N396HA

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON WEB LOCATION Y2462 AT FR17. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

SEAT TRACK ADAPTER CORRODED AT -YB. TRACK WAS REPLACED.

Part: FILLER — CORRODED (ZONE 100)

AIRCRAFT REG: N396HA, AIRCRAFT MSN 1488. BULK CARGO DOOR ENTRANCE CUTOUT LOWER EDGE FILLER FOUND WITH 4 OFF LOCATION CORRODED. MEASURING 30X15MM, 25X10MM,20X20MM AND 10X10MM.

Part: WEB — CORRODED (ZONE 200)

CORROSION FOUND ON WEB LOCATION Y2462 AT FR17. WEB REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y953 BETWEEN FR11 TO FR18. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND BELOW SEAT TRACK CROWN LOCATION Y1552.5 BETWEEN FR31 TO FR35. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR53.3 TO FR53.4. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND BELOW SEAT TRACK CROWN LOCATION Y1522.5 AT FR33. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR53.3 TO FR53.4. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND BELOW SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR26 TO FR37.4. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y450 BETWEEN FR59 TO FR60. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR40 TO FR47. SEAT TRACK REPLACED

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND BELOW SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR47 TO FR53.2. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y1450 BETWEEN FR47 TO FR53.2. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y1959 BETWEEN FR26 TO FR37.4. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y450 BETWEEN FR26 TO FR37.4. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200)

CORROSION FOUND ON SEAT TRACK CROWN LOCATION Y450 BETWEEN FR26 TO FR37.4. SEAT TRACK REPLACED.

Part: APU — SHUTDOWN (ZONE 100) · airframe 47,467 hrs · 7,538 cycles

ETOPS - APU AUTO SHUTDOWN. PER ENGINEERING REMOVED AND REPLACED FLOW DIVIDER ASSY PER AMM 49-31-51. LEAK CHECK OK, CONDITION SAME. REINSTALLED ORIGINAL FLOW DIVIDER. REMOVED AND REPLACED APU PER T/C 330-49-HWI-02. OPS/LEAK CHECK GOOD. OK FOR SVC.

Part: UNION — BROKEN (APU DRAIN LINE) · airframe 47,294 hrs · 7,510 cycles

ETOPS - FOUND APU DRAIN LINE UNION NUT BROKEN. REMOVED AND REPLACED APU DRAIN LINE UNION NUT PER AMM 49-17-00, RUN APU FOR 5 MINS. NO LEAK NOTED. A/C OK FOR SVC.

Part: SENSOR — FAILED (APU) · airframe 47,088 hrs · 7,478 cycles

ETOPS - APU AUTO SHUTDOWN. PERFORMED WIRING CHECKS OF SPEED SENSORS 59KV56 AND 59KV57 PER TSM 49-62-00-810-805-A. 59KV26 CONTINUITY GOOD. NO SHORTS TO GND. 59KV57 INTERMITTENT CONTINUITY WHEN TAPPING BEHIND SENSOR CONNECTOR. NO SHORTS TO GROUND. FOUND SPEED SENSOR 2 (59KV27) STRAP BROKEN. REMOVED AND REPLACED SPEED SENSOR PER AMM 49-71-13. INSTALLED NEW SPEED SENSOR AND STRAP PER AMM 49-71-13 UPTO STEP 4 B(5). RETERMINATED 59KV27 PLUG PIN 1,2,3, PER CMM 49-25-95 AND 49-14-01. CONNECTED PLUG TO SPEED SENSOR PER AMM 49-71-13 STEP 4 B (6) (7). ACCOMPLISHED REMAINING STEPS OF AMM 49-71-13-400-801-A. OPS CHECK GOOD. NO FAULTS NOTED. OK FOR SERVICE.

Part: INSERT — DAMAGED (APU PROBE) · airframe 47,036 hrs · 7,470 cycles

ETOPS - APU FAULT UPON APU START. REMOVED AND REPLACED ECB AND CONDITION SAME. RE-INSTALLED THE ORIGINAL ECB PER AMM 49-71-04. REMOVED/REPLACED IGV ACTUATOR PER AMM 49-23-51. UPON REPLACEMENT OF IGV ACTUATOR, FOUND PNEUMATIC LINE TO THE TOTAL PRESSURE PROBE LOOSE. FOUND TOTAL PRESSURE PROBE UNSECURED (MISSING INSERT) FROM MOUNT. REMOVED AND REPLACED MOUNTING INSERT FOR TOTAL PRESSURE PROBE PER AMM 49-51-14. OPS/LEAK/SECURITY CHECK GOOD. REMOVED/REPLACED "A" AND "B" IGNITOR PLUGS PER AMM 49-41-41. OPS CHECK GOOD. OK FOR SVC.

Part: FUEL CONTROL — FAULTED (APU) · airframe 47,004 hrs · 7,462 cycles

ETOPS - APU AUTO SHUTDOWN @ 80%. REMOVED & REPLACED APU FUEL CONT UNIT IAW AMM 49-32-51-000/400-801A. BLEED/LEAK /OPS CHECK GOOD. OK FOR SVC

