N381HA

Part: LANDING GEAR — FAULTED (RIGHT) · airframe 61,827 hrs · 10,055 cycles

ATB - MLG R LENGTHENING FAULT. ECAM HOT BRAKES. (#4 BRAKE 315) RAN ECAM, EXTENDED MLG, ONCE COOLED, UNABLE TO RETRACT. ECAM L/G R LENGTHENING FAULT. PERFORMED TSM 32-30-00-810-817-A THROUGH 4(A)3. PROX SENSORS MEASURED IN LIMITS BEFORE MLG SWING. AFTER MLG SWING AMM 32-31-00-710-801-A, PROX SENSORS OUT OF LIMITS. LUBED MLG SHORTENING MECH RT SIDE. PERFORMED CONTINUITY CHK OF 28GA2 TO PINS 6C&6D READ 8.1 OHMS & NO SHORTS TO GRND. CHK CONTIUNITY AT 28GA1 TO PINS 6C&6D. READ 9.3 OHMS & NO SHORTS TO GRND. CONTINUITY CHK GOOD. PERFORMED MLG SWING REF AMM 32-31-00. ADDED 2MM SHIM TO 28GA1 PROX SENSOR PER AMM 32-31-73. PERFORMED MLG SWING AND OPS CHK PER AMM 32-31-00. MLG SWING GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: FILTER — TRIPPED (APU) · airframe 61,645 hrs · 10,026 cycles

ETOPS - APU OIL LUBE FILTER DIFFERENTIAL PRESS IND POP OUT, AND UNABLE TO RESET. PER AMM 49-91-41-960-801-A, REPLACED APU OIL LUBE FILTER AND INSP FILTER COND CLEAN. T/S DELTA P IND STUCK. AFTER CLEANED, RESET SUCCESSFUL. APU RUN 10 MINS NO LEAKAGE FOUND. OK TO SERVICE

Part: WARNING LIGHT — ILLUMINATED (NR 1 ENGINE) · airframe 61,159 hrs · 9,948 cycles

ETOPS - ENGINE 1 OIL CHIP DETECT. PERFORMED DETAILED INSPECTION OF EMCD PER AMM 79-00-00-200-822-A. ACCEPTABLE LIMITS FOR ONE FLAKE COLLECTED. REMOVED AND CLEANED EMCD PER AMM 79-22-46. REPLACED SCAVENGE FILTER PER AMM 79-22-45. OPS AND LEAK CHK GOOD, OK FOR SVC.

Part: HYDRAULIC LINE — LEAKING (ZONE 700) · airframe 59,424 hrs · 9,653 cycles

ATB - AFTER TAKE OFF L/G RETRACTION FAULT. GEAR NEVER CAME UP. HOSE ON L/H L/G PITCH TRIMMER LEAKING. HOSE REPLACED IAW: 32-11-15-400-801-A (33) AND G SYST BLEEDING C/OUT. NIL LEAKS EVIDENT. PN ON: 201042197.

Part: HANDSET — DAMAGED (INTERPHONE) · airframe 58,143 hrs · 9,453 cycles

ETOPS - FA INTERPHONE AT 3L LOCATED, CORD IS DAMAGED. REMOVED AND REPLACED 3L HANDSET ASSY PER AMM 23-73-44. OK FOR SVC.

Part: ENGINE — MAKING METAL (ZONE 400) · airframe 57,964 hrs · 9,421 cycles

ETOPS - ENG 1 OIL CHIP DETECTED. REMOVED EMCD AND INSPECTED PER AMM 79-00-00-200-822-A. FOUND ONE FLAKE, ACCEPTABLE DEBRIS. REINSTALLED EMCD PER AMM 79-22-46-400-811. REMOVED AND INSPECTED SVAVENGE FILTER PER AMM 79-22-45-000-81. NO DEBRIS FOUND. INSTALLED NEW SCAVENGE FILTER PER AMM 79-22-45-400-801. OK FOR SVC. LEAK CHK GOOD.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 57,564 hrs · 9,361 cycles

4L EXIT SIGN AND OVERHEAD EXIT INOP. REMOVED AND REPLACED ESPU (17WL) PER AMM 33-51-38. OPS CHECK TEST OK.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 57,564 hrs · 9,361 cycles

3L DOOR EXIT SIGNS DO NOT ILLUMINATE. REMOVED & REPLACED 3L DOOR EXIT SIGN EPSU ASSY AND CHECKED OK PER A330 AMM 33-51-38. A/C OK FOR CONTINUE SVC,

Part: MICROPHONE — MALFUNCTIONED (ZONE 200) · airframe 57,321 hrs · 9,325 cycles

ETOPS - CA HAND MICROPHONE TRANSMITS INTERMITTENTLY. REPLACED HANDMIC. OPS CK OK PER AMM 23-73-00. OK FOR SERVICE

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 57,153 hrs · 9,294 cycles

ETOPS - AIR ENG 2 BLEED UPON ENG 2 SHUT DOWN. REMOVED AND REPLACED ENGINE 2 HPV BLEED VALVE PER AMM 36-11-51 OPS AND LEAK CHECK GOOD. VALVE WAS REPLACED DUE TO MULTIPLE HITS .

Part: CHIP DETECTOR — ACTIVATED (ENGINE NR 1) · airframe 56,814 hrs · 9,248 cycles

ETOPS - AFTER ENGINE SHUTDOWN, ECAM ENG 1 OIL CHIP DETECTED. PERFORMED TSM 79-20-00-810-823A. REMOVED AND REPLACED ENG 1 SCAVENGE FILTER REF AMM 79-22-45. REMOVED AND REPLACED ENG 1 EMCD REF AMM 79-22-46. OPS/LEAK CHK GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: FILTER — UNKNOWN · airframe 56,529 hrs · 9,206 cycles

ETOPS - REMOVED ENG #1 EMCD AND SCAVENGE OIL FILTER FOR INSPECTION. REMOVED AND REINSTALLED EMCD PER AMM 79-22-46. REMOVED AND REPLACED OIL SCAVENGE FILTER PER AMM 79-22-45. OPS CHK GOOD. LEAK CHK GOOD OK FOR SVC.

Part: A/C PACK — FALSE INDICATION (NR 2) · airframe 56,090 hrs · 9,137 cycles

ETOPS - AFTER ENGINE START AIR PACK 2 REG FAULT BLOCK TURN BACK. PERFORMED WIRE CHECK & INSULATION CHECK PER TSM 21-52-00-810-813-A RAN BOTH ENGINES NO PACK 2 FAULT DETECTED. REMOVED AND REPLACED PACK CONTROLLER 2 PER AMM 21-53-34. SYSTEM TEST OF PACK CONTROL & INDICATING SYSTEM SUCCESSFUL.

Part: MICROPHONE — BROKEN (HEATSET) · airframe 55,451 hrs · 9,043 cycles

ETOPS - HEADSET MIC BROKEN. REPLACED F/O HEADSET. OPS CK OK PER AMM 23-73-00. OK FOR SERVICE

Part: INTERPHONE — DETACHED · airframe 55,405 hrs · 9,037 cycles

ETOPS-4R DOOR INTERPHONE CORD HAS COME OFF. REMOVED AND REPLACED 4R F/A HANDSET PER 23-73-44. OPS CK GOOD. OK FOR SERVICE.

Part: LINE — LEAKING (HYD SERVO) · airframe 55,300 hrs · 9,021 cycles

ATB - HYD G SYS LEAK. FOUND RT WING OTBD AILERON SERVO LINE LEAKING. REMOVED AND REPLACED RT WING OTBD AILERON SERVO LINE PN AE2463926G0090 PER AMM 27-14-51 STEP 4.A.(14) & BLED AILERON SERVO CONTROL PER STEP 4.E.(1) THRU 4.E.(4). OPS & LEAK CHECKS OK. OK FOR SVC.

Part: FUEL LINE — DAMAGED (FUEL INJECTOR) · airframe 54,893 hrs · 8,962 cycles

ETOPS - FUEL DRIPPING FROM BOTTOM OF ENG #2 FAN COWL. FOUND FUEL EJECTOR LINE P/N FK22657 CHAFFE DAMAGE AND PIN HOLE. REMOVED AND REPLACED LINE AND CUSHION CLAMPS. LEAK CHECK GOOD PER AMM 73-12-41. OK FOR SERVICE.

Part: HANDSET — CRACKED (R3) · airframe 54,442 hrs · 8,893 cycles

ETOPS- 3R HANDSET PLASTIC CRACKED AT WIRE. REMOVED AND REPLACED 3R HANDSET PER AMM 23-73-44. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,001 hrs · 8,825 cycles

OTHER - ECAM ENG1 OIL CHIP DETECTED AFTER LANDING. ENG1 OIL CHP DETECTOR GOOD. REPLACED PRECAUTIONARY ENG1 SCAVENGE OIL FILTER PER TSM 79-20-00-869-052-A, 4, B. LEAK TEST OKAY. SECURITY CHECK OK. OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,969 hrs · 8,820 cycles

ETOPS - L1 PA WEAK. REPLACED 1L HANDSET, OPS CHK OK REF AMM 23-73-44.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,687 hrs · 8,777 cycles

DIV - A/C OSCILATES DURING CLIMB FROM 14,000-34,000 FT. WITH ASSOCIATED LEFT O/B AIRLERON MOVEMENT. NO OSCILATES IN CRUISE ON DESCENTS. REPLACED LH OUTBOARD (GREEN) AILERON SERVOVALVE IAW TSM 27-10-00-10-831-A & AMM 27-14-51-400-803. LEAK CHECK GOOD. OPS CHECK GOOD. BITE GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 53,017 hrs · 8,675 cycles

ETOPS - ENG2 CTL SYS FAULT ECAM MSG DISPLAYED ON SHUTDOWN. REMOVED AND REPLACED #2 ENG VSV CONTROLLER PER AMM 75-33-51. OPS CHK LEAK CHK OK. HIGH POWER RUN PER AMM 71-00-00 CHK OK. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,566 hrs · 45,664 cycles

AGGRESSIVE NOSE WHEEL SHIMMY ON BOTH T.O AND LANDING ROLL. FOR NOSE WHEEL SHIMMY, FOUND RH NOSE GEAR AXEL SLEEVE DAMAGED. REMOVED AND REPLACED NOSE GEAR AXEL SLEEVE (RIGHT SIDE) PER AMM 32-41-14. REMOVED AND REPLACED #1 NLG TIRE PER AMM 32-41-12. SPIN AND SECURITY CHECK GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,566 hrs · 45,664 cycles

ETOPS - AIR ENG 1 BLEED HI TEMP ECAM ON DESCENT 7000' IT DID NOT RESET 290 DEGREE C. REMOVED AND REPLACED FAN AIR VALVE CONTROL THERMOSTAT FILTER PER AMM 36-11-43. IDLE ENGINE RUN PERFORMED. NO FAULT NOTED. NO LEAKS NOTED. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,082 hrs · 8,527 cycles

OTHER - DURING DESCENT FAINT ODOR OF WET SOCKS DETECTED. ACCOMPLISHED LEVEL A MANUAL DECONTAMINATION PER AMM 21-00-00-615-809-A. REMOVED AND REPLACED SCAVANGE FILTER PER AMM 49-91-41-400-802-A. NO METAL SHAVING FOUND. LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,078 hrs · 8,526 cycles

"ETOPS - PLANE STILL SMELL OF OIL AND DIRTY SOCKS. ECS FORWARD FILTER ELEMENTS 5250HG,5251HG, 5252HG AND 5253HG REMOVED AND REPLACED AS PER AMM TASK 21-21-41-400-801-A. OPS CHECK ACCOMPLISHED. NIL ODOR, NIL FAULTS"

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,078 hrs · 8,526 cycles

OTHER - WHEN ENTERING THE PLANE, STRONG ODOR THROUGHOUT THE PLANE. F/A ARE COMPLAINING. INSPECTION ACCOMPLISHED. APU OIL FILLER HOUSING ASSY FOUND DETACHED. RESECURED USING SEAL AND HARDWARE. AMM REF 20-21-11-911-801A. LEVEL A MANUAL DECONTAMINATION OF ECS ACCOMPLISHED. AMM REF 21-00-00-615-809-A.

Part: GENERATOR — ABNORMAL (APU) · airframe 49,848 hrs · 8,163 cycles

ETOPS - APU GENERATOR KICKED OFF AFTER GND POWER REMOVED, ATTEMPTED ONE RESET FAILED AGAIN. ACCOMPLISHED TSM 24-20-00-810-997-A, BITE TEST OF ECMU1 FAULTING MESSAGE BTC-1(11XU1) / ECMU1(1XM1). REMOVED AND REPLACED BTC-1 (11XU1) REF AMM 24-22-55-000-803 AND AMM 24-22-55-400-803, BITE TEST ECMU1 NIL HELP GIVING SAME MESSAGE. REMOVED AND REPLACED ECMU-1(1XM1) PER AMM 24-29-34-400-801. BITE TEST OK. RUN APU AND ENG #1 FOR 10 MINS, NO FAULTS NOTED.

Part: TRANSDUCER — FAULTED (APU) · airframe 49,848 hrs · 8,163 cycles

APU AUTO SHUTDOWN ON VERIFICATION FLIGHT. REMOVED & REPLACED PRESS TRANSDUCER PER A330 AMM 49-23. AS PRECAUTION PER MCC REPLACED APU ECB PER A330 AMM 49-61. OPS CHK OF APU CHKS GOOD. VOLT/FREQS GOOD. LOAD CHK GOOD. NO FAULTS/MSGS AT THIS TIME. APU TEST OK. PSI XDCR S/N OFF 980478 S/N ON 34345

Part: APU — SHUTDOWN (ZONE 100) · airframe 49,841 hrs · 8,161 cycles

APU AUTO SHUTDOWN ON VERIFICATION FLIGHT. STILL IN WORK

Part: FIRE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 49,564 hrs · 8,115 cycles

APPROX. 2- HOURS INTO FLIGHT MW LAV TRASH BIN FIRE ALARM. CABIN CREW CHECKED ALL LAVS AND SPOKE TO PAX - NO FIRE IN LAV OR BIN. VISUALLY INSPECTED LAVATORIES NO EVIDENCE OF FIRE PERFORM TSM 26. SMOKE DETECTOR TEST AND ALL LAVS TEST GOOD

Part: NONE — NONE · airframe 48,430 hrs · 7,948 cycles

SHIP 381 EXIT PLACARD AT DOOR 3R FELL OFF. CORRECTIVE ACTION: RESECURED EXIT SIGN LENS AT 3R DOOR. (9322169)

Part: NONE — NONE · airframe 48,120 hrs · 7,860 cycles

APU VERIFICATION FAILED / UNSAT AIR TURN BACK CONDUCTED BACK TO HNL // UPON ARRIVAL FOUND LUBE FILTER DPI POPPED ALONG WITH FOD IN FILTER HOUSING. OIL SIGHT GLASS AT 0 OR CLOSE TO 0 1834731 7/20/2022. REMOVED APU OIL PUMP MODULE PER AMM 49-91-45 TO INSPECT INLET SCREEN FILTER, INSPECTION ACCOMPLISHED PER AMM 49-91-45-200-802-A AND FOUND DEBRIS. INLET SCREEN FOUND DAMAGED WITH FOD AND NEEDS TO BE REPLACED 1834731 7/21/2022. FOUND APU GEN DAMAGED. REMOVED APU GEN PER AMM 24-23-51. AS A PRECAUTIONARY, PERFORMED TSM 49-62-00-810-837-A STEPS 4.A.(2) DRAG FOR MAUAL DRIVESHAFT WAS 50 INCH POUNDS WITHIN LIMITS 2537249. INSTALLED INLET SCREEN AND APU OIL PUMP MODULE PER AMM 49-91-45. OPS AND LEAK CHECK GOOD. PERFORMED TSM 49-62-00-810-916-A. REPLACED LUBE AMD SCAVENGE FILTERS AND RAN APU FOR 15 MINS 2133186. NO CONTAMINATIONS NOTED IN FILTERS OR OIL. INSTALLED NEW LUBE AND SCAVENGE OIL FILTERS. INSTALLED APU GEN REF AMM 24-23-51 UP TO STEP 4.C.(3). 2133186 21JUL22. NEED TO REPLENISH APU OIL AND OPS LEAK CHECK APU GEN. AND INSTALL INTAKE PLENUM. CONTINUED ON REMAINING STEPS. OPS,LEAK, AND GENERATOR TEST GOOD PER AMM 24-23-57. OK FOR SERVICE.GENERATOR, APU, OFF 33-2423-9-0001 S/N 03134 ON 33-2423-9-0001 S/N 04895

Part: NONE — NONE · airframe 48,117 hrs · 7,866 cycles

SHIP 381 APU EMITTING DIRTY SOCK AND GARBAGE SMELL INTO CABIN. NO BURNING SMELL NOTED AT THAT TIME. CORRECTIVE ACTION: REMOVAL AND INSTALLATION OF APU. NO SMELL DETECTED. (9330637)

Part: NONE — NONE · airframe 48,106 hrs · 7,862 cycles

SHIP 381 MILD HYDRAULIC SMELL IN COCKPIT AFTER LANDING. ALSO IN CABIN. CORRECTIVE ACTION: DIRTY SOCK SMELL PRESENT WHEN APU BLEED IS SELECTED. WHEN ENGINES SUPPLY BLEED SMELL GOES AWAY. INSPECTED NBR 1 AND 2 ENGINES FOR EXTERNAL LEAKS, NONE NOTED. APU INLET PLENUM SHOWS SLIGHT OIL CONTAMINATION. ALL OIL LEVELS NORMAL ON ARRIVAL . INSPECTED DUCTING FORWARD OF EACH LT AND RT PACK OZONE CONVERTERS WITH UV LIGHT, DUCTS AND CONVERTERS CLEAN. PERFORMED A330 TSM TASK 05-50-00. DECISION TABLE LEADS TO APU AS SOURCE OF CONTAMINATION. PERFORMED DECONTAMINATION OF ECS SYSTEM. DIRTY SOCK SMELL DISAPPEARED 2-3 MIN INTO DECONTAMINATION AND DID NOT RETURN USING ENGINE BLEED. REMOVED AND REPLACED ALL RECIRCULATION FILTERS PER A330 AMM 21-21. AFTER FILTER CHANGES RAN PACKS WITH GROUND AIR AND THEN BOTH ENGINES. NO SMELL NOTED. (9330624)

Part: NONE — NONE · airframe 47,911 hrs · 7,824 cycles

SHIP 381 34H PATHWAY LIGHT INOP. CORRECTIVE ACTION: SECURED 34H PATHWAY LIGHT. (9319414)

Part: NONE — NONE · airframe 47,901 hrs · 7,821 cycles

SHIP 381 3L EXIT SIGN DID NOT ILLUMINATE W/ GEAR EXTENSION. CORRECTIVE ACTION: REMOVED AND REPLACED 14WL EPSU AND BATTERY PER A330 AMM 33-51-38. (8498793)

Part: NONE — NONE · airframe 47,826 hrs · 7,806 cycles

SHIP 381 SEAT 3L EXIT SIGN IS LOOSE. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT ASSY. PER A330 AMM 33-51. (8498718)

Part: NONE — NONE · airframe 47,790 hrs · 7,799 cycles

SHIP 381 47AB PHOTO STRIP MISSING. CORRECTIVE ACTION: INSTALLED PHOTO STRIP AND CHECKED OK PER A330 AMM 25-21. (8496862)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-450 (RH) FR 28 - FR 37.4 FOUND MULTIPLE CORROSION AT FR 31 - FR 32, FR 34 - FR 35.. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-450(RH) FR28 - FR37.4 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257464)

Part: NONE — NONE · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND SECTION Z BOTTOM AT FR 79 TO FR 80 AT RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2257550)

Part: NONE — NONE · airframe 47,604 hrs · 7,768 cycles

SHIP 381 LDMCR BUNK 2 UNABLE TO DEPLOY O2 MASK DURING AUTO DROP CHECK. CORRECTIVE ACTION: LDMCR BUNK 2 ROBBED FROM N380HA BUNK #2 AND INSTALLED AND OPERATIONAL CHCK C/O SATISFACTORY AS PER AMM 35-21-44. (2233825)

Part: NONE — NONE · airframe 47,605 hrs · 7,769 cycles

SHIP 381 FOUND FIBREGLASS DAMAGE AT SKIN NEAR RUDDER HINGE #8 (TOP OF RUDDER). CORRECTIVE ACTION: REMOVAL OF RUDDER CARRIED OUT IAW AMM NO 27-21-41. RUDDER SENT TO WORKSHOP FOR REPAIR REPAIR ON RUDDER CARRIED OUT AS PER ER/A 599354-14. REINSTALLED RUDDER. (2243114)

Part: NONE — NONE · airframe 47,605 hrs · 7,769 cycles

SHIP 381 DURING INSPECTION ON RUDDER (P/N: F5547108400000; S/N: TS6235), FOUND DISBOND/DELAMINATION AND FLUID INGRESS IN ZONE P AT T/E SCREW NO. #1, #8, #10, #11 & #14. CORRECTIVE ACTION: REMOVAL OF RUDDER CARRIED OUT IAW AMM NO 27-21-41. RUDDER SENT TO WORKSHOP FOR REPAIR REPAIR ON RUDDER CARRIED OUT AS PER ER/A 599354-14. INSTALLED RUDDER. (2243092)

Part: NONE — NONE · airframe 47,604 hrs · 7,768 cycles

SHIP 381 DURING OPS CHECK FOUND ENG 2 AFT BOTTLE PRESSURE SWITCH INOP. CORRECTIVE ACTION: REMOVED AND NEW BOTTLE INSTALLED AS PER AMM 26-21. (2230322)

Part: NONE — NONE · airframe 47,604 hrs · 7,768 cycles

SHIP 381 DURING OPS CHECK FOUND ENG #1 AFT BOTTLE PRESSURE SWITCH INOP. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF ENG #1 AFT FIRE BOTTLE IAW AMM 26-21-41. (2224924)

Part: FLOOR SUPPORT — CRACKED · airframe 47,604 hrs · 7,768 cycles

SHIP 381 BULK CARGO FLOOR STRUCTURE FR 68 SUPPORT STRUT FOUND CRACK. CORRECTIVE ACTION: BULK CARGO FLOOR STRUCTURE FR 68 SUPPORT STRUT REPLACED AS PER SRM 51-42-11. (2214286)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK AT WL Y953 LH, FROM FR 19 - 25.5, CORRODED AT 03 LOCATIONS ON CROWN. LOCATION: FR18, FR 20 AND FR 22. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257443)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, WATERLINE Y953 LH, FR 11 - FR 19, BADLY CORRODED. LOCATION: FR17. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257432)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, WATERLINE Y953 LH, FR 11 - FR 19, BADLY CORRODED. LOCATION: FR17. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214192)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK AT WL Y953 LH, FROM FR 19 - 25.5, CORRODED. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214184)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y1959 (LH), FR 28 - FR 37.4 FOUND MULTIPLE CORROSION BETWEEN FR 32 - FR 34. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y 1959 (LH), FR28 - FR37.4 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257469)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN FLOOR STRUCTURE RAIL AT Y-1959 BETWEEN FR 12A - FR 18 FOUND CORROSION AT MOUNTING POINT. RAIL LOCATED AT PAX DR 1 RIGHT. CORECTIVE ACTION: MAIN DECK CABIN FLOOR STRUCTURE RAIL AT Y-1959 BETWEEN FR12A - FR18 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214182)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-450 (RH) FR 28 - FR 37.4 FOUND MULTIPLE CORROSION AT FR 31 - FR 32, FR 34 - FR 35. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-450(RH) FR28 - FR37.4 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214284)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, WATERLINE -Y953 RH, FR 11 - FR 19, BADLY CORRODED. LOCATION: FR17. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-953, FR11 - FR19 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257447)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, WATERLINE Y953 RH, FR 11 - FR 19, BADLY CORRODED. LOCATION: FR17. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-953, FR11 - FR19 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214172)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND CORROSION ON LONGITUDINAL BEAM AT AFT CABIN AT FR 74-80, STRINGER -Y1137.1 ON RH SIDE. CORRECTIVE ACTION: MAIN DECK CABIN LONGITUDINAL BEAM AT Y-1137.1, FR74 - FR80 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257532)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-1959 RH FR53.2 - FR54 FOUND MULTIPLE CORROSION AT FR53.4, FR53.6. CORRECTIVE ACTION: MAIN DECK CABI SEAT TRACK AY Y-1959(R/H) FR 53.2 - FR 54 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257487)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y1959 (LH), FR 28 - FR 37.4 FOUND MULTIPLE CORROSION BETWEEN FR 32 - FR 34. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y 1959 (LH), FR28 - FR37.4 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214293)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN FLOOR STRUCTURE RAIL AT Y-1959 BETWEEN FR 12A - FR 18 FOUND CORROSION AT MOUNTING POINT. RAIL LOCATED AT PAX DR 1 RIGHT ENTRANCE. CORRECTIVE ACTION: MAIN DECK CABIN FLOOR STRUCTURE RAIL AT Y-1959 BETWEEN FR12A - FR18 REPLACED AS PER SRM 51-42-11 AND SRM 51-71-11. (2257537)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y2462 (LH) FR 28 - FR 37.4 FOUND MULTIPLE CORROSION AT FR 33 - FR 34, FR 35 - FR 36. . CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AY Y 2462(LH) FR28 - FR37.4 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257475)

Part: BEAM — CORRODED · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND CORROSION ON LONGITUDINAL BEAM AT AFT CABIN AT FR 74-80, STRINGER -Y1137.1 ON RH SIDE. CORRECTIVE ACTION: MAIN DECK CABIN LONGITUDINAL BEAM AT Y-1137.1, FR74 - FR80 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214359)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, FR 53.2 - FR 54.5, Y-2462 RH, BADLY CORODED. LOCATION: FR 53.3. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-2462, FR 53.2 - FR54.5 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214156)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-450 (RH), FR53.2 - FR53.4 FOUND MULTIPLE CORROSION AT FR53.2, FR53.4. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-450, FR53.2 - FR53.4 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214191)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-1959 (RH), FR53.2 - FR54, FOUND MULTIPLE CORROSION AT FR53.4, FR53.6. CORRECTIVE ACTION: MAIN DECK CABI SEAT TRACK AY Y-1959(R/H) FR 53.2 - FR 54 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214158)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y2462 (LH) FR 28 - FR 37.4 FOUND MULTIPLE CORROSION AT FR 33 - FR 34, FR 35 - FR 36. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AY Y 2462(LH) FR28 - FR37.4 REPLACED AS PER SRM 51-42-11, SRM 51-71-11. (2214288)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 MAIN DECK CABIN SEAT TRACK AT Y-450 RH FR53.2 - FR53.4 FOUND MULTIPLE CORROSION AT FR53.2, FR53.4. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-450, FR53.2 - FR53.4 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257490)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, FR 53.2 - FR 54.5, Y-2462 RH, BADLY CORODED. LOCATION: FR53.3. CORRECTIVE ACTION: MAIN DECK CABIN SEAT TRACK AT Y-2462, FR 53.2 - FR54.5 REPLACED AS PER SRM 51-42-11 & SRM 51-71-11. (2257454)

Part: NONE — NONE · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND SECTION Z AT FR 80/82, STRINGER -Y1137.1 TO -Y1447.8 RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2257546)

Part: NONE — NONE · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND SECTION Z AT FR 79 TO FR 80 AT RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2257547)

Part: NONE — NONE · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND SECTION Z BOTTOM AT FR 79 TO FR 80 AT RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2214260)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK, FR 71.5 - FR 75, Y450 LH BADLY CORRODED . LOCATION: FR72. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257449)

Part: FRAME — CRACKED · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND SECTION Z AT FR 79 TO FR 80 AT RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2214198)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, FR 71.5 - FR 75, Y-450 RH WITH 04 OFF DEEP CORROSION AREA. LOCATION: FR 72, FR 74, 74.5 & 75.. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257480)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN MAIN DECK, FR 71.5 - FR 75, Y-450 RH WITH 04 OFF DEEP CORROSION AREA. LOCATION: FR 72, FR 74, 74.5 & 75. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214254)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN AFT CABIN, FR 58.5 - FR 67.5, Y-450 RH WITH 04 DEEP CORROSION AREA. LOCATION: FR 61, 62, 63 & 67. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257482)

Part: STRINGER — CRACKED · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND SECTION Z AT FR 80/82, STRINGER Y1137.1 TO Y1447.8 LH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2214207)

Part: NONE — NONE · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND SECTION Z AT FR 80/82, STRINGER Y1137.1 TO Y1447.8 LH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2257542)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK, FR 71.5 - FR 75, Y450 LH BADLY CORRODED . LOCATION: FR72. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214257)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND 01 OFF SEAT TRACK IN AFT CABIN, FR 58.5 - FR 67.5, Y-450 RH WITH 04 DEEP CORROSION AREA. LOCATION: FR 61, 62, 63 & 67. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214197)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND CORROSION ON SEAT TRACK FROM FR 73.5 TO FR 74, STRINGER - YC1 ON RH SIDE. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214210)

Part: NONE — NONE · corrosion level 2 · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND CORROSION AT SEAT TRACK FROM FR 73.5 TO FR 74, STRINGER YC1 ON LH SIDE. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2214258)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND CORROSION AT SEAT TRACK FROM FR 73.5 TO FR 74, STRINGER YC1 ON LH SIDE. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257499)

Part: STRINGER — CRACKED · airframe 47,604 hrs · 7,768 cycles

SHIP 381 FOUND SECTION Z AT FR 80/82, STRINGER -Y1137.1 TO -Y1447.8 RH SIDE TO BE CRACKED. CORRECTIVE ACTION: SAID SECTION REMOVED AND REPLACED AS PER SRM 51-42-11. (2214205)

Part: NONE — NONE · corrosion level 2 · airframe 47,711 hrs · 7,785 cycles

SHIP 381 FOUND CORROSION ON SEAT TRACK FROM FR 73.5 TO FR 74, STRINGER - YC1 ON RH SIDE. CORRECTIVE ACTION: SAID SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11. (2257530)

Part: NONE — NONE · airframe 47,274 hrs · 7,708 cycles

SHIP 381 3L EMERG EXIT LT COVER LOOSE SECURED WITH TAPE. CORRECTIVE ACTION: RESECURED COVER. (8460353)

Part: DOOR — DEFECTIVE · airframe 46,754 hrs · 7,595 cycles

SHIP 381 4R DOOR WOULD NOT ARM. CORRECTIVE ACTION: PERFORMED INSPECTION OF 4R DOOR & DOOR JAM. FOUND DEBRIS (SCREW) WEDGED IN THE LOCKING MECHANISM. REMOVED. (7716115)

Part: NONE — NONE · airframe 46,191 hrs · 7,473 cycles

ETOPS - FOUND MCDU #3 BRT/DIM BUTTON BROKEN // REMOVED AND REPLACE MCDU #3 PER AMM 22-82-12. OPS TEST GOOD. NO DEFECT NOTED. OK FOR SVC UNIT, DISPLAY, OFF 33-2282-9-0003 S/N 53441 ON 33-2282-9-0003 S/N 49347

Part: NONE — NONE · airframe 46,006 hrs · 7,447 cycles

SHIP 381 ROW 39 R/H SIDE EMER LIGHT LENS COVER MISSING. CORRECTIVE ACTION: INSTALLED LENS AND SECURED. (7726591)

Part: TRANSDUCER — FAULTED (VIBRATION MONITO) · airframe 44,279 hrs · 7,137 cycles

ETOPS - ENG #2 VIB MONITORS DISPLAYED AS AMBER "X'S"//REPLACED VIBRATION TRANSDUCER PER AMM 77-32-11

Part: FCU — DEFECTIVE · airframe 44,167 hrs · 7,120 cycles

ETOPS - DUE TO FCU FAULT IN OGG- MOC REQUEST TO REPLACE FCU. // INSTALLED NEW FCU PER AMM 22-81-12, OPS TEST AND "LAND TEST" PASSED PER AMM 22-97-00. OK FOR SERVICE. UNIT, FLIGHT CO OFF 43-2281-9-0002 02025 ON 33-2281-9-0001 01281

Part: BOLT — SHEARED (STOP FITTING) · airframe 43,826 hrs · 7,067 cycles

EMERGENCY EQUIPMENT, FOUND TWO BOLTS SHEARED ON 1L FORWARD LOWER STOP FITTING AND STOP SCREW FACE CRACKED. CORRECTIVE ACTION: R & R 2 SHEARED BOLTS ON STOP FITTING, PER AMM 52-11. REMOVED & REPLACED 1L BEAM 8 FWD END STOP FITTING, REF AMM 52-11. ADJ PER AMM 52-11. OPERATIONS CHECK GOOD.

Part: ACCUMULATOR — DEFECTIVE (BLUE HYD SYS) · airframe 43,685 hrs · 7,036 cycles

ETOPS - BLUE HYD POWER ACCUMULATOR LEAKS INTERNALLY. REMOVED & REPLACED BLUE HYD ACCUMULATOR, PER AMM 29-12-42 UP TO STEP 4D(7). LEAK CHECK GOOD. PENDING STEP 4D(7). CHECK FOR AIR, 2158677. ACCOMPLISHED REMAINING STEPS. OK FOR SERVICE. ACCUMULATOR, PO OFF 33-2911-9-0006 03740 ON 33-2911-9-0006 05233.

Part: PLENUM — DELAMINATED (AC BAY) · airframe 43,634 hrs · 7,028 cycles

ETOPS SIGNIFICANT SYSTEM - DIRECT Z190 NT: LH PACK PLENUM FOUND BADLY DE-LAMINATED AT MOUNTING BOLT AREAS AND CRACK LINES AT AFT EDGE. // ELECTRICAL CONNECTORS 521HH5 AND 521HH7 DISCONNECTED. 1)LH PACK PLENUM CHAMBER, PRIMARY HEAT EX-CHANGER, MAIN HEAT EX-CHANGER AND DUCT ARE REMOVED AS A SINGLE UNIT AS PER AMM21-51-41-000-803-A. 2)LH PACK PLENUM CHAMBER REMOVED AS PER AMM21-52-22-000-801-A. 3)LH PACK PLENUM CHAMBER INSTALLED AS PER AMM21-52-22-420-801-A REV 75.02 SN: 2230A00LI000571, PN:2230A000-01, FOUND SATISFACTORY. 4)LH PACK PLENUM CHAMBER, PRI AND MAIN HEAT EX-CHANGER AND DUCT ARE INSTALLED AS A SINGLE UNIT AS PER AMM21-51-41-400-803-A, REL 75.02 FOUND SATISFACTORY. 5)ELECTRICAL CONNECTORS 521HH5 AND 521HH7 ELECTRICALLY CONNECTED IAW AMM21-52-41-400-801, FOUND NIL DEFECT. LEAK CHECK PERFORMED AT DUCT JOINTS AND PLENUM CHAMBER CONNECTIONS AS PER AMM12-33-21-018-801-A-02, REL 75.02, FOUND NIL LEAK AND DEFECTS. OP TEST OF PACK CONTROL AND INDICATING SYSTEM PERFORMED AS PER AMM21-53-00-710-801-A REL 75.02, FOUND NIL LEAK AND DEFECTS. OP TEST OF THE CONDITIONED SERVICE - AIR SYSTEM WITH BLEED AIR PERFORMED AS PER AMM21-58-00-710-803-A. REL 75.02, FOUND NIL LEAK AND DEFECTS. RESET OF THE HEAT EX-CHANGER TREND MONITORING VIA MCDU PERFORMED AS PER AMM21-53-00-740-801-A REV 75.02, FOUND NIL DEFECT. PN OFF: 2230A0000-01 PN ON: 2230A0000-01

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,634 hrs · 7,028 cycles

FUSELAGE SKIN FOUND SUSPECTED CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - STRINGER 42 LH. (AFT CUTOUT HOLE OF WASTE EXHAUST SYSTEM). // FUSELAGE SKIN CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - 42 LH REPAIRED AS PER REPAIR DESIGN APPROVAL SHEET REF. 80779761/003/2020 ISSUE A, ENGINEERING REPAIR/ AUTHORIZATION NO. 586365-14 REV ORIGINAL.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 43,634 hrs · 7,028 cycles

DURING CCK AND DURING INSPECTION PER EM 5753-01164, CORROSION WAS FOUND ON THE LH MLG RIB 6 FITTING. THE CORROSION WAS REWORKED PER SECT I OF ERA 586363-14AD. // THE REWORKED LH RIB 6 FITTING IS APPROVED FOR 30,033 TOTAL FLIGHT CYCLES OR 193,119 TOTAL FLIGHT HOURS (WHICHEVER COMES FIRST). CONTACT LIAISON ENGINEERING PRIOR TO THIS THRESHOLD FOR CONTINUED SERVICE OF THE FITTING AND AIRCRAFT.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 43,634 hrs · 7,028 cycles

FOUND EEPL DAMAGED AT GALLEY DOOR 2. // REPLACED PHOTO-LUMINESCENT STRIP FLOOR EMERGENCY ESCAPE PATH MARKING AS PER AMM 33-51-21-000-801 AND 33-51-21-400-801. OPS CHECK GOOD.

Part: AXLE — CORRODED (LANDING GEAR) · corrosion level 2 · airframe 43,634 hrs · 7,028 cycles

FOUND #5 AXLE SLEEVE WITH CORROSION ON SHOULDER. // #5 AXLE SLEEVE REPLACED AS PER AMM 32-41-14 REV 75.02

Part: LIGHT — UNSECURE (GALLEY) · airframe 42,471 hrs · 6,861 cycles

MID GALLEY PATHWAY LIGHT STRIP CAME OUT, NEEDS TO BE RE-SECURED. SECURED LIGHT STRIP.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR LOCK) · airframe 41,702 hrs · 6,732 cycles

AIRCRAFT 381 ATB-RETURNED TO HNL DUE TO THE FORWARD CARGO DOOR INTERMITTENT UNLOCKED ECAM MESSAGE APPEARED. PRESSURIZATION NOT AN ISSUE THE FLIGHT WAS AT 10000 FEET. DEFERRED PER MEL 52-70-1-HNL PERFORMED TSM TASK 52-31-00-810-803-A, NO FAULTS DETECTED. CLEANED AND INSPECTED FORWARD DOOR COMPARTMENT PROXIMITY SENSORS, NO DEFECTS NOTED. LP 5391956

Part: PROXIMITY SENSOR — DIRTY (CARGO DOOR) · airframe 41,702 hrs · 6,725 cycles

ATB - ON CLIMB FWD CARGO INTERMITTENT UNLOCKED ECAM, PRESSURIZATION NOT AN ISSUE AT TIME AS WE WERE 10000 LEVELED OFF 11000 THEN DESCENDED. PERFORMED TSM TASK 52-31-00-810-803-A, NO FAULTS DETECTED. CLEANED AND INSPECTED FWD DOOR COMPARTMENT PROX SENSORS NO DEFECTS NOTED. OK FOR SERVICE.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 41,363 hrs · 6,673 cycles

ETOPS SIGNIFICANT SYSTEM - OUTER-TANK FUEL INLET VALVE FAILED. // REMOVED AND REPLACED OUTER-TANK FUEL INLET VALVE (RH) PER AMM 28-25-57-OPS CHECK GOOD. OK FOR SVC. ACTUATOR, SINGLE OFF 43-2826-9-0002 58020 ON 43-2826-9-0001 46124

Part: ACCESS PANEL — OPEN (LT WING) · airframe 39,676 hrs · 6,423 cycles

TFOA - LT FUEL PANEL FOUND OPEN ON ARRIVAL TO LAX. FUEL CAPS MISSING & HOLD OPEN ROD DAMAGED. REPLACED FUEL COUPLING CAPS PER AMM 28-25 REPLACED STRUT PER AMM 57-42. DOOR OPS CHK GOOD. OK FOR SVC.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 39,049 hrs · 6,340 cycles

DOOR 3L EXIT LIGHT COVER BROKEN. REPLACED EXIT MARKING SIGN AT DOOR 3L.

Part: NOT REPORTED — MISSING (EXIT LIGHT) · airframe 38,707 hrs · 6,290 cycles

FLOOR LIGHT STRIP IN AFT GALLEY IS MISSING PARTS. REPLACED EMERGENCY LIGHT STRIP IN AFT GALLEY. LP 5847373

Part: GENERATOR — FAILED (NR 1) · airframe 38,302 hrs · 6,229 cycles

AIRCRAFT 381, DIVERTED TO HNL DUE TO THE NBR 1 GENERATOR FAILED IN FLIGHT. CORRECTIVE ACTION: REPLACED NBR 1 IDG AND GENERATOR CONTROL UNIT. LP 4966279, 4966281.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,769 hrs · 6,136 cycles

ETOPS SIGNIFICANT SYSTEM - DURING CLIMB ECAM A.ICE L OUTR WING HI PR - CREW AWARENESS. PERFORMED TSM 30.11.00.810.805A. A-ICE VALVES OPERATED NORMALLY. NO MSG'S, OK TO CONT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,721 hrs · 6,129 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER PARKING ON ENGINE SHUTDOWN, ENG 1 OIL CHIP DETECTED.// PERFORMED A330 TSM 79-20-00-810-823 FOUND NO DEBRIS ON ENG 1 EMCD. PERFORMED EMCD CLEANING FUNCTIONAL TEST AND EMCD TEST, GIVEN TEST OK. ENG RUN-UP TEST AND NO ECAM MESSAGES ON. OK FOR SVC. ENG RUN.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 IDG OIL SYS) · airframe 37,649 hrs · 6,118 cycles

ETOPS SIGNIFICANT SYSTEM - ELEC IDG 1 OIL SYS FAULT.// RESET ACFT ELEC SYS PER TSM 24-20-00. OPS NORMAL.

Part: FAIRING — PUNCTURED (LE SLAT) · airframe 37,457 hrs · 6,089 cycles

LEFT WING NR 4 CANOE FAIRING HAS A PUNCTURE ON BOTTOM. INSTALLED PERMANENT REPAIR IAW SRM 57-56-00-300. A/C OK FOR SERVICE.

Part: VALVE — OPEN (CABIN PRESSURE) · airframe 36,833 hrs · 5,999 cycles

AIRCRAFT 381, ATB TO HNL DUE TO THE CABIN ALT ECAM VENT EXTRACT VALVE FULL OPEN AT FL110. CORRECTIVE ACTION: FOUND VENT EXTRACT VALVE IN OPEN POSITION PER ME 21-26-2 (LP 4964629). VALVE NEED TO BE IN NOT FULLY OPEN POSITION PRIOR TO PUSHBACK. RE-POSITIONED VALVE PER MEL 21-26-2. LP 4964647

Part: VALVE — OPEN (CABIN PRESSURE) · airframe 36,839 hrs · 5,994 cycles

OPEN - ATB, AT FL370 CABIN ALT CLIMBED TO 11,000'. CABIN ALT ECAM VENT EXTRACT VALVE FULL OPEN. FOUND VENT EXTRACT VALVE IN OPEN POSITION, VALVE NEEDS TO BE IN NOT FULLY OPEN POSITION PRIOR TO PUSH BACK REF MPM 21-18-21-20.

Part: PRESSURE SWITCH — MALFUNCTIONED (OIL PRESSURE) · airframe 36,823 hrs · 5,991 cycles

SUP - ETOPS SIGNIFICANT SYSTEM - ON LANDING ENG 1 MINOR FAULT ECAM.// ACCOMPLISHED TSM 73-25-81-801-934-A FOUND LO OIL PRESS FAULT #1 ENG, REMOVED AND REPLACED #1 ENGINE LO OIL PRESSURE SWITCH PER AMM 79-34-15-000-804-A/400-804-A OPS/LEAK CK GOOD NO FAULTS ON GND SCAN DURING ENGINE RUN, OK FOR SVC.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 36,768 hrs · 5,984 cycles

ETOPS SIGNIFICANT SYSTEM - FUELERS ADVICE AIRCRAFT IS NOT ACCEPTING FUEL. REPLACED INR TK INLET VLV 1 ACTUATOR (603QL1) PER AMM 28-26-53-400-801-A. OPS TEST OK, AIRCRAFT FUELED OK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 36,423 hrs · 5,928 cycles

FUMES AFTER TAKEOFF AT 30,000 FT, ODOR OF BURNING PLASTIC THEN SWEET ODOR IN THE FLIGHT DECK & R3 DOOR AREA. FLT ATTENDANTS STATED NO ODOR NOTED IN CABIN. PERFORMED DUCT BURNOUT IAW IAW AMM 36-11 AND HIGH POWER RUNS IAW AMM 71-00. NO ABNORMAL ODORS NOTED. PERFORMED GVI OF APU BLEED FLEX DUCT, NO OIL OR CONTAMINATION FOUND. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 36,418 hrs · 5,927 cycles

FUMES PRESENT IN THE FLIGHT DECK ONLY ON DECENT THROUGH LANDING. WET SOCK ODOR. FLT ATTENDS STATED NO ODOR NOTED IN CABIN. . PERFORMED DUCT BURNOUT IAW A330 AMM 36-11 AND HIGH POWER RUNS IAW AMM 71-00. NO ABNORMAL ODORS NOTED. PERFORMED GVI OF APU BLEED FLEX DUCT NO OIL OR CONTAMINATION FOUND. ACFT OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 36,150 hrs · 5,882 cycles

APU LOW OIL LEVEL ON STARTING. SERVICED THE APU OIL SYSTEM TO FULL. INSPECTED FOR LEAKS AND GENERAL SECURITY OF APU COMPARTMENT. NO DEFECTS NOTED. OK FOR SERVICE.

Part: LUG — CRACKED (RT MLG) · airframe 35,896 hrs · 5,847 cycles

WHILE ACCOMPLISHING WC 5753-01164-02B, FOUND A CRACK ON THE FWD LUG OF THE RT MLG RIB 6.

Part: LUG — CRACKED (RT MLG) · airframe 35,891 hrs · 5,853 cycles

DURING LINE MAINTENANCE IN SEA, THE RT MLG SUPPORT RIB NR 6 AFT PINTLE FORWARD LUG WAS FOUND CRACKED WHILE ACCOMPLISHING EM 5753-01164-02B DETAILED VISUAL INSPECTION. REPLACED RIB 6 AND REAR PINTLE PIN ASSEMBLY.

Part: RIB — CRACKED (RT MLG) · airframe 35,893 hrs · 5,846 cycles

DURING AFT TRUNNION AD INSPECTION, FOUND THE RT WING MLG RIB 6 AFT BEARING LUG CRACKED. REMOVED AND REPLACED THE NR 6 RIB IAW ENGINEERING REPAIR AUTHORIZATION 570123-14AD. PERFORMED ALL SYSTEM AND OPERATIONAL CHECKS. AIRCRAFT OK FOR SERVICE IAW ERA 570123-14AD, REV ORIG.

Part: CHIP DETECTOR — FALSE INDICATION (NR 1 ENGINE) · airframe 35,464 hrs · 5,779 cycles

NR 1 ENGINE OIL CHIP DETECTED AFTER LANDING. IAW AMM 79-20-00-810-823-A, INSPECTED THE CHIP DETECTOR. NO DEBRIS FOUND. CLEANED AND REINSTALLED THE CHIP DETECTOR. PERFORMED EMCD TEST. TESTED OK.

Part: FCU — FAULTED · airframe 35,053 hrs · 5,712 cycles

AUTO FLT FCU FAULT, STATUS PAGE INDICATES PART FCU. ILLUMINATED WHEN CHANGING ALTITUDE FROM FL 400 TO FL 410. FAULT NOT CONFIRMED ON ARRIVAL. TROUBLESHOT IAW TSM 22-81-00-810-859A. NO FAULTS. NO 30 DAY HISTORY. PERFORMED LAND CAT 3 CAPABILITY TEST IAW AMM 22-97. ACFT IS OK FOR CAT 3 OPERATION.

Part: SCAVENGE PUMP — MALFUNCTIONED (GENERATOR) · airframe 35,006 hrs · 5,703 cycles

APU FAULT ECAM ILLUMINATED. APU LAST LEG SHOWS LUBE PUMP FILTER & GENERATOR SCAVANGE FILTER. PERFORMED TSM 49-62-00-810-916-A. LUBE AND GEN FILTERS SHOW NO METAL PARTICLES. BOTH DPIS NOT EXTENDED. APU WIRING CHECKED OK IAW TSM 49-62-00-810-916-A, STEP 4.D.(2)(B). REMOVED AND REPLACED THE GENERATOR SCAVENGE & LUBRICATION DELTA P SWITCHES AND COMPLETED TSM 49-62-00-810-916-A. OPS & LEAK CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 34,799 hrs · 5,673 cycles

ONE HOUR INTO FLT FUEL, A LOW FUEL PRESSURE L2 PUMP, RECYCLED PUMP OFF & ON, NO CHANGE, CLEARED ITSELF AFTER 5 MINUTES. PERFORMED AN OPS TEST OF THE MAIN & STANDBY PUMPS, AUTOMATIC AND MANUAL MODE IAW AMM 28-21-00-710-801A, NO DEFECTS NOTED, OK FOR SERVICE.

Part: FIRE DETECTOR — SHORTED (NR 2 PYLON) · airframe 34,142 hrs · 5,579 cycles

INTERMITTENT NR 2 ENGINE FIRE LOOP B FAULTED. REMOVED AND REPLACED FDU 2 IAW AMM 26-12-34, CONDITION SAME, ORIGINAL FDU REINSTALLED. FOUND PYLON DETECTOR 7WD2 READING 9.9 OHMS PIN C TO A OUT OF LIMITS AND SHORTED TO GROUND FROM STUD. REPLACED THE PYLON FIRE DETECTOR 7WD2 IAW AMM TASK 26-12-16-400-808-A. OPS CHECKED OK, NO FAULTS NOTED.

Part: REGULATOR VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 33,299 hrs · 5,449 cycles

AIR ENGINE NR 1 BLEED FAULT. PERFORMED BITE TEST OF BMC. FAULTED NR 1 PRESSURE REG VALVE, REMOVED AND REPLACED NR 1 PRESSURE REG VALVE PER AMM 36-11-52. LEAK CHECK AND BITE TEST GOOD. OK FOR SERVICE. VALVE, BLEED, P OFF 33-3611-9-0002 01965 ON 33-3611-9-0002 02595.

Part: SIGN — DETACHED (CABIN) · airframe 32,643 hrs · 5,363 cycles

EXIT SIGN AT DOOR 3R DETACHED FROM THE DOOR. RE-SECURED EXIT SIGN COVER.

Part: ACTUATOR — FAILED (LT INLET VALVE) · airframe 32,241 hrs · 5,298 cycles

LEFT INLET VALVE FAILED. OUTER TANK. REMOVED AND REPLACED THE OUTER TANK INLET VALVE ACTUATOR IAW AMM 28- 25-57. OPS CHECKED AND TESTED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 31,643 hrs · 5,216 cycles

NR 2 ENGINE HAD A MINOR FAULT AND NR 2 AIR EXCHANGER FAULT ILLUMINATED DURING ROLLOUT, AFTER MOVING THRUST REVERSER LEVER TO IDLE REVERSE POSITION. PERFORMED TSM 79-20-00-810-809-A, FADEC SYSTEM TESTED OK. AIR/OIL HEAT EXCHANGER VALVE OPERATES SMOOTHLY. OK FOR SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (NR 2 ENGINE) · airframe 31,545 hrs · 5,201 cycles

NR 2 ENGINE CONTROL SYS FAULT DURING SHUTDOWN. TROUBLESHOT THE NR 2 ENGINE CONTROL SYS IAW 71-00-00-810-924-A. ALL OPS NORMAL, UNABLE TO DUPLICATE FAULT. NO HISTORY. ACFT OK FOR SERVICE.

Part: MANIFOLD — LEAKING (NR 2 FUEL) · airframe 31,290 hrs · 5,165 cycles

FUEL LEAKING FROM NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE INBOARD FUEL MANIFOLD ASSEMBLY IAW AMM 73-11-43-400-802-A. LEAK CHECKED OK. ACFT OK FOR SERVICE.

Part: LINE — LEAKING (ENGINE OIL SYS) · airframe 30,831 hrs · 5,100 cycles

NR 2 ENG OIL LEAK NOTED FROM UNDER THRUST REVERSER COWLS AND UPLIFTED 4.5 QTS. LEAK TRACED TO OIL RETURN PIPE FROM FWD BEARING COMPARTMENT TO SCAVANGE PUMP. PIPE REPLACED IAW MM 79-22-51-000-803-A. ENG RUN C/OUT. NIL LEAKS EVIDENT.

Part: WARNING MESSAGE — ILLUMINATED (BRAKE SYSTEM) · airframe 30,815 hrs · 5,105 cycles

ABORTED TAKEOFF DUE TO RECEIVING A ECAM FOR BRAKES RELEASE AND BRAKE 1 RELEASED MESSAGE AT 90 KNOTS. FOUND NR 1 WHEEL HUB CAP MISSING.

Part: ACTUATOR — DEFECTIVE (FUEL SYSTEM) · airframe 3,507 hrs · 22,212 cycles

FUELERS REPORT HAVING TROUBLE FUELING. LT FUEL OUTER TANK, INLET VALVE ACTUATOR FAULT. RESET FCMC 1 & 2, NO HELP, DOWN POWER A/C, RESET POWER, FCMC 1 & 2 SYS TEST OK. NO FURTHER DEFECTS NOTED DURING CONTINUED FUELING. OK FOR SERVICE. REMOVED & REPLACED LT FUEL OUTER TANK, INLET VALVE ACTUATOR PER AMM 28-25-57-400-801-A. OPS NORMAL. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,340 hrs · 5,026 cycles

ETOPS SIGNIFICANT SYSTEM - DURING CLIMB, STS PAGE DISPLAYED " INOP SYS FUEL AFT XFR" NO ASSOCIATED ECAM, NO FUEL XFR'D FROM INNERS TO TRIM TANK. MAN FWD XFR OK, AUTO FWD XFR OK. FUEL AFT XFR VLV 2 (700QN2),T/S'D PER TSM 28-27-00, PERFORMED FUEL VALVE TEST PER AMM 28-51-00 & AFT XFR VLV 2 OPS CHK'D OK.

Part: UNKNOWN — MALFUNCTIONED (THRUST REVERSER) · airframe 30,192 hrs · 5,007 cycles

ETOPS, AFTER LANDING ECAM ENG 2 REV UNLOCKED, CYCLED NR 2 ENG TR MULTIPLE TIMES ON GROUND. OPS CHECK NORMAL. OK TO CONTINUE PER AMM 78-31-00-740-802A

Part: CONNECTOR — DIRTY (THRUST REVERSER) · airframe 30,192 hrs · 5,007 cycles

ETOPS, ENG 2 REV UNLOCKED. FOUND LOWER OUTBOARD THRUST REVERSER HAD GAP. T/S PER TSM78-30. REMOVE AND REINSTALLED, CLEANED CONNECTOR PER AMM 78-31. CYCLED T/R MULTIPLE TIMES PER AMM 78-31. NO CURRENT FAULTS NOTED. OK TO CONTINUE SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 29,722 hrs · 4,935 cycles

ON DESCENT BTW 7000' & 4000' FUMES WERE SMELT IN CABIN & COCKPIT ODOR WAS DESCRIBED AS OILY SOCK SMELL. ACCOMPLISHED GROUND ENGINE RUN NR 1 ENGINE, SHUTDOWN THEN RAN NR 2 ENGINE WITH PACKS ON ENGINE BLEED ONLY, NO ODOR OR SMELL IN COCKPIT OR CABIN NOTED, OK FOR SERVICE 1 OTHER ODOR REPORT IN 30 DAYS. NO SMELLS REPORTED ON RETURN TO LAX (SAME CABIN CREW, DIFFERENT FLIGHT CREW).

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 29,355 hrs · 4,869 cycles

CAB PRESS SYS 1 FAULT CAUTION. T/S PER TSM 21-31-00-810-803-A. FOUND FWD OUTFLOW VALVE INOP. REMOVED AND INSTALLED FWD OUTFLOW VALVE PER AMM 21-31-51-000-801-A AND 21-31-51-400-801-A. OPS CHECKS GOOD PER AMM 21-31-00-710-801-A AND AMM 21-31-00-710-802-A. A/C OK FOR SERVICE VALVE, OUTFLOW; OFF 33-2132-9-0001 62009 ON 33-2132-9-0001 52015

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 29,044 hrs · 4,829 cycles

EMERGENCY LIGHT STRIP FLIGHT DECK ENTRY IS LOOSE. REPLACED FLIGHT DECK ENTRY AND FIRST CLASS GALLEY EMERGENCY LIGHT STRIP.

Part: LIGHT — BROKEN (CABIN) · airframe 29,033 hrs · 4,827 cycles

EMERGENCY LIGHTING AT FLIGHT DECK ENTRY IS BROKEN. SECURED EMERGENCY LIGHTING.

Part: FWC — FAULTED (NR 1) · airframe 28,090 hrs · 4,659 cycles

FWS FWC 1 FAULT. REPLACED THE NR 1 FWC IAW AMM 31-53-34-400-801-A. BITE TESTED OK IAW AMM 31-50-00-740-801-A. LAND CAT 3 TEST OK IAW AMM 22-97-00-740-801-A.

Part: MODULE — FAILED (NR 2) · airframe 27,483 hrs · 4,559 cycles

NR 2 ENGINE SHUTDOWN, AC BUSS 2 FAULT ON ECAM. REMOVED & REPLACED THE NR 2 ECMU IAW AMM 24-29-34. BITE TEST FAILED NR 1 ECMU ATA 242255 GLC-2(9XU2)/ECMU(1XM1). REMOVED & REPLACED CONTACTOR 9XU2, OPS CHECKED OK IAW AMM 24-22-55-400-803A. ACCOMPLISHED TSM 24-22-00-810-871-A, BITE #1 & #2 ECMU'S PER AMM 24-29-00-740-801-A OK. BITE GAPCU PER AMM 24-41-00-740-801-B OK. BITE LGCU & RGCU IAW AMM 24-41-740-801-B OK. GROUND RAN LT & RT ENGINES, CHECKED AC BUSSES WITH BOTH ENGINES, APU & EXTERNAL POWER ON, POWER TRANSFER NORMAL. OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 26,746 hrs · 4,440 cycles

LEFT ENGINE AFT SIDE - GREEN HYD PUMP IS LEAKING // GREEN SYSTEM EDP REPLACEMENT DETAILS PN 3022053-001, SN G1010196. REMOVED PN 3022053-001, SN G1340336 INSTALLED. EDP REPLACED IAW AMM 29-11-51. REV 53, PUMP, HYDRAULIC OFF 33-2912-9-0002, 10196 ON 33-2912-9-0002 40336.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 26,746 hrs · 4,440 cycles

NR 2 ENGINE GREEN EDP LEAKING. NR 2 ENGINE INT GREEN EDP REPLACED IAW AMM 29-11-51 R53. PUMP, HYDRAULIC OFF 33-2912-9-0002 10200 ON 33-2912-9-0002 30289.

Part: SEAT TRACK — CORRODED (FRAMES 25-38) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C25-38, 2462 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53276428.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C47-53.2, Y450 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53334777 AND ER/A 54-616514.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 26,756 hrs · 4,452 cycles

AFT CARGO DOOR INNER SKIN DAMAGE BETWEEN FRAMES 64-64A. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW SRM 52-32-00, PARA 5.V, FIG 222.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C47-53.2, 450 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5333477 AND ER/A 546165-14.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C47-53.2, -450 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5333477.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C40-47, -1959 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F7112824.

Part: SKIN — DENTED (RT WING SLAT) · airframe 26,756 hrs · 4,452 cycles

DURING H-CHECK, L/E OF RT WING NR 4 SLAT WAS FOUND DENTED. REPAIRED IAW ER/A 543882-14 AND SRM 57-40-00, FIG 202.

Part: LINKAGE — OUT OF ADJUST (R4 DOOR SLIDE) · airframe 26,756 hrs · 4,452 cycles

DURING H-CHECK, R4 DOOR FAILED OPS CHECK OF THE LOCKING MECHANISM. ADJUSTED ESCAPE SLIDE LINKAGES AND SENSOR 36MJ.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C40-47, 1959 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG, F57112819.

Part: CROSSBEAM — CORRODED (FRAME 17) · airframe 26,756 hrs · 4,452 cycles

DURING H-CHECK, CROSSBEAM AT FRAME 17 BETWEEN 1400 -1953 WAS FOUND CORRODED. REPLACED CROSSBEAM IAW SRM 51-72-11 AND DWG F25310722

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FR 53.2-47, 1959 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53312812.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, FLOOR SUPPORT AT FRAME 75, Y0, 52275, FOUND CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND 51-42-11 AND DWG F53478042.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK FRAME 53.6-54, Y-1959 WAS FOUND CORRODED. INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 53-31-15, FIG 201, 51-72-11 AND DWG F53326941.

Part: SEAT TRACK — CORRODED (FRAME 31) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 31, 1953 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53113473.

Part: SEAT TRACK — CORRODED (FRAMES 59-67) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 59-67, -450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5347704006.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME C 40-47, -Y450 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F57112816.

Part: SEAT TRACK — CORRODED (FRAMES 63-71) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 63-71, 1959 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53477040006.

Part: SEAT TRACK — CORRODED · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C40-47, 450 FOUND CORRODED. REPLACED SEAT TRACK SRM 51-72-11 AND DWG F571124362.

Part: SEAT TRACK — CORRODED (FRAMES 25-38) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C25-38, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53276421.

Part: SEAT TRACK — CORRODED (FRAMES 37-39) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C37-39.2, 1959 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG 5331114.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 62-71, 2462 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5347704006.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C47-53.2, 1959 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53312812.

Part: SEAT TRACK — CORRODED · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C47-53.2, Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DWG F53312813.

Part: SEAT TRACK — CORRODED (FRAMES 68-71) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 68-71, -450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5347704006.

Part: SEAT TRACK — CORRODED (FRAMES 55-58) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 55-58, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F534762004.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C 53.2-54, 450 FOUND CORRODED. REPLACED SEAT TRACK SRM 51-72-11 AND DWG F53326973.

Part: SEAT TRACK — CORRODED (FRAMES 55-58) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 55-58, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F5347765004.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C47-53.2, 2462 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53312813.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C53.2-54, 1959 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53326912004.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C 53.2-54, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53326912.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 53.6-54, 1959 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53326941.

Part: SEAT TRACK — CORRODED (FRAMES 25-26) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT C 25-26 AND C 37.4-38, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53276421.

Part: SEAT TRACK — CORRODED (FRAMES 55-58) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 55-58, 1959 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F534762212.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 26,755 hrs · 4,452 cycles

SEAT TRACK FRAMES 62-71, Y1959 HAS AREAS OF CORROSION. CORROSION REMOVED IAW SRM 51-74-00, REV 89. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 89 AND DWGS F5347850 AND F53477040.

Part: SEAT TRACK — CORRODED (FRAMES 59-62) · corrosion level 2 · airframe 26,755 hrs · 4,452 cycles

SEAT TRACK FRAME 59-62 -Y1959 HAS 3X AREAS OF CORROSION AT BS 1.43 0622, 44406 3.45 176 CORROSION REMOVED AT 3 X LOCATIONS IAW RM 51-74-00, REV 89. DAMAGE DIMENSIONS AS FOLLOWS: 1.000" X FULL CROWN WIDTH X 0.030, CROWN SUPERIOR, CROWN LATERAL BOTH SIDES 0.025" REMOVED, 3.0.200" X 0.150" X 0.030" CROWN SUPERIOR. ALL 3 X AREAS OUT OF LIMITS IAW SRM 53-00-15, PARA 4.B, REV 89. DEPTH GAUGE TZA05899, CAL DUE: 02 MAR 17, VERNIERS TWA17491 CAL DUE: 22OCT16. RII OF REMOVED CORROSION CARRIED OUT IAW HAL VOL1, CHAP5. SEAT TRACK FRAME 59-62 -Y1959 REPLACEMENT REQUIRED. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 89 AND DWG F53477650. RII OF NEW SEAT INSTALLATION FRAME 59-62 -Y1959 CARRIED OUT IAW HAL GMM VOL 1, CHAP 5.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 26,755 hrs · 4,452 cycles

SEAT TRACK FRAMES 53.6 - 54, 450 HAS AREAS OF CORROSION. CORROSION REMOVED IAW SRM 51-74-00 REV 89. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 89 AND DWG F53326973.

Part: SEAT TRACK — CORRODED (FRAMES 59-67) · corrosion level 2 · airframe 26,755 hrs · 4,452 cycles

SEAT TRACK FRAMES 59-67, 450 HAS EIGHT AREAS OF CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-15 PARA 4B, REV 89. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 89 AND DWG F53477044000.

Part: SEAT TRACK — CORRODED (FRAMES 59-67) · airframe 26,756 hrs · 4,452 cycles

DURING H1 CHECK, SEAT TRACK AT FRAME 59-67, 450 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53477044000.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 26,601 hrs · 4,416 cycles

ENGINE 1 REVERSER FAULT, ENGINE 1 LP SHAFT PROT LOSS. PERFORMED ENGINE RUN IAW AMM 71-00-501. NO MESSAGES NOTED, NO FAULTS NOTED. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NAV SYS) · airframe 25,935 hrs · 4,309 cycles

NAV IR 3 FAULT IN FLIGHT. IAW TSM 34-10-00-810-940 FWS SYS TEST CARRIED OUT OK IAW AMM 31-50-00-740-801.

Part: LIGHT — MISSING (CABIN) · airframe 25,610 hrs · 4,260 cycles

EMERGENCY LIGHT STRIP MISSING FROM FORWARD GALLEY FLOOR. REPLACED EMERGENCY LIGHT STRIP IN FWD GALLEY IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BEARING — FAILED (MLG WHEEL) · airframe 11,578 hrs · 1,774 cycles

AFTER ARRIVAL, MAINTENANCE DISCOVERED NR 6 MLG WHEEL BEARING FAILURE. AXLE IS DAMAGED.

Part: INDICATOR — SLOW · airframe 24,007 hrs · 3,996 cycles

ATB ISIS STARTED DRIFTING AFTER TAKEOFF VERY SLOW TO LEVEL AFTER A ROLL & PITCH CONTINOUSLY DRIFTED FROM 0 DEGREES TO PLUS 20 DEGREES. REPLACE ISIS GROUND, OPS CHK OK AMM 34-22-25.

Part: INDICATOR — MALFUNCTIONED · airframe 24,007 hrs · 3,996 cycles

ISIS STARTED DRIFTING AFTER TAKEOFF VERY SLOW TO LEVEL AFTER A ROLL & PITCH CONTINOUSLY DRIFTED FROM 0 DEGS TO PLUS 20 DEGS. AIR TURNBACK, REPLACED ISIS GROUND. OPS CHECK OK AMM 34-22-25.

Part: THERMOSTAT — MALFUNCTIONED (FAN AIR VALVE) · airframe 23,903 hrs · 3,979 cycles

AT 30000', ECAN AIR ENGINE BLEED 2 FAULT. PRE-COOLER TEMP AT 225 DEGREES C. UNABLE TO RESTORE. R & R FAN AIR VALVE CONTROL THERMOSTAT ON RT ENG B LEED SYS IAW AMM 36-11-43-400-804A, REACTIVATED HPV ON RT ENG BLD SYS IAW AMM36-11-00-440-812A. BMC 2 BITE TEST OK IAW AMM36-11-00-740-803.

Part: FIRE LOOP — SHORTED (RT NACELLE) · airframe 23,883 hrs · 3,977 cycles

ENGINE 2 FIRE LOOP A FAULT ECAM WARNING DISPLAYED IAW FLIGHT CREW. FOUND RT ENGINE LOOP A PYLON DETECTOR, 6WD2, SHORTED TO GROUND. R & R LOOP A, 6WD2, AMM 26-12-16-400 -808A, ACCOMPLISHED TO STEP 5B, 3. OPS CHECK GOOD. COMPLETED REMAINING STEPS AMM 26-12-16-400-808A.

Part: TIRE — WORN (NLG) · airframe 23,820 hrs · 3,981 cycles

ON TAKEOFF ROLL, EXTREME NOSE WHEEL VIBRATION. T/S IAW TSM 32-20-00-810. FOUND UNEVEN WEAR BETWEEN NLG TIRE ASSY. REPLACED BOTH NLG TIRE ASSY IAW AMM 32-41-12. INSPECTED NLG ASSY FOR IRREGULARITIES. NONE NOTED.

Part: TIRE — WORN (NLG) · airframe 23,821 hrs · 3,981 cycles

DUE TO EXTREME NOSEWHEEL VIBRATION DURING TAKEOFF ROLL. T/S IAW TSM 32-20-00-810, FOUND UNEVEN WEAR BETWEEN NLG TIRE ASSY. REPLACED BOTH NLG TIRE ASSY IAW AMM 32-41-12. INSPECTED NLG ASSY FOR IRREGULARITIES. NONE NOTED.

Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 23,648 hrs · 3,941 cycles

NR 2 ENGINE BLEED ECAM DURING DESCENT. R & R RIGHT ENGINE EXCHANGER OUTLET SENSOR IAW AMM 36-11-17-400-804-A.

Part: BRAKE — OVERHEATED (NR 6) · airframe 23,414 hrs · 3,917 cycles

DURING TAKEOFF ROLL, AROUND 65 KTS ECAM MESSAGE HOT BRAKE, NR 6 BRAKE AT 320 DEGREES. ALL BRAKE TEMPS AROUND 130 DEGREES PRIOR TO TAKEOFF ROLL. VERIFIED WHEEL SPINS FREELY, REPLACED NR 6 TIRE AND BRAKE.

Part: BRAKE — OVERHEATED (NR 6) · airframe 23,357 hrs · 3,895 cycles

DURING TAKEOFF ROLL AROUND 65 KTS, ECAM MESSAGE HOT BRAKE, NR 6 BRAKE AT 320. ALL BRAKE TEMPS AROUND 130 PRIOR TO TAKEOFF ROLL. VERIFIED WHEEL SPINS FREELY. REPLACED NR 6 TIRE AND BRAKE.

Part: INDICATOR — MALFUNCTIONED (AIR SPEED)

ABORTED T/O, F/O AIRSPEED ERROR ABORTED AT 65 KTS. NO AIRSPEED FAULTS ON PFR, ADR2 & IR2 SYSTEM TEST OK IAW AMM 34-13-00 & 34-14-00. HA MOC REPLACED F/O PITOT PROBE IAW AMM 34-11-15, OPS TEST OK. REPLACED ADM-2, 19FP2 AND HOSE IAW AMM 34-11-17. ADR2 SYSTEN TEST OK. LEAK CHECK OF CAPT AND F/O TOTAL PRESSURE LINES, GOOD IAW AMM 34-11-00. FUNCTIONAL TEST OF CAPT & F/O AIRSPEED DATA GOOD IAW AMM 34-13-00. ACCOMPLISHED AFS BITE TEST IAW AMM 22-96-00, TEST OK. LAND 3 CAPABILITY TEST PASSED IAW AMM 22-97-00. OK FOR SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,690 hrs · 3,794 cycles

ENGINE AIR BLEED FAULT ON CLIMBOUT. RESET NR 1 ENGINE BLEED ECAM, CLEARED. R & R NR 1 ENGINE BLEED VALVE, OPS AND LEAK CHECKED OK. OK FOR SERVICE.

Part: BLEED AIR SYS — MALFUNCTIONED (NR 1) · airframe 22,676 hrs · 3,791 cycles

NR 1 ENGINE BLEED AIR FAULT ON CLIMB OUT. RESET ENGINE 1 BLEED IAW MAINTENANCE CONTROL REQUEST. PACK FLOW "LOW" AND FAULT CLEARED. PERFORMED TSM 36-11-00-710-813-A. OPS CHECKED GOOD, NO FAULTS NOTED. ALSO, PERFORMED HIGH POWER RUN, OPS CHECKED GOOD, NO FAULTS NOTED. TESTED OK. OK FOR SERVICE.

Part: BLEED AIR SYS — MALFUNCTIONED (NR 1) · airframe 22,676 hrs · 3,791 cycles

NR 1 ENGINE BLEED AIR FAULT DURING CLIMBOUT. RESET NR 1 ENGINE BLEED IAW MX CONTROL REQUEST. PACK FLOW "LOW" AND FAULT CLEARED. PERFORMED TSM 36-11-00-710-813-A. OPS CHECKED GOOD, NO FAULTS NOTED. ALSO PERFORMED HIGH POWER RUN, OPS CHECKED GOOD, NO FAULTS TEST OK. OK FOR SERVICE.

Part: CYLINDER — FAILED (L1 DOOR SLIDE) · airframe 22,573 hrs · 3,776 cycles

1L DOOR ESCAPE SLIDE/RAFT TEST DEPLOYMENT FAILED. DURING SAMPLING INSPECTION IAW FORECAST 43-0525-8-0040, 1L DOOR FAILED TO OPEN SUFFICIENTLY TO FIRE THE SLIDE. FOUND THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER HAD FAILED INTERNALLY.

Part: SLIDE — LEAKING (EMERGENCY EXIT) · airframe 22,573 hrs · 3,776 cycles

LEFT EMERGENCY DOOR ESCAPE SLIDE FAILED OPS CHECK. SLIDE DID NOT STAY INFLATED FOR 10 MINUTES. SLIDE HAD 1" HOLE IN FWD SIDE. R & R SLIDE.

Part: CYLINDER — FAILED (L1 DOOR SLIDE) · airframe 22,583 hrs · 3,788 cycles

DURING OPS CHECK, DOOR 1L ESCAPE SLIDE FAILED DEPLOYMENT TEST. FOUND THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED INTERNALLY, SO THE SLIDE FAILED TO OPEN SUFFICIENTLY. REPLACED DOOR ACTUATOR AND SLIDE. LP 1939106, 1915911.

Part: SLIDE — DAMAGED (EMERGENCY EXIT) · airframe 22,583 hrs · 3,788 cycles

LEFT EMERGENCY DOOR ESCAPE SLIDE FAILED OPERATIONAL CHECK. SLIDE DID NOT STAY INFLATED FOR 10 MINUTES. FOUND 1" HOLE IN FORWARD SIDE OF SLIDE, SUSPECT PREVIOUS REPAIR FAILED. REPLACED SLIDE. LP 1939117.

Part: VALVE — FAULTED (NR 2) · airframe 22,522 hrs · 3,768 cycles

AIR PACK VALVE 2 FAULT ON CLIMB OUT. POST FLIGHT REPORT SHOWS AIR ENGINE 2 BLEED FAULT PRESSURE REGULATOR V. R & R PRV BLEED VALVE IAW AMM 36-11-52. OPS CHECK NORMAL. OK FOR SERVICE.

Part: VALVE — FAULTED (NR 2 ACM) · airframe 22,532 hrs · 3,780 cycles

RETURNED TO AIRPORT DUE TO AIR PACK VALVE 2 FAULT DURING CLIMB. POST FLIGHT REPORT SHOWS AIR ENG 2 BLEED FAULT PRESSURE REGULATOR MESSAGE. REPLACED PRV BLEED VALVE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 19,967 hrs · 3,358 cycles

IDG NR 2 LOW OIL PRESSURE DISCONNECTED IDG & TURNED OFF GENERATOR NR 2. REMOVED AND INSTALLED NR 2 ENGINE IDG IAW AMM 24-21-51. FOUND IDG FILTER DPI POPPED AND METAL PARTICLES ON FILTER. FILTER ELEMENT WAS NOT DAMAGED AND NO SIGNS OF BYPASS WERE FOUND. OPS CHECKED NORMAL. PERFORMED OPS CHECK OF IDG. DISC SYS CHECKED OK. NO LEAKS NOTED AND OIL LEVEL CHECKS GOOD. OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 19,884 hrs · 3,345 cycles

AFT CARGO DOOR INTERIOR SIDE RIVET HEAD DAMAGED 4PT AFT OF FWD DOOR EDGE 1.5 FEET FROM BOTTOM DOOR EDGE. BETWEEN FRAME 62 AND FRAME 62A BEAMS. REPAIRED IAW E105-381000. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU OIL) · airframe 19,874 hrs · 3,343 cycles

DURING CRUISE FLT, RECEIVED ECAS ELEC CIRCUIT BREAKER TRIPPED. BITE TEST APU, NO FAULTS. RESET OIL/SERVICE CIRCUIT BREAKER. FUCTIONAL CHECKED OF APU OK. LEAK TEST OF APU OIL HEATER OK. NO LEAKS. OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (APU) · airframe 19,874 hrs · 3,343 cycles

DURING CRUISE, RECEIVED ECAM ELEC CIRCUIT BREAKER TRIPPED AND CIRCUIT BREAKER PAGE MESSAGE APU 5000VU. BITE TEST APU. NO FAULTS. RESET OIL SERVICE CIRCUIT BREAKER. FUNCTIONAL CHECKED OK. LEAK TEST OF APU OIL HEATER OK. NO LEAKS. OK FOR SERVICE.

Part: JETTISON SYSTEM — MALFUNCTIONED · airframe 18,947 hrs · 3,188 cycles

ACFT DIVERTED DUE TO FUEL JETTISON NOT CLOSED, X4, LT TANK FUEL JETTISON VALVE. SHOWED OPENED.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,951 hrs · 45,504 cycles

APPROX 1.5 HRS INTO THE FLIGHT, ECAM MESSAGE A ICE RT WINDSHIELD HEAT. SIMULTANTOUSLLY WITH APPEARENT SHORT OF RT WINDSHIELD, BLACK MARK WITH DELAMINATING LAYER BELOW. R & R F/O WINDSHIELD IAW AMM 30-42-34, OPS CHECKED GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,951 hrs · 45,504 cycles

APPROXIMATELY 1.5 HRS INTO THE FLT ECAM MESSAGE A. "ICE RT WINDSHIELD HEAT". SIMULTANEOUSLY WITH APPEARENT SHORT OF RT WINDSHIELD, BLACK MARK WITH DELAMINATION LAYER BELOW. R & R F/O WINDSHIELD IAW AMM 30-42-34, OPS CHECKED GOOD.

Part: ADIRU — MALFUNCTIONED · airframe 13,832 hrs · 2,387 cycles

AT APPROX 95 KTS DURING TAKEOFF ROLL. F/O AIRSPEED INDICATOR TAPE LOST SPEED INDEXES AND BEGAN FLASHING RED. MOVED NR 3 ADIRU INTO NR 2 POSITION AND REPLACED NR 3 ADIRU. OPS AND LEAK CHECKED GOOD.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 13,695 hrs · 2,367 cycles

CAPTAINS AIR SPEED INOPERATIVE RTO -80 KTS. ON ARRIVAL AT GATE PFR SHOWED NO FAULTS. ADR-1, SYS TESTS OK, NO FAULTS IAW AMM 34-13-00. AFS BITE TEST FAULTS FMGEC-1 AND FMGEC-2 RESET BOTH FMGEC, AFS BITE TEST OK IAW AMM22-96-00. INSPECTED PITOT PROBE 1, NO DEFECTS OR BLOCKAGE. INSPECTED ADM-1 FOR CONNECTOR SECURITY CHECKED OK. FLUSHED PITOT-1 PRESSURE LINE IAW AMM 34-11-00, AMM 34-13-00. PENDING HIGH SPEED TAXI CHECK. PERFORMED 2 HIGH SPEED TAXI CHECKS. OPS CHECKED GOOD NO DEFECTS NOTED, OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 8,349 hrs · 1,567 cycles

SMOKE, FWD & AFT BOTTLE FAULT 1 & 2 WARNING LIGHTS. PERFORMED MCDU TEST IAW AMM 26-10, SYS TESTED OK. MESSAGE CLEARED.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 7,573 hrs · 1,430 cycles

SMOKE AFT CARGO BOTTLE 1(2) FAULT CARGO AFT CARGO DETECT FAULT 1(2) DISPLAY ECAM. RESET SDF1 AND SDF2 IAW SUPPLEMENTAL MANUAL. NO FAULTS NOTED. OK TO CONTINUE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 6,842 hrs · 1,299 cycles

FWD & AFT CARGO SMOKE BOTTLES 1 & 2 FAULT DURING PREFLIGHT. PERFORMED CARGO SMOKE TEST IAW AMM 26-16-00, NO FAULTS NOTED.

Part: UNKNOWN — UNKNOWN · airframe 5,813 hrs · 1,111 cycles

ETOPS SIGNIFICANT SYS - BTB -NR 2 ENGINE OVERSPEED PROTECTION LOST. ENGINE NR2 LP SHAFT PROTECTION LOST. ACCOMPLISHED FIM 73-21-89. NO FAULTS NOTED. ACFT OK FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 5,042 hrs · 968 cycles

ETOPS SIGNIFICANT SYS - SMOKE FWD/AFT CARGO BTL1 FAULT, SMOKE FWD/AFT CRG BTL2 FAULT, SMOKE BULK DET FAULT, SMOKE BULK REST FAULT, SMOKE BULK REST DET FAULT, SMOKE BAND DET FAULT DISPLAYED. RESET SDF 1 & 2. MESSAGES CLEARED. SMOKE DETECT SYS TEST OK. NO DEFECTS NOTED.

Part: IRU — MALFUNCTIONED (NR 3) · airframe 4,872 hrs · 938 cycles

ETOPS SIGNIFICANT SYS - NR3 INERTIAL REF, ALTHOUGH RE-ALIGNED TWICE, FAULT LIGHT CONTINUOUSLY FLASHES. RE-RACKED & RE-ALINGED NR3 IRU, GND CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 BLEED SYS) · airframe 4,856 hrs · 935 cycles

ETOPS SIGNIFICANT SYS - BTB - ENG 2 BLEED FAULT ECAM MESSAGE, CAME ON SHORTLY AFTER ENG START. PERFORMED FIM 36-11-81, BMC 2 BITE CHECKED, NO FAULTS FOUND, RAN ENGINES, NO FAULTS FOUND, SWAPPED NR 1 & NR 2 PACK CONTROLLERS IAW AMM 21-51-00. OPS CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,810 hrs · 928 cycles

ECAM MEMO ALERT APPEARED AT TOP OF DESCENT SMOKE FWD CARGO BLT 1 FAULT, AFT CARGO BLT 1 FAULT, FWD CARGO BLT 2 FAULT AFT CARGO BLT 2 FAULT, THE MESSAGE CLEARED ABOUT 10 MIN LATER. PERFORMED A FWC BITE NO FAULTS FOUND, INFO NOTED. RECORDED MESSAGE REAPPEARED. PERFORMED A FWC AND SDAC RESET. CHECKED OK IAW AMM BITE 26-10-00.

Part: SMOKE WARNING — FALSE ACTIVATION · airframe 4,810 hrs · 928 cycles

ACM MEMO ALERT APPEARED AT TOP OF DESCENT, SMOKE FWD CARGO BLT 1 FAULT, AFT CARGO BLT 1 FAULT, FWD CARGO BLT 2 FAULT, AFT CARGO BLT 2 FAULT, THE MESSAGE CLEARED ABOUT 10 MIN LATER. PERFORMED A FWC BITE, NO FAULTS FOUND, INFO NOTED. RECORDED MSG REAPPEARED. PERFORMED A FWC AND SDAC RESET. CKS OK IAW AMM BITE 26-10-00.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,265 hrs · 826 cycles

SMOKE FWD CARGO BLT FAULT "AFT" "FWD" "2" AFT. RESET SDF 1 AND SDF 2 PERFORMED SDF TEST, TEST PASS, NO FAULT NOTED. OK FOR SERVICE.

Part: DECODER — MALFUNCTIONED (ICE PROTECTION) · airframe 4,254 hrs · 824 cycles

SLIDE ICE PROTECTION NO DATA AVAILABLE AT DOOR L1, 1R, AND 2R MSG ON FWD FAP. CIDS GROUND SCANNING FAULT IPCU FWD 14DS DEU B 300 RT 4. R & R DEU B300RH4 IAW AMM 23-73-47. BITE OK. FAP MSG CLEARED. OK FOR SVC.

Part: ADIRU — INOPERATIVE · airframe 4,218 hrs · 817 cycles

ETOPS SIGNIFICANT SYS - ATB - ON T/O RUN, ABOVE 100 KTS, CAPT'S IAS WENT ROD/INOP/UNRELIABLE. TRANSFERED CONTROL. BOTH F/O & ISIS ACCURATE. CAPTS ALTIMETER OK CHANGED AIRDATA TO "CAPT ON 3" - DISPLAY OK. OK TO CONT IAW MEL 34-10-1B. PLACARDED AND ENTERED ON LIDS. DMI 41137 T/S FOUND NR1 ADIRU INOP. SWAPPED NR1 AND NR2 ADIRU. PLACARDED NR2 ADIRU INOP. NR1 ADIRU GROUND OPS CHECK OK IAW AMM 34-12-34. OPEN

Part: SKIN — DAMAGED (BS 18698-19228) · airframe 4,217 hrs · 816 cycles

SUB-FOUND DAMAGE ON LT FUSELAGE BETWEEN STA 18698 AND 19228, AND BETWEEN STRINGER 28 AND 30. BLENDED UPPER AND LOWER GOUGED AREA. UPPER AT .040 MATERIAL REMAINING. LOWER AT 0.062 REMAINING UPPER BLEND 1.2500" W X .7500"H LOWER BLEND 1" W X .7500". HFEC OF FUSELAGE SKIN - NO CRACKS IND,TOTAL DENT TO LIDS. W X 10"H DEPTH TOTAL=0.307. DRILLED OUT RIVETS FROM EFFECTED AREA AND REMOVED DAMAGED SECTION OF STRINGER 27 IAW SRM 53-00-13, CUTOUT DAMAGED SKIN IAW SRM 53-00-11. FABRICATED DOUBLER AND TRANSFERRED DRILL HOLES IAW SRM 53-00-11. HFEC CK AROUND DAMAGE CUT OUT AREA. FABRIATED FILLER FROM 2024T-3.063. MATERIAL VERIFICATION DOUBLER 2024T-3 0.071. HOLES THRU STRINGER PENDING. COUNTERSUNK HOLES FOR 1097- 6. FABRICATED DOUBLER FILLER STRINGER, SPLICE, OK TO INSTALL. ACCOMPLISH HFEC AROUND DAMAGE CUTOUT AREA, NO CRACK INDICATION. REPAIRED FUSELAGE IAW SRM 53-00-11, FIG 224 AND STRINGER IAW SRM 53-00-13, FIG 201. IAW SRI 53-00-11 ACFT NEEDS PERFORM AN ULTRA SONIC EDDY CURRENT INSP, ITEM DEFER IAW MON. NEED EDDY CURRENT INSP BFR 11500 F/C, ITEM TRANSFERRED TO LIDS.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 4,218 hrs · 817 cycles

ABORTED T/O BELOW 100 KTS, LOSS OF CAPT'S IAS. VISUALLY INSPECTED PITOT PROBE FROM FRONT OF TUBE, NOTHING OBVIOUS FOUND. PRESSURIZED 2 OUT OF 3 PITOT SYS AT THE SAME TIME. TRIED SEVERAL DIFFERENT COMBINATIONS AND DIFFERENT SWITCH SELECTIONS IN COCKPIT. NO MATTER WHAT SELECTION WAS MADE, WHENEVER CAPT READING NR 1 PITOT INFORMATION, CAPT AIRSPEED MUCH SLOWER THAN F/O, UP TO 30 KTS DIFFERENCE. REMOVED NR 2 ADM AND INSTALLED NR 1 POSITION IAW AMM 34-11-17. PERFORMED INSPECTION/CHECK OF CAPT PITOT IAW AMM 34-11-15-200-801-A. TUBE CLEARED USING COMPRESSED AIR. PRESSURIZED ALL 3 PITOT SYSTEMS AND ALL AIRSPEEDS EXACTLY THE SAME. ACFT CONSIDERED SERVICEABLE.

Part: SKIN — DAMAGED (BS 18698-19228) · airframe 4,217 hrs · 816 cycles

FOUND DAMAGE ON LT FUSELAGE BETWEEN STA 18698 AND 19228, AND BETWEEN STRINGER 28 AND 30. BLENDED UPPER AND LOWER GOUGED AREA. UPPER AT .040 MATERIAL REMAINING. LOWER AT 0.062 REMAINING UPPER BLEND 1.2500" W X .7500" H LOWER BLEND 1" W X .7500". HFEC OF FUSELAGE SKIN - NO CRACKS INDICATED, TOTAL DENT TO LIDS. W X 10"H DEPTH TOTAL=0.307. DRILLED OUT RIVETS FROM EFFECTED AREA AND REMOVED DAMAGED SECTION OF STRINGER 27 IAW SRM 53-00-13, CUTOUT DAMAGED SKIN IAW SRM53-00-11. FABRICATED DOUBLER AND TRANSFERRED DRILL HOLES IAW SRM 53-00-11. HFEC CK AROUND DAMAGE CUT OUT AREA. FABRICATED FILLER FROM 2024T-3.063. MATERIAL VERIFICATION DOUBLER 2024T-3 0.071. HOLES THRU STRINGER PENDING. COUNTERSUNK HOLES FOR 1097-6. FABRICATED DOUBLER FILLER STRINGER, SPLICE, OK TO INSTALL. ACCOMPLISH HFEC AROUND DAMAGE CUTOUT AREA, NO CRACK INDICATION. REPAIRED FUSELAGE IAW SRM 53-00-11, FIG 224 AND STRINGER IAW SRM 53-00-13, FIG 201. IAW SRI 53-00-11 ACFT NEEDS PERFORM AN ULTRA SONIC EDDY CURRENT INSP. ITEM DEFER IAW MON. NEED EDDY CURRENT INSP BFR 11500 F/C, ITEM TRANSFERRED TO LIDS.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHTS) · airframe 4,180 hrs · 809 cycles

AFTER START EMERGENCY LIGHTS SIGN ON AND FLASHING CYCLED EMERGENCY LIGHTS NO CHANGE. FOUND MOISTURE AND LITE CORROSION AT CONNECTOR PLUG LOCATED AT 5158VC CLEANED AND RESECURED IAW AWM 33-51-05 AND AMM 33-31. OPS CK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 3,940 hrs · 763 cycles

PERFORMED OPS TEST OF EMERGENCY POWER SUPPLY UNIT, FORECAST 43-0533-8-0001. FOUND 4L DOOR POWER SUPPLY BATTERY INOP. R & R DOOR 4L 300R7 POWER SUPPLY IAW AMM 33-57-38,OPS CK NORMAL, OK FOR SERVICE.

Part: IDG — FAULTY (NR 2) · airframe 1,633 hrs · 325 cycles

ETOPS SIGNIFICANT SYSTEM - ATB: FLIGHT ELECTRIC IDG 2 OIL LO PR ECAM. REMOVED AND REPLACED NR 2 IDG ASSY PER AMM 24-21-51. OPS AND LEAK CHECKS OK.

Part: WARNING LIGHT — ILLUMINATED (FUEL SYSTEM) · airframe 1,601 hrs · 319 cycles

ETOPS SIGNIFICANT SYSTEM - APROX 3+15 INTO FLT ECAM STATED CTR TO INR: MAN ONLY PLUS INOP SYS - "FUEL AFT XFR" ANNUNCIATED. CTR TANK 0 QTY, ALL TAIL TANK FUEL XFR TO INNER WING TANKS UNTIL CTR TANK EMPTY. PERFORMED TSM TASK 28-26-00-810-801. SYSTEM TESTS ON FCMC 1 AND FCMC 2 OK. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (FUEL) · airframe 33,825 hrs · 6,408 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE FUEL CENTER TO INNER FAULT APPROX AT ATTEMPTED TRIM TANK TRANSFER. MESSAGE DISAPPEARED AFTER 2 MIN. PERFORMED AMM 28-51-00-740-801. NO FUEL CENTER TO INNER FAULT MESSAGE FOUND. OK FOR SERVICE.

Part: FCU — FAILED (APU) · airframe 1,225 hrs · 247 cycles

ETOPS SIGNIFICANT SYS - UNSUCCESSFUL INFLT APU START. REPAIRED CLASS 1 FCU FLOW DIVIDER. BITE CHECK AND CLASS 1 FAULT CLEARED.

Part: COMPUTER — FAULTED (FLT CONTROLS) · airframe 588 hrs · 121 cycles

ETOPS SIGNIFICANT SYS - BTB - F/CTL AIL SERVO FAULT. REPLACED FCPC1 IAW 27-93-400-801, PG 400, ALL INDICATIONS NORMAL, ACFT OK FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (FLT CONTROL) · airframe 598 hrs · 123 cycles

ETOPS SIGNIFICANT SYS - BTB - ECAM (AMBER) WARNING - FLT CONTROL AIL FAULT LIGHT. CHECKED SV SIGNAL WIRING FROM FCPC1 AD/12J, 12K TO SERVO CTL (8CS1) A /E,F AND SV CTL WIRING FROM FCPC-1 AD/12G, 12H TO AB/1J, 1K CONTINUITY CHECKS GOOD, NO SHORTS TO GND. SHAKE CHECK WIRING AT SERVO CTL (8CS1) PLUG AND AT TERM BLOCK 1203VT17, NO DEFECTS NOTED. DUE TO HISTORY R & R FCPC1 IAW AMM.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (GREEN SYS) · airframe 402 hrs · 83 cycles

ETOPS SIGNIFICANT SYSTEM - ATB - AFTER T/O GREEN HYD PRESS 'O'. GREEN HYD SYS QTY NORMAL. DUMPED FUEL BELOW MAX LANDING WT AND RETURNED TO DEPARTURE AIRPORT. REPLACED GREEN HYD RESERVOIR LOW LEVEL SWITCH PER AMM 29-31-12-000-801-0. REPLACED HSMU PER AMM 29-11-34-000-801-0 GROUND TEST OK.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 401 hrs · 82 cycles

ETOPS SIGNIFICANT SYSTEM - ATB - GREEN HYD SYS ECAM SHOWS LOW QTY. ACCOMPLISHED TSM 29-11-00-810-832 STEP 4, A, (1), (A), 1, A IAW DELTA TECH SVC. FOUND NO FAULTS, CONTINUITY OF 0.8 OHM & NO SHORTS TO GROUND. G RSVR LO LVL SW 10JS1 HAS A SHORT OF 2.5K OHM FROM PIN A TO THE CASE. CONTINUITY CHECK OK & NO SHORTS TO GND OF WIRING FROM SDACS TO HSMU TO SW 10JS1. SDAC'S INSTALLED & TEST OK IAW AMM 31-55-34-400-801. ECAM G HYD SYS QTY, CHECK OK. REPLACED GREEN HYD. RESERVOIR LOW LEVEL SWITCH IAW AMM 29-31-12-000-801-0. REPLACED GREEN HYD. RESERVOIR LOW LEVEL SWITCH IAW AMM 29-31-12-000-801-0, REPLACED HSMU IAW AMM 29-11-34-000-801-0, GROUND TEST OK.

Part: PUMP — MALFUNCTIONED (RT ENGINE) · airframe 70 hrs · 14 cycles

ETOPS SIGNIFICANT SYSTEM - DURING CLIMB PWR SET, RT ENG OIL PRES LT ILLUMINATED WITH MASTER WARNING. REDUCING THRUST TO LWR THRUST SETTING INCR OIL PRESS IN GREEN, KEPT ENG RUNNING AT REDUCED THRUST FOR NORMAL LANDING. REMOVED RT ENG OIL PUMP AND FILTER HOUSING PER AMM-79-22-51. C/B K49, Q74 PULLED AND COLLARDED. INSTALLED NEW ENG OIL PUMP AND FILTER HOUSING ASSY PER AMM 79-22-51. OK FOR SERVICE.