SUPPLY — INOPERATIVE (EVAC SLIDE) · airframe 52,370 hrs · 8,310 cycles
PHL - EPSU 3R FAILS A-CHECK CARD "OPS CHECK EMERGENCY LIGHTS VIA MCDU" #33C22033002. REPLACED DR-3 SLIDE PER TASK 25-62-42. ALSO REPLACED EMERGENCY POWER SUPPLY UNIT.
Part: SLIDE — FAILED (R3 DOOR) · airframe 52,370 hrs · 8,310 cycles
PHL - EPSU 3R FAILS A-CHECK CARD "OPS CHECK EMERGENCY LIGHTS VIA MCDU" #33C22033002. REPLACED R-3 SLIDE PER TASK 25-62-42. ALSO REPLACED EMERGENCY POWER SUPPLY UNIT.
Part: COVER — OUT OF POSITION (CABIN) · airframe 52,356 hrs · 8,308 cycles
PHL - 3-R DOOR EMERGENCY EXIT LIGHT COVER MISSING. MAINTENANCE FOUND EXIT LIGHT COVER AND REINSTALLED.
Part: LENS — DISLODGED (CABIN) · airframe 52,243 hrs · 8,294 cycles
LGW - NO LENSE ON EMERGENCY LIGHT NEXT TO 4R LAV MAINTENANCE FOUND LENS + REFITTED NOW SATIS.
Part: FASTENER — LOOSE (CENTER WING) · airframe 50,787 hrs · 8,104 cycles
CWF - 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 SIDE AT RIB 1. BOLTS WERE REPLACED & AREA WAS SEALED IAW EA 117587C.
Part: LIGHT — INOPERATIVE (EXIT SIGN)
FRA - THE L3 DOOR EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L3 DOOR EMERGENCY EXIT LIGHT ASSEMBLY.
2010
Part: ATTACH FITTING — CORRODED (RT PYLON) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON RIGHT PYLON WING TO ATTACH FITTING ON OUTBOARD SIDE WHERE LOWER ATTACH BOLT INSTALLS AT RIB 12. REMOVED CORROSION ON RIGHT PYLON WING TO ATTACH FITTING. FOUND TO BE WITHIN LIMITS IAW EA 134330A.
Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - NR 2 PYLON STIFFENER CRACKED AT STATION 6261. REPAIRED NR 2 PYLON STIFFENER AT STATION 6261 IAW A330 SRM 51-42-11, 51-44-11, CMM 54-56-11.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON STRINGER AT FR65, S54L. REPAIRED STRINGER AT FR65, S54L IAW A330 SRM 53-00-13, 51-42-11 & 51-21-11.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - AVIONICS COMPARTMENT FLOOR SUPPORT ATTACH ANGLE (BRACKET) CRACKED AT FR 17 - FR 18. REPLACED AVIONICS COMPARTMENT FLOOR SUPPORT ATTACH ANGLE (BRACKET) AT FR 17 - FR 18 IAW A330 SRM 51-42-11, 51-75-12, 51-21-11 & 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON SEAT TRACK, FR 59, -Y2462. REPLACED SEAT TRACK, FR 59, -Y2462 IAW A330 SRM 53-00-15.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR SUPPORT FR73A BETWEEN Y1570 TO Y1950. REPLACED FLOOR SUPPORT FR73A BETWEEN Y1570 TO Y1950 IAW A330 SRM 51-42-11 & 51-44-11.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RT CABIN CREASE BEAM WEB, FR 78 AND FR 79 BOTTOM SURFACE AROUND SCREW HOLES. REPLACED RT CABIN CREASE BEAM WEB, FR 78 AND FR 79 IAW A330 SRM 51-42-11, 53-41-14 FIGURE 11, 51-74-00 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 74 - FR 75, +Y793. REPLACED FLOOR SUPPORT AT FR 74 - FR 75, +Y793 IAW A330 SRM 53-41-14.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,513 cycles
BFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR79, Y1447. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR79, Y1447 IAW A330 SRM 51-41-11, 51-21-11, 51-72-11 & 51-44-00.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT LONGERON AT FR 75 -Y450. REPLACED FLOOR SUPPORT LONGERON AT FR 75 -Y450 IAW A330 SRM 51-44-11 & 51-42-11.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON CREASE BEAM WEB BETWEEN FR 77 & FR78 BOTTOM SURFACE AROUND SCREW HOLES. REPLACED CREASE BEAM WEB BETWEEN FR 77 & FR78 IAW A330 SRM 51-42-11, 51-72-11 7 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT LONGERON UPPER FLANGE AT FR 74, -Y1137. REPLACED FLOOR SUPPORT LONGERON AT FR 74, -Y1137 IAW A330 SRM 51-42-00, 51-44-11 & 51-75-12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON SEAT TRACK AT FR 16A - FR 17, -Y953. REPLACED SEAT TRACK AT FR 16A - FR 17, -Y953 IAW A330 SRM 53-11-15 FIGURE 101, & 51-42-11.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RT CREASE BEAM WEB BETWEEN FR 79 AND 80 BOTTOM SURFACE ARUND SCREW HOLES. REPLACED RT CREASE BEAM WEB BETWEEN FR 79 AND 80 IAW A330 SRM 51-42-11, 51-44-11 & 51-74-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,351 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR772 TO FR75, Y450. REPLACED SEAT TRACK BETWEEN FR772 TO FR75, Y450 IAW A330 SRM 51-42-11 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT ANGLE UPPER FLANGE BETWEEN FR 75A THRU 77 -Y1950. REPLACED FLOOR SUPPORT ANGLE BETWEEN FR 75A THRU 77 -Y1950.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT FR 11- FR13, -Y721.6. REPLACED FLOOR SUPPORT FR 11- FR13, -Y721.6 IAW A330 SRM 53-11-14 FIGURE 101, 51-42-11 & 51-72-11.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 49,358 hrs · 79,130 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR PANEL 272KF, FR 73-FR 80. REPLACED FLOOR PANEL 272KF, FR 73-FR 80 IAW TRM 53-02-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 67, +Y480. REPLACED FLOOR SUPPORT AT FR 67, +Y480 IAW A330 SRM 51-42-11 & 53-41-14.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR33 TO FR37, Y953. REPLACED SEAT TRACK BETWEEN FR33 TO FR37, Y953 IAW A330 SRM 53-00-15, 51-74-00 & 51-42-11.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 43,958 hrs · 79,130 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR PANEL 271KF. REPLACED FLOOR PANEL 271KF IAW TRM 53-02-01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR68 TO FR71, Y450. REPLACED SEAT TRACK BETWEEN FR68 TO FR71, Y450 IAW A330 SRM 51-42-11, 51-72-11 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON RT CABIN FLOOR SUPPORT AT FR 75A BET -Y794 & -Y137. REPLACED RT CABIN FLOOR SUPPORT AT FR 75A BET -Y794 & -Y137 IAW A330 SRM 53-00-40 & 51-42-11.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON THE LEFT CREASE BEAM WEB AT FR79 - FR 80. REPLACED LEFT CREASE BEAM WEB AT FR79 - FR 80 IAW A330 SRM 51-42-11, 51-72-11 & 51-21-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON SEAT TRACK, FR14A-FR18, Y 450. REPLACED SEAT TRACK, FR14A-FR18, Y 450 IAW A330 SRM 53-11-15 FIGURE 101, 51-74-00, 51-42-11.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON CREASE BEAM WEB AT FR 75A - FR 77, +Y1447.8. REPLACED CREASE BEAM WEB AT FR 75A - FR 77, +Y1447.8. IAW A330 SRM 51-42-11 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,658 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT (LONGERON) BETWEEN FR75 TO FR76, Y=0. REPLACED FLOOR SUPPORT (LONGERON) BETWEEN FR75 TO FR76, Y=0 IAW A330 SRM 51-42-11, 51-72-11, 53-41-14 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT (SEALING PLATE) AT FR 80, -Y393. REPLACED FLOOR SUPPORT (SEALING PLATE) AT FR 80, -Y393 IAW A330 SRM 51-44-11, 53-41-14 & 51-74-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK 2 INCHES AFT OF FR33, Y2462. REPLACED SEAT TRACK 2 INCHES AFT OF FR33, Y2462 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR33 TO FR34, Y2462. REPLACED SEAT TRACK BETWEEN FR33 TO FR34, Y2462 IAW A330 SRM 51-44-11, 51-75-12 & 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR71, -Y1137. REPLACED SEAT TRACK AT FR71, -Y1137 IAW A330 SRM 53-00-15, 51-42-11, 51-44-00, 53-41-14, 51-75-12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR60 TO FR61, -Y450. REPLACED SEAT TRACK BETWEEN FR60 TO FR61, -Y450 IAW A330 SRM 51-42-11, 51-44-11, 51-75-12, 53-00-15.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK 6 INCHES AFT OF FR43, -Y450. REPLACED SEAT TRACK 6 INCHES AFT OF FR43, -Y450 IAW A330 SRM 51-42-11, 51-44-11, 51-75-12.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR BEAM SUPPORT AT FR80 + 6 INCHES, Y393. REPLACED FLOORBEAM SUPPORT AT FR80 + 6 INCHES, Y393 IAW A330 SRM 51-42-11 & 53-41-14.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR53.2 TO FR53.3, -Y450. REPLACED SEAT TRACK BETWEEN FR53.2 TO FR53.3, -Y450 IAW A330 SRM 53-31-51, 51-42-11, 51-44-11, 51-75-00.
Part: SLEEVE — CORRODED (RT PYLON) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON RIGHT PYLON RIB 12 PYLON TO RIB ATTACH FITTING OUTBOARD LOWER ATTACH SLEEVE UNDER HEAD FLANGE AT WS 6261. REPLACED RIGHT PYLON RIB 12 PYLON TO RIB ATTACH FITTING OUTBOARD LOWER ATTACH SLEEVE UNDER HEAD FLANGE AT WS 6261 IAW A330 AMM 54-51-17-400-803.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOORBEAM SUPPORT AT FR73, Y793. REPLACED FLOORBEAM SUPPORT AT FR73, Y793 IAW A330 SRM 51-42-11, 53-41-14 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR80, Y457. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR80, Y457 IAW A330 SRM 51-42-11 & 53-41-14.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOORBEAM SUPPORT BETWEEN FR72 TO FR73, -Y1237. REPLACED FLOORBEAM SUPPORT BETWEEN FR72 TO FR73, -Y1237 IAW A330 SRM 51-42-11 & 53-41-14.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR33 TO FR34 & BETWEEN FR36 TO FR37, Y450. REPLACED SEAT TRACK BETWEEN FR33 TO FR34 & BETWEEN FR36 TO FR37, Y450 IAW A330 SRM 53-00-15, 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR37.4 TO FR38, -Y450. REPLACED SEAT TRACK BETWEEN FR37.4 TO FR38, -Y450 IAW A330 SRM 53-00-15, 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR47 TO FR48, Y450. REPLACED SEAT TRACK BETWEEN FR47 TO FR48, Y450 IAW A330 SRM 51-44-11.
Part: PIN — CORRODED (LT PYLON) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR -S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LT PYLON TOP SLEEVE (PIN) OF PYLON TO WING ATTACH FITTING. REPLACED LT PYLON TOP SLEEVE (PIN) OF PYLON TO WING ATTACH FITTING IAW A330 AMM 54-51-17.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR30.5 TO FR33.5, Y1959. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR33.5, Y1959 IAW A330 SRM 53-00-15, 51-42-11, 51-40-04.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR58 TO FR62, Y2462. REPLACED SEAT TRACK BETWEEN FR58 TO FR62, Y2462 IAW A330 SRM 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR57.3 TO FR57.4, -Y450. REPLACED SEAT TRACK BETWEEN FR57.3 TO FR57.4, -Y450 IAW A330 SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR35, -Y1456. REPAIRED SEAT TRACK AT FR35, -Y1456 IAW A330 SRM 51-74-00, 51-42-11, 53-00-15, 51-44-11, 51-21-00, 51-23-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR63 TO FR64, -Y2462. REPLACED SEAT TRACK BETWEEN FR63 TO FR64, -Y2462 IAW A330 SRM 53-00-15, 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR74 TO FR75, Y450. REPLACED SEAT TRACK BETWEEN FR74 TO FR75, Y450 IAW A330 SRM 53-00-15, 52-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR73 TO FR74, -Y450. REPLACED SEAT TRACK BETWEEN FR73 TO FR74, -Y450 IAW A330 SRM 51-42-11, 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR57.2, -Y2462. REPLACED SEAT TRACK AT FR57.2, -Y2462 IAW A330 SRM 53-00-15, 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 CORROSION ON SEAT TRACK, FR14A - FR17, -Y450. REPLACED SEAT TRACK, FR14A - FR17, -Y450 IAW A330 SRM 53-11-15 FIGURE 101.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR40 TO FR47, Y1959. REPLACED SEAT TRACK BETWEEN FR40 TO FR47, Y1959 IAW A330 SRM 51-42-11, 51-72-11, 51-44-11, 51-75-12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR33.5 TO FR37, -Y450. REPLACED SEAT TRACK BETWEEN FR33.5 TO FR37, -Y450 IAW A330 SRM 53-00-15, 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR73 TO FR74, Y1237. REPLACED FLOOR SUPPORT BETWEEN FR73 TO FR74, Y1237 IAW A330 SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR30.5 TO FR33, -Y450. REPLACED SEAT TRACK BETWEEN FR30.5 TO FR33, -Y450 IAW A330 SRM 53-00-15, 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT, FR 76, +Y1447. REPLACED FLOOR SUPPORT, FR 76, +Y1447 IAW A330 SRM 51-72-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR22, -Y450. REPAIRED SEAT TRACK AT FR22, -Y450 IAW A330 SRM 51-42-11, 53-00-15, 51-44-11, 51-21-11, 51-75-12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR74, -Y1230. REPLACED SEAT TRACK AT FR74, -Y1230 IAW A330 SRM 53-00-15, 51-42-11, 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR78, Y381. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR78, Y381 IAW A330 SRM 51-42-11 & 53-00-15.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK BETWEEN FR30 TO FR30.5, -Y450. REPLACED SEAT TRACK BETWEEN FR30 TO FR30.5, -Y450 IAW A330 SRM 53-00-15.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR37, Y953. REPLACED SEAT TRACK AT FR37, Y953 IAW A330 SRM 53-00-15.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR 74, -Y1230. REPLACED SEAT TRACK AT FR 74, -Y1230 IAW A330 SRM 53-00-15, 51-42-11 & 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR33, Y1959. REPLACED SEAT TRACK AT FR33, Y1959 IAW A330 SRM 53-00-15.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR75 TO FR78, -Y381. REPLACED FLOOR SUPPORT BETWEEN FR75 TO FR78, -Y381 IAW A330 SRM 51-42-11, 51-72-11 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT AT FR72, -Y1186. REPLACED FLOOR SUPPORT AT FR72, -Y1186 IAW A330 SRM 51-41-14, 51-44-11 & 51-72-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN FR71 TO FR73, -Y1137. REPLACED FLOOR SUPPORT BETWEEN FR71 TO FR73, -Y1137 IAW A330 SRM 51-42-11 & 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 78, Y = 0. REPLACED LOOR SUPPORT AT FR 78, Y = 0 IAW A330 SRM 53-41-14, 51-72-11 & 51-44-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - S2 - MAJOR REPAIR - CORROSION ON MAIN CABIN SEAT TRACK AT FR37, Y450. REPLACED SEAT TRACK AT FR37, Y450 IAW A330 SRM 53-00-15.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR 76, -Y1447 TO -Y1950. REPLACED FLOOR SUPPORT AT FR 76, -Y1447 TO -Y1950 IAW A330 SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,358 hrs · 7,913 cycles
BFM - MAJOR REPAIR - S2 CHECK - CORROSION ON FLOOR SUPPORT AT FR 72, -Y1422. REPLACED FLOOR SUPPORT AT FR 72, -Y1422 IAW A330 SRM 53-41-14 & 51-42-11.
Part: WIRE — BROKEN (CABIN)
PHL - THE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT 13G/H. REPAIRED WIRING.
Part: WIRE — BROKEN (CABIN)
PHL - THE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT 28A/B. REPAIRED WIRING.
Part: BATTERY — DISCHARGED (FLASHLIGHT)
MAN - TORCH BATTERY AT DOOR R4 WAS INOPERATIVE. BATTERY REPLACED.
Part: FILTER — DIRTY (AC SYSTEM)
PHL - FLT 719 FCO TO PHL. THE CABIN CREW, AND SEVERAL PASSENGERS, EXPERIENCED DISCOMFORT DUE TO APPARENT "DUSTY" AIR FLOW FROM A/C AIR SYSTEM. THE FLIGHT CONTINUED TO PHL WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED ALL EIGHT CABIN RECIRC FILTERS. FOUND VERY DIRTY.
Part: DIAPHRAGM — LEAKING (R1 DOOR) · airframe 45,824 hrs · 7,439 cycles
BFM - EES - C1 CHECK - R-1 DOOR ASSIST BOTTLE PRESSURE IS LOW. REPLACED THE PERCUSSION MECHANISM DIAPHRAGM AND RE-SERVICED THE R1 DOOR ASSIST BOTTLE IAW A330 AMM 52-10-00-02 AND 52-10-00-03.
2009
Part: FLASHLIGHT — INOPERATIVE (CABIN)
PHL - R3 JUMPSEAT FLIGHT ATTENDANT FLASHLIGHT NOT FLASHING. REMOVED AND REPLACED JUMPSEAT FLASHLIGHT.
Part: WIRE — SHORTED (CABIN)
PHL - EPSU R3 FAULT WHILE ACCOMPLISHING A CHECK. RED UNIT FAULT ILLUMINATED ON EPSU. REPAIRED SHORTED WIRING AT ROW 9.
Part: EPSU — FAULTY (EMERGENCY LIGHTS)
PHL - FOUND THE R3 EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT.
Part: SKIN — CORRODED (FUSELAGE) · airframe 41,786 hrs · 6,903 cycles
BFM - MAJOR REPAIR - C1 CHECK - CORROSION ON FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE AT FRAME 40 BOTTOM FLANGE RT SIDE. REPLACED FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE AT FRAME 40 BOTTOM FLANGE RT SIDE IAW A330 SRM 51-42-11.
2008
Part: RELAY — UNSERVICEABLE (NR 1 ENGINE)
PHL FLT 754 - EN ROUTE PHL - CDG. DURING FLIGHT, RECEIVED ECAM MESSAGE "AUTO FLT A/THR OFF", AND " ENG 1 EPR MODE FAULT". THE FLIGHT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE ENGINE RELAY UNIT. OPERATIONALLY CHECKS OK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,702 hrs · 6,211 cycles
BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4523 / FR 56, +Y450. REPLACED CABIN SEAT TRACK, BS 4523 / FR 56, +Y450 IAW A330 SRM 51-42-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,702 hrs · 6,211 cycles
BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5478 / FR 70, +Y450. REPLACED CABIN SEAT TRACK, BS 5478 / FR 70, +Y450 IAW A330 SRM 51-42-00.
2007
Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 34,034 hrs · 5,843 cycles
FLIGHT 731, LGW-PHL: DURING CRUISE, GREEN HYDRAULIC SYSTEM QUANTITY BEGAN DROPPING. CAPTAIN DECLARED EMERGENCY INBOUND TO PHL. FLIGHT LANDED WITH NO DIFFICULTIES. MAINTENANCE REPLACED AN O-RING ON THE GREEN SYSTEM HIGH PRESSURE FILTER MODULE.
Part: RIB — CRACKED (RT WING) · airframe 33,239 hrs · 33,239 cycles
RT WING RIB 6 AT AFT APERTURE REFUEL PIPE ATTACHMENT FASTENERS. TEMPORARY REPAIR PER EA 98639. DEFECT SIZE: LESS THAN 1"