Part: OIL SYSTEM — LEAKING (APU GENERATOR) · airframe 46,514 hrs · 7,377 cycles

ETOPS - DURING PREFLIGHT WHOLE ENTIRE AIRCRAFT SMELLS BAD (SMELLS LIKE ROTTEN RUBBISH) AS TIME PROGRESS TENDS TO GET BETTER. PERFORMED TSM 05-05-00-810-829-A. NARROWED FROM APU. UPON FURTHER INSPECTION OF APU, FOUND OIL LEAKING FROM APU GEN. OIL WAS FOUND ON APU BLEED VALVE AND "V" BAND OF BLEED DUCTING. CLEANED "V" BANDS, APU DUCTING, AND BLEED VALVE OF OIL. REMOVED/REPLACED SHAFT SEAL, SEAL PLATE, & PACKING PER AMM 24-23-51. OPS/LEAK CHECK GOOD. PERFORMED LEVEL "A" DECON PER AMM 21-00-00-615-809-A. ODOR STILL LINGERING IN MAIN ENTRY, MID CABIN, AND COCKPIT. FOUND OIL LEAKING FROM FUEL DRAIN LINE. REMOVED & REPLACED FCU PERAMM 49-32-51. OPS & LEAK CHECK GOOD. PERFORMED LEVEL B MANUAL DECONTAMINATION OF ECS PER AMM 21-00-00-615-810-A. SMELL CHECK GOOD. OK FOR SVC.

Part: IGNITER — FAULTED (APU) · airframe 46,465 hrs · 7,369 cycles

ETOPS - APU FAULT ON TAXI INTO GATE. APU AUTO SHUTDOWN. BITE TEST SHOWS CLASS 2 IGN PLUG/ IGN EXCITER MESSAGE, REMOVE AND REPLACE BOTH APU IGN PLUG PER AMM 49-41-41/201 & OPS CHECK GOOD, CYCLED 4 TIMES WITH NO DEFECTS NOTED, BITE TEST OK, NO MESSAGES DISPLAYED. A/C OK FOR SERVICE

Part: LATCH — MISSING · airframe 46,330 hrs · 7,345 cycles

ETOPS - DURING PDSC FOUND MISSING XZ-SINGLE LATCH 19. REMOVED AND INSTALLED XZ SINGLE LATCH 19 PER AMM 25-51-25. OPS CHECK GOOD. OKAY FOR SERVICE.

Part: FUEL LINE — LEAKING (NR 2 ENGINE) · airframe 46,254 hrs · 7,334 cycles

ETOPS - DURING WALK AROUND, FOUND FUEL LEAK COMING FROM #2 ENG STATOR VANE CONTROLLER FUEL LINE. PN: FK12075, LOW PRESSURE RETURN LINE (CHAFFING). REMOVED AND REPLACED LOW PRESSURE RETURN LINE ON #2 ENG VSV CONTROL UNIT. PN: FK12075. REF AMM 75-33-51. LEAK AND OPS CHECK GOOD. OK FOR SVC

Part: TRANSDUCER — MALFUNCTIONED (ENG VIBRATION) · airframe 45,234 hrs · 7,181 cycles

ETOPS - INFO TO MAINT DURING CRUISE ENG 1 N1 VIB FLUCTUATES BETWEEN 2.1-3.1. PERFORMED TSM 77-00-00-810-814-A. EXAMINED ENG#1 LP COMPRESSOR BLADES, ANNULUS FILLERS, SPINNER. NO DEFECTS NOTED. PERFORM ENG #1 HPR AND VIB SURVEY PER AMM 77-00-00-700-838-A. N1 VIBS AT 1.8, EPR AT 1.54. PER ENGINEERING. REMOVED TRIM BALANCE BOLTS 2,3,4,5,6 AND INSTALL 7,8,9 PER AMM 71-00-00. REMOVED AND REPLACED ENG. #1 VIBRATION TRANSDUCER PER AMM 77-32-11. PERFORMED TEST NO. 11 ENGINE VIBRATION PER AMM 71-00-00-700-803-A. N1 VIBE 1.2. OK FOR SERVICE.

Part: FADEC — FAULTED (NR 2 ENGINE) · airframe 45,182 hrs · 7,173 cycles

"ETOPS - BTB ENG 2 FADEC SYS FAULT. PFR INDICATED N2 COMPRESSOR SPEED PROBES (E2-4089KS1 + 3) FAULT. PERFORMED RESISTANCE CHECK FROM OPU 2 CONNECTOR PIN 6-7 & OPU CONNECTOR PIN 12-13. OHMS READ 11.5 & 10.6 RESPECTFULLY. RESISTANCE WITHIN LIMITS PER TSM 77-11-00-810-910-A. AVICONICS PERFORMED WIRE SHAKE DOWN WITH NO FINDINGS. REMOVED AND REPLACED ENG 2 OPU PER AMM 73-21-36. FADEC BITE TEST OK. IDLE ENGINE RUN OK. NO FAULTS OK FOR SVC. "

Part: ACTUATOR — FAULTED (ZONE 100) · airframe 45,115 hrs · 7,163 cycles

ETOPS - ECAM: TRIM TANK TRANSFER FAULT. FOUND FUEL OUTER TK INLET VALVE 2 FAILED. REMOVED AND REPLACED OUTER TANK FUEL INLET-VALVE ACTUATOR PER AMM 28-25-57. OPS CHECK GOOD. OK FOR SVC.

Part: ANTENNA — FAULTED (WX RADAR) · airframe 44,823 hrs · 7,120 cycles

ETOPS - NAV PRED W/S DET FAULT ON SYS 1. WXR ANT MSG ON NAV DISPLAY. REMOVED AND REPLACED XMTR WEATHER RADAR #1 RECEIVER PER 34-41-51. ALSO REPLACED DRIVE UNIT WEATHER RADAR ANTENNA PER 34-41-11. BITE TEST ALL PASSED. NO FAULTS NOTED. OK FOR SERVICE.

Part: COVER — BROKEN (ZONE 200) · airframe 44,250 hrs · 7,029 cycles

4L DOOR EMERGENCY EXIT LIGHT SIGN INOP. REPLACED BROKEN EMERGENCY EXIT LIGHT COVER. COND / SECURITY / OPS CHK OK.

Part: CONTROL UNIT — FAULTED (VSV) · airframe 44,215 hrs · 7,022 cycles

ETOPS - PERFORMED TEST OF THE VSV SYSTEM PER AMM 75-33-00-740-80LA. TEST FAILED. PERFORMED ENG#2 RUN. FAULT CONFIRMED. ENG 2 CTL. SYS FAULT" BLUE TO DO MSG" SHUT ENG DOWN". FURTHER T/S REQ. REMOVED AND REPLACED VSV CONTROL UNIT, PER AMM 75-33-51, UP TO STEPS. 4.(E). LEAK CHECK GOOD. A/C OK FOR SERVICE.

Part: COMPUTER — FAULTED (NR 1) · airframe 44,090 hrs · 7,006 cycles

ETOPS - DURING PDSC "FCMC 1 FAULT". REMOVED AND REPLACED FCMC 1 PER TSM 28-51-00-810-801-A. NO FAULTS NOTED.

Part: BATTERY — FAULTED (ZONE 200) · airframe 44,090 hrs · 7,006 cycles

EMERGENCY LIGHTS CAME ON DURING FLIGHT. WE RESET LIGHTS. EMERGENCY LIGHTS CAME ON AGAIN AT 1000' ( LEFT SIDE ONLY). REMOVED & REPLACED BATTERY AT 15WL &18WL. PER AMM 33-51-38 OPERATIONAL CHECK OK.

Part: SKIN — DAMAGED (ZONE 500 SLAT) · airframe 44,014 hrs · 6,994 cycles

LH WING #7 SLAT (Z517) DAMAGED

Part: FUEL FILTER — CLOGGED (LT ENGINE) · airframe 4,409 hrs · 6,993 cycles

ETOPS - ECAM FUEL FILTER CLOG. REMOVED AND REPLACED L/H ENG FUEL FILTER PER TSM 73-21-79-810-803-A. OP SCHECK GOOD. OK FOR FURTHER SVC.

Part: FUEL FILTER — CLOGGED (NR 1 ENGINE) · airframe 43,929 hrs · 6,980 cycles

ETOPS - ENG 1 FUEL FILTER CLOG IN CRUISE. REMOVED AND REPLACED ENG 1 FUEL FILTER PER TSM 73-21-76-810-803-A, PERFOMED ENGINE RUN. NO DEFECTS NOTED. OK FOR SVC.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 43,511 hrs · 6,915 cycles

ETOPS - ENG 1 "EPR MODE FAULT" DISPLAYED ON DESCENT. PERFORMED TSM 73-21-00-200-804-A FOUND NO DEFECTS ON P50 AIR TUBES. REMOVED AND REPLACED P50 EEC LINE RAN ENGINE NO FAULTS FOUND. BITE TEST OF EEC OK. PERFORMED AIRFLOW & PRESSURE CECK OF ENG #1 P20 & P50 AIR TUBES ANDFOUND NO FAULTS PER AMM 73-21-00-200-802-A & 73-21-80-200-804-A. PERFORMED TSM 73-21-71-810-934-A. INSPECTION, RESISTANCE CHCKS GOOD. NO SHORTS. COMPLETED UP TO SECTION 4.A. PER ENGINEERING, REMOVED & REPLACED EIVMU 1 PER AMM 73-25-34. BITE TEST OK. 08/28/2024 19194. ENGINE IDLE RUN GOOD. NO DEFECT NOTED. FUNCTIONAL CHECK FLIGHT FOR ENG 1 MODE EPR FAULT COMPLETED SATISFACTORILY. NO FAULTS NOTED.

Part: EPR SYSTEM — MALFUNCTIONED (NR 1 ENGINE) · airframe 43,511 hrs · 6,915 cycles

ENG CTL - RTO. ENGINE 1 EPR WAS SLOW TO INCREASE AND DID NOT REACH TAKE OFF THRUST.RTO INITIATED BELOW 100 KIAS BRAKE TEMP SLOWLY INCREASE TO APPROX.400C. FOUND MOISTURE AND LOOSE CONNECTOR ON P50 LINE .REMOVED MOISTURE .RETIGHTEN/RE TORQUED PER A330 TSM 71-00-81-810-801-A. ENGINE 1 & 2 OPERATED AS PER AMM 71-00-00-860-810-A. ENGINE 1 RAN ABOVE IDLE AND EPR INCREASE TO SELECTED THROTTLE POSITION, NO FAULT OBSERVED. ENGINE 2 RAN ABOVE IDLE TO COMPARE EPR INDICATIONS TO ENGINE 1, SAME RESULT, NO FAULTS.

Part: EEC — FAULTED (NR 1 ENGINE) · airframe 43,501 hrs · 6,913 cycles

ETOPS - ENG 1 EPR MODE FAULT. REMOVED + REPLACED ENG 1 EEC PER A330 AMM 73-21-34. ALL OPS CHECKS GOOD. A/C OK FOR SERVICE

Part: DRAIN MAST — LEAKING (APU) · airframe 42,789 hrs · 6,802 cycles

ETOPS - APU DRAIN MAST ( FWD ) LEAKING FUEL / SURGE VALVE. REMOVED AND REPLACED APU SURGE VALVE PER AMM 49-51-52 & OPS CHECK GOOD NO LEAKS NOTED @ THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,756 hrs · 6,633 cycles

BURNING SMELL NOTICED AND ENTIRE CABIN FILLED WITH LIGHT SMOKE. DEPLANED AIRCRAFT. NO SMOKE/SMELL AT MX ARRIVAL. APU BLEED & PACKS WERE NOT TURNED OFF. CHKD CARGO PITS, LAVS, LCDMR, E&E BAY NO DEFECTS NOTED. CHKD ALL C/B PANELS, FAP, ECAM NO DEFECTS. A/C OK TO CONT.

Part: ACM — WARNING MESSAGE (NR 2) · airframe 41,756 hrs · 6,633 cycles

ETOPS - AIR PACK 2 OVHT PERFORMED ECAM ACTION. SHUT OFF PACK 2. REMOVED & REPLACED RH AIR CYCLE MACHINE (ACM) PER 21-52-21-000 / 400-81-A, OPS & LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,390 hrs · 6,422 cycles

ETOPS - BOTH #1 + #2 WX RADARS DID NOT PAINT SIGNIFICANT CONVECTIVE TARGETS AT OR ABOVE CRUISE FL. PREVIOUS WRITE-UP FOR WX #1. REMOVED AND REPLACED WX #1 TRANSCEIVER PER AMM 34-41-33. TEST OK. BITE TEST OF WX #2 OK PER AMM 34-41-00. NO FAULTS NOTED. OK FOR SERVICE.

Part: TRANSMITTER — FAULTY · airframe 39,460 hrs · 6,272 cycles

ETOPS - FOB NOTED AT DEP 87.3 HOWEVER AT 4 HRS INTO FLIGHT 1200 LB UNACCOUNTED FOR. SUSPECT. FUEL LEAK ON RIGHT SIDE AS THE DIFFERENCE WOULD BE THERE. ENG BURNS MATCH AS WELL @ 6000LB/HR. REFERENCE TSM 28-26-00-810-832-A AND TSM 28-46-00-810-961-A. UNABLE TO FIND A LEAK ON LH OR RH INNER TANKS, #1 OR #2 ENGINES, OR CENTER FUEL TANK. QUANTITY INDICATIONS REMAIN STEADY ON GROUND. NOTED THAT FCMC 1 & FCMC 2 SHOWS A SLIGHT DIFFERENCE ON FOB LEVELS- FCMC 1 READING @ 61000 LBS (CONTINUED ON LOGPAGE 944512-2). AND FCMC 2 @ 59800 LBS. SWAPPED POSITIONS OF FCMC 1&2 PER AMM 28-51-34. FOUND FCMC 2 FOB INDICATION STILL READING LOWER THAN FCMC 1. FCMC POSITIONS REMAIN SWAPPED FOR TROUBLESHOOTING PURPOSES (NOTE: FCMC 1 SN: 550 AND FCMC 2 SN: 761). PERFORMED PRECAUTIONARY REPLACEMENT OF RH FUEL FLOW TRANSMITTER PER AMM 73-31-11. LEAK CHECK OKAY. OK FOR SERVICE

Part: CONTROL VALVE — FAULTED (UNKNOWN) · airframe 38,997 hrs · 6,199 cycles

ETOPS - AFTER START UNABLE TO CONTROL CABIN TEMP. ZONES INDICITNG BETWEEEN 88-90F DEGREEES AND ZONE CONTROLLER INDIATING 88F DEGREES OUTPUT @ COLDEST SETTING. REMOVED AND REPLACED RH PACK TEMPERATURE CONTROL VALVE PER AMM 21-53-53. CHECKS OKAY. ALSO FOUND BELLOWS CONNECTION TO VALVE TORN. REPLACED BELLOWS (PN:956-0009). PACK OUTPUTS IN NORMAL RANGE. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,772 hrs · 6,007 cycles

ETOPS - ENG 1 OIL CHIP DETECTED. PERFORMED TSM 79-20-00-810-823-A. NO DEBRIS FOUND. CLEANED EMCD #1. EMCD #1 TEST GOOD. REPLACED SCAVENGE OIL FILTER ELEMENT PER AMM 79-22-45. NO LEAKS NOTED. OK FOR SVC.

Part: EEC — FAULTY · airframe 37,755 hrs · 6,004 cycles

ETOPS - ENG 1 AND 2 EPR MODE FAULT, CONTINUED IN N1 MODE. MANUAL THRUST. REMOVED AND REPLACED EEC ON ENG 1.OPS CHECK GOOD. AC OK FOR CONTINUED SERVICE. REF AMM 73-21-34-400-804-A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,335 hrs · 5,934 cycles

SHIP 396 CEILING EXIT LIGHT COVER AT 3L DOOR FELL OFF AND HAVE BURNT OUT BULBS. TEMP SECURED WITH TAPE. CORRECTIVE ACTION: R/R LIGHT ASSY. (7273991)

Part: SERVO CONTROL — LEAKING · airframe 37,225 hrs · 5,915 cycles

OTHER - FLUID LEAKING FROM UNDER PANEL UNDER RT WING. FOUND INBD AILERON SERVO CTRL (7C52G) LEAKING. REMOVED & REPLACED INBD AILERON SERVO CTL REF AMM 27-14-51. UPTO STEP 4.C. (2). RII 386502. COMPLETED REMAINING STEPS PER A330 AMM 27-14-51-400-801-A. LEAK CHECK AND OPS CHECK GOOD. RII 534571.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,225 hrs · 5,915 cycles

OTHER - FOUND HYDRAULIC LEAK COMING FROM BELLY OF AIRCRAFT. REPLACED PACKING ON BLUE POWER ACCUMULATOR PER AMM 29-12-42. LEAK AND OPS CHK GOOD. OK FOR SVC.

Part: NONE — NONE · airframe 34,192 hrs · 5,443 cycles

SHIP 396 DURING WALK AROUND, NOTED THAT THE SILICONE PROTECTIVE LAYER MATERIAL WAS MISSING FROM LH UPPER TRIMMABLE HORIZONTAL STABILIZER APRON FAIRING. FIN: 333AT. THE DAMAGE MEASURES APPROXIMATELY 77" WIDE AND 22" LONG. CORRECTIVE ACTION: WORK PERFORMED REF 600866-14. (8463977)

Part: NONE — NONE · airframe 33,633 hrs · 5,339 cycles

SHIP 396 DOOR 2R SLIDE ARM/DISARM PIN WILL NOT SLIDE INTO THE HOLE. CORRECTIVE ACTION: DOOR 2R SLIDE ARM/DISARM PIN WILL NOT SLIDE INTO THE HOLE. (8462136)

Part: NONE — NONE · airframe 33,467 hrs · 5,316 cycles

SHIP 396 - ATB - GEAR WOULD NOT RETRACT. CORRECTIVE ACTION: FOUND LT GEAR SHORTENING LINK BROKEN. RMVD + RPLCD LT MLG SHORTENING LINK MECHANISM. FERRIED TO LAX. REMOVED AND REINSTALLED LEFT MLG ADJUSTABLE SHORTENING LINK. ALSO PERFORMED PRI ER/A 599443-14. JACKED AIRCRAFT. FUNCTIONAL CHECK OF NORMAL EXTENSION AND RETRACTION SYSTEM. BITE TEST LGCIU. (8496325)

Part: NONE — NONE · airframe 33,471 hrs · 5,316 cycles

SUPPLEMENTAL INFORMATION - LMLG SHORTENING LINK REPLACED & ADJUSTED // GEAR SWING & FREEFALL CHECKS ACCOMPLISHED, ALL CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: NONE — NONE · airframe 32,685 hrs · 5,164 cycles

ETOPS - DURING FUELING PROCESS LINE SERVICE UNABLE TO MOVE FUEL INTO TAIL.// REMOVED AND REPLACED TRIM TANK INLET VALVE (705QN) PER AMM 28-27 -52. CHECKS OK. OK FOR SVC ACTUATOR, SINGL OFF 43-2826-9-0002 S/N 43015 ON 43-2826-9-0001 S/N 46140

Part: NONE — NONE · airframe 32,533 hrs · 5,143 cycles

SHIP 396 EXIT SIGN COVER AT 3R DOOR IS LOOSE .CORRECTIVE ACTION: RESECURED EXIT SIGN COVER AT 3R. (7721777)

Part: SWITCH — INOPERATIVE · airframe 31,881 hrs · 5,044 cycles

SHIP 396 ALL CABIN DOORS RED PRESSURE LIGHTS FLASHING. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN PRESSURE SWITCH 40MJ. PERFORMED TEST PER A330 AMM 52-71-00. C/W PRESS LINE LEAK CK. (7247881)

Part: NONE — NONE · airframe 31,789 hrs · 5,030 cycles

SHIP 396 CEILING EMERGENCY EXIT SIGN 3L DOOR HELD IN PLACE BY TAPE. CORRECTIVE ACTION: RESECURED EXIT SIGN. (7247804)

Part: SIGN — DETACHED (CABIN) · airframe 31,724 hrs · 5,019 cycles

SHIP 396 EXIT SIGN FELL OFF BY LAV E . CORRECTIVE ACTION: RESECURED EXIT SIGN AT LAV E. (7742434)

Part: NONE — NONE · airframe 31,625 hrs · 5,000 cycles

SHIP 396 ECAM DOOR L FWD CABIN NO VS CABIN ALT INDICATION. CORRECTIVE ACTION: BITE TEST. NO FAULTS NOED SYSTEM TEST PASS. (7742262)

Part: NONE — NONE · airframe 31,583 hrs · 4,993 cycles

SHIP 396 AFTER ENGINE SHUTDOWN ECAM WARNING CABIN PRESSURE RESIDUAL PR. ALL DOORS SHOWED RESIDUAL PRESSURE. OUTFLOW VALVES WERE OPEN + COCKPIT WINDOW CRACKED TO CHECK. CORRECTIVE ACTION: NO FAULT FOUND. TEST OK. (7742220)

Part: NONE — NONE · airframe 31,563 hrs · 4,991 cycles

SHIP 396 EXIT SIGN 3R DOOR FELL OFF. CORRECTIVE ACTION: RESECURED EXIT SIGN. (7742209)

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 31,191 hrs · 4,920 cycles

SHIP 396 3L EXIT SIGN LOOSE. CORRECTIVE ACTION: SECURED 3L EXIT SIGN. (7740457)

Part: DOOR FRAME — DAMAGED (FRM 65 S42-43R) · airframe 30,955 hrs · 4,876 cycles

SHIP 396 AFT CARGO DAMAGE. CORRECTIVE ACTION: FOUND DAMAGE AT DOOR CUTOUT FR65 BETWEEN STRG 42RH -43RH. BLENDED AREA PER SRM 53-41-11 LENGTH IS .5? X .031 DEPTH. HFEC OK. (7735907)

Part: COVER — UNSECURE (R1 DOOR HANDLE) · airframe 30,863 hrs · 4,859 cycles

SHIP 396 R1 DOOR ARMING LEVER COVER DIFFICULT TO OPEN. CORRECTIVE ACTION: SECURED R1 DOOR ARMING LEVEL COVER. (7735510)

Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 30,831 hrs · 4,853 cycles

SHIP 396 ARMING AND DISARMING 2R DOOR IS DIFFICULT. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR. (7720185)

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 29,824 hrs · 4,673 cycles

SHIP 396 3R DOOR EMERGENCY EXIT SIGN BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY EXIT SIGN AT DOOR 3R. (7236400)

Part: COUPLER — DEFECTIVE (HF ANTENNA) · airframe 29,006 hrs · 4,533 cycles

ETOPS, HF 1+2 UNABLE TO TRANSMIT, SIDE TONE ONLY. FOUND CPLR2 (231133) FAULT ON HF 2 BITE TEST. REMOVED & REPLACED NR 2 HF COUPLER, PER A330 AMM 23-11-36. BITE TEST & OPERATIONS TEST OF BOTH HF 1 & HF 2 SYSTEMS GOOD. OK FOR SERVICE. COUPLER, ANTENNA OFF 43-2311-9-0001 04537 ON 43-2311-9-0001 04554.

Part: TRANSCEIVER — DEFECTIVE (HF COMMS) · airframe 28,975 hrs · 4,527 cycles

ETOPS-HF RADIOS TUNING INTERMITTENT. NORMAL TOWARDS END OF FLIGHT. REMOVED & REPLACED HF 2 TRANSCEIVER, PER A330 AMM 23-11-33. OPERATIONS TEST GOOD. OK FOR SERVICE. TRANSCEIVER, HF OFF 43-2311-9-0003 00208 ON 43-2311-9-0003 01253.

Part: COUPLER — DEFECTIVE (HF ANTENNA) · airframe 28,882 hrs · 4,507 cycles

WHILE TROUBLESHOOTING MC LOG 1638967 BITE TEST FAULTED "CPLR2(3RE2)" HF 2 ANTENNA COUPLER. FAULT CODE 231133. REMOVED & REPLACED HF2 COUPLER, PER AMM TASK 23-11-36. OPERATIONS CHECK OK, NO FAULTS NOTED. OK FOR SERVICE.

Part: ACTUATOR — FAULTED (FUEL) · airframe 28,488 hrs · 4,435 cycles

ETOPS SIGNIFICANT SYSTEM. AFT FUEL TXFR ECAM ON TAXI. SYSTEM TESTS OF FCMC 1 FAULTED INNER TANK INLET 603QL1 REMOVED AND REPLACED 603QL1 FUEL INLET ACTUATOR PER AMM 28-26-53-400-801-A. OPERATIONS TEST OK, OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (FUEL TRIM) · airframe 28,204 hrs · 4,385 cycles

ETOPS SIGNIFICANT SYSTEM - "FUEL AFT XFER" INOP STATUS MESSAGE ON STATUS PAGE. // PER TSM TASK 28-27-00-810-829-A FOUND FUEL TRIM TANK ISOLATION VALVE FAULTING (FIN 702QN). REMOVED AND REPLACED FUEL TRIM TANK ISOLATION VALVE ACTUATOR (FIN 702QN) PER AMM 28-27-52-400-802-A. OK FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (APU) · airframe 27,821 hrs · 4,314 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM APU FAULT. // T/S PER A330 TSM 49-62-00-810-916 4 D NO DEBRIS ON ELECTRICAL CHIP DETECTOR OR IN OIL FILTER ELEMENTS PER STEP 4.D SUSPECT GEN SCAVENGE 591CT32 AND LUBRICATION 59KT37 DELTA P SWITCHES AT FAULT. R/R GEN SCAV DELTA P 59K732 PER A330 AMM 49-41 LUBRICATION 59KT36 DELTA P SWITCH STILL REQUIRES TO BE REMOVED AND REPLACED. REMOVED AND REPLACED LUBE DELTA P SWITCH PER AMM 49-41, OK FOR SERVICE, OPS AND LEAK CHECK GOOD NO MSG OK FOR SERVICE.

Part: PROBE — SHORTED (EGT) · airframe 27,598 hrs · 4,278 cycles

ETOPS SIGNIFICANT SYSTEM - #1 ENGINE EGT THERMOCOUPLES PROBES 4045KS1 & 4045KS8 SHORTED TO GROUND. // REMOVED AND REPLACED EGT THERMOCOUPLES PER AMM 77-21-11-600-803-A AND REMOVED AND REPLACED EGT HARNESS PER AMM 77-21-61-400-802-A. FADEC OPS CHECK PENDING. #1 FADEC BITE GOOD. NO FAULTS NOTED. IDLE RAN #1 ENGINE GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 27,542 hrs · 4,264 cycles

ETOPS SIGNIFICANT SYSTEM - IN THE CLIMB WITH AP-2 ENGAGED, AFTER PASSING FL-280 THE A/C STARTED AN UNCOMMANDED INCREASED CLIMB RATE OF 9500 FPM. CLICKED OFF AUTO PILOT AIRSPEED, WAS APPROACHING A STALL. LEVELED OFF, REGAINED AIRSPEED. RE-ENGAGED AP-2, A/C STARTED TO CLIMB EXCESSIVELY AGAIN. CLICKED OFF AP-2 AGAIN. MANUALLY CLIMBED TO OUR CRUISE ALTITUDE OF FL-380. RE-ENGAGED AP-2. OPS NORMAL. // RESET FMGEC 2. PERFORMED AFS BITE TEST PER AMM 22-96-00. TEST PASSED. NO FAULTS NOTED. OK FOR SVC.

Part: HF COMM — MALFUNCTIONED (NR 1) · airframe 26,556 hrs · 4,118 cycles

ETOPS SIGNIFICANT SYSTEM - #1 HF CAN'T TRANSMIT (INOP) - CONSTANT KEY TONE. // PERFORM OPS CK OF HF #1 PER AMM 23-11-00. OPS CK GOOD. OK FOR SERVICE. BITE TEST HF #1 BITE TEST PASSED PER AMM 23-11-00.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 53.5+14 AND 54+12 AT -Y450 IS CORRODED AT LOCATIONS: FR53.8" ; FR53.8+2" ; FR53.9+8" ; FR54+1". // REMOVED CORROSION FROM SEAT TRACK AT FR53.8";FR53.8+2"; FR53.9+8" & FR54.1 INBOARD AND OUTBOARD LATERAL AREAS IAW A330 SRM 51-74-00 PARA 6.A THRU 6.B (3). ESTABLISHED REMAINING THICKNESS IAW A330 SRM 51-74-00 PARA 6.B (6), REASSESSED DAMAGE AT FR53.8";FR53.8+2"; FR53.9+8";FR54+1" IAW A330 SRM 51-74-00 PARA 6.B (7). DAMAGE AT FR54+1" INBOARD AND OUTBOARD LATERAL AREAS MEASURED AT 0.154" WIDE AND IS BEYOND SRM LIMITS. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53326973 ISSUE A REV 103. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 58+8 AND 62 AT -Y1959 IS CORRODED AT LOCATIONS: FR59 ; FR60+9" ; FR61 ; FR61+16". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATION FR61+16-Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. COMPLETED INSTALL OF REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) REV 103 AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 37-39) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 37.4 AND 39.2 AT -Y450 IS CORRODED AT LOCATIONS: FR37.4, FR38 + 8", FR39 + 2", FR39.2. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR37.4, FR38+8", FR39+2" FR39.2 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6)RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103, DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4 REV 103.00) AND AIRBUS DWG F53311114 ISSUE A. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAME 53) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 53.2 AND 53.4+9 AT +Y450 IS CORRODED AT LOCATIONS: FR53.2+9" & FR53.4. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR53.2+9? AND FR53.4 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53326973 ISSUE A JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y2462 IS CORRODED AT LOCATIONS: FR30+8", FR32+3",FR32+13". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR30+8", FR32+3", FR32+13" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. REPLACED COMPONENT IAW 51-72-11 PARA 2.A (4) REV 103 AND AIRBUS DWG F53276421008 ISSUE T. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 58+8 AND 62 AT -Y2462 IS CORRODED AT LOCATIONS: FR61+16 ; FR61+14 ; FR60+9 ; FR59. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR61+14" -Y12462 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103, RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. COMPLETED REPLACEMENT I.A.W. A330 SRM 51-72-11 PARA 2.A (4), REV 103.00 AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y953 IS CORRODED AT LOCATIONS: FR40.3,FR42+12",FR44+5",FR45+1",FR45+10".// CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATIONS FR40.3, FR42+12", FR44+5", FR45+1", FR45+10" +Y953 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F57112817 ISSUE D. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 37-39) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 37.4 AND 39.2 AT +Y450 IS CORRODED AT LOCATIONS: FR37.4+14",FR39+8",FR39.1+6",FR39.2. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATION FR37.4+14", FR39+8", FR39.1+6", FR39.2 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103, RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLATION OF NEW REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4)REV.103.00 AND AIRBUS DWG F53311114 ISSUE A. JOB COMPLETED

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 26 AND 34.7 AT +Y1959 IS CORRODED AT LOCATIONS: FR29,FR30+10",FR32+2",FR32+8",FR33+4",FR37.2+20", FR37.4+9". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR29,FR30+10",FR32+2",FR32+8",FR33+4",FR37.2+20",FR37.4+9" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-00-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53276421008 ISSUE T. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 31-35) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 31 AND 35 AT +Y1552 IS CORRODED AT LOCATIONS: FR33 + 3". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR33 + 3" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DRAWING F53275877, ISSUE F. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 39.2 AND 40 AT -Y450 IS CORRODED AT LOCATIONS: FR39.2 + 10", FR39.2 + 12". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATIONS FR39.2+10" AND 39.2+12" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103, RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED, COMPLETED INSTALLATION OF REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53325662 & F53325685 ISSUE B REV 103.00. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 39.2 AND 40 AT -Y1959 IS CORRODED AT LOCATIONS: FR39.2+13". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR39.2+13" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B(6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW A330 SRM 51-72-11 PARA 2.A (4), REV 103.00 AND AIRBUS DWG F53325662 & F53325685 ISSUE B. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 37-39) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 37.4 AND 39.2 AT -Y1959 IS CORRODED AT LOCATIONS: FR37.4", FR38 + 6", FR39 + 4", FR39.1 + 15". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR37.4, FR38+6", FR39+4", FR39.1+15" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW A330 SRM 51-72-11 PARA 2.A (4) REV 103.00 AND AIRBUS DWG F53311114 ISSUE A. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y450 IS CORRODED AT LOCATIONS: FR29+6",FR32,FR32+14",FR36+10",FR37.2+14". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATIONS FR29+6",FR32+14", FR36+10", FR37.2+14" +Y450 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B(6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALL REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53276421008 ISSUE T. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR40.1+14",FR41+2",FR45+1",FR46+2". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATIONS FR 40.1+14", 41+2", FR45+1", FR46+2" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F57112821 ISSUE E. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 55-58) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK #34 BETWEEN FRAME 55 AND 58+8" AT -Y2462 IS CORRODED AT LOCATIONS: FR57+9". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B.CORROSION AT LOCATION FR57+9" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-00-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53476200006 ISSUE S. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 55-58) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 55 AND 58+8" AT -Y1959 IS CORRODED AT LOCATIONS: FR55+1 ; FR56 ; FR56+13 ; FR57+8". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR57+8" -Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PAR 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. COMPLETED INSTALLATION OF NEW REPLACEMENT COMPONENT IAW A330 SRM 51-72-11 PARA 2.A (4) REV.103.00 AND AIRBUS DWG F53476200006 ISSUE S. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR40.3, FR42+16",FR44+7", FR45+17",FR48+16". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATIONS FR40.3, FR42+16", FR44+7", FR45+17", FR48+16" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F57112824 ISSUE C. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y450 IS CORRODED AT LOCATIONS: FR40.1+4",FR40.3+6",FR42,FR43+8",FR44+3". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR40.1+4",FR40.3+6",FR42,FR43+8",FR44+3" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F57112816 ISSUE E. JOB COMPLETED.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 62 AND 71+11" AT -Y1959 IS CORRODED AT LOCATIONS: FR63+10". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR63+10-Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6), RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. COMPLETED INSTALLATION OF REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) REV 103.00 AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.3+5" ; FR53.9 + 3. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR53.3+5" -Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT I.A.W. A330 SRM 51-72-11 PARA 2.A (4), REV 103.00 AND AIRBUS DWG F53326941 ISSUE A. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 54+12" AND 58+12" AT -Y450 IS CORRODED AT LOCATIONS: FR55+11";FR56+5";FR57;FR57+16" TO 19". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR56+5 -Y450 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B(6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53476200006 ISSUE S REV 103. JOB COMPLETE

Part: ROLLER TRAY — CORRODED (AFT CARGO) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

AFT CARGO ROLLER TRAY -Y1470 FR58-60 HAS EVIDENCE OF CORROSION. // CORROSION FOUND TO BE FULL THICKNESS AND OUT OF SRM LIMITS. REPLACED TRACK ROLLER TRAY IAW A330 AMM 25-51-21 REV 71. TASK NOW COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 62 AND 71+11" AT -Y1959 IS CORRODED AT LOCATIONS: FR63+10". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR63+10-Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7)FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. COMPLETED INSTALLATION OF REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) REV 103.00 AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 62 AND 71+11" AT +Y1959 IS CORRODED AT LOCATIONS: FR62+12";FR63+10";FR64+3";FR65" & FR66+10". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATION FR62 +Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B(6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103, RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. REPLACED COMPONENT IAW 51-72-11 PARA 2.A(4) AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 58-67) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 58+12" AND 67+12" AT -Y450 IS CORRODED AT LOCATIONS: FR59+4" TO +7";FR59+17";FR63+18";FR65+5" \& FR66+16". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR63+18 -Y450 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. TRACK REPLACED IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 54+13 AND 58+8 AT +Y1959 IS CORRODED AT LOCATIONS: FR56+13/& FR57+10. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR56+13 & FR57+10 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-00-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53476200006 ISSUE S. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 58.8 AND 62 AT +Y1959 IS CORRODED AT LOCATIONS: FR59;FR60+9" & FR61+19". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR59;FR60+9" & FR61+19" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-00-15 REV 103, RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR / REPLACEMENT REQUIRED. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4),REV.103.00 AND AIRBUS DWG F53477040012 ISSUE J. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 67-71) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 67+9" AND 71+9" AT -Y450 IS CORRODED AT LOCATIONS: FR68+4" TO +9";FR70 & FR69+14" TO +15". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR70 -Y450 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/ REPLACEMENT REQUIRED. TRACK REPLACED IAW 51-72-11 PARA 2.A (4) AND AIRBUS DWG F53477040 ISSUE J. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y1959 IS CORRODED AT LOCATIONS: FR40+12",FR40.1+6",FR40.1+10",FR40.2+9",FR41+1",FR42+18". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATIONS FR40+12", FR40.1+6", FR40.1+10", FR40.2+9", FR41+1", FR42+18" Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7)FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. RII CARRIED OUT IAW HAL GMM VOL1 CHAPTER 5 REV 50 - CORROSION CONFIRMED LEVEL 2 - PART REPAIR/REPLACEMENT REQUIRED. INSTALLED REPLACEMENT COMPONENT IAW 51-72-11 PARA 2.A (4) REV 103.00 AND AIRBUS DWG F57112819 ISS C. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 31-35) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552 IS CORRODED AT LOCATIONS: FR33 + 2". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR33+2" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B(6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53275878 REV E. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 53.2 AND 54 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.4. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR53.4 +Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-31-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53919398 REV C. JOB COMPLETE

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,898 hrs · 4,021 cycles

SEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: FR29+9",FR32,FR33+12",FR37.2+2",FR37.3. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 10 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR29+9",FR32,FR33+12",FR37.2+2",FR37.3 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 103 DUE TO INACCESSIBILITY. DAMAGE REASSESSED I.A.W. A330 SRM 51-74-00 PARA 6.B (7) FOUND TO BE OUT OF LIMITS I.A.W. A330 SRM 53-00-15 REV 103. TRACK REPLACED IAW A330 SRM 51-72-11 PARA 2.A (4), REV.103.00 AND AIRBUS DWG F53276421008 ISSUE T. JOB COMPLETE

Part: UNKNOWN — ODOR (CABIN) · airframe 25,233 hrs · 3,918 cycles

ATB, STRONG FUMES IN ENTIRE AIRCRAFT DURING INITIAL CLIMB FOR UP TO 20 MINS. CLEARED WITH NO USAGE OF CHECKLIST. T/S PER A330 FIM 21-00-00-810-801-A. NO DEFECTS NOTED. INSPECTED BOTH ENG'S . NO DEFECTS . OPENED AND INSPECTED BOTH PACKS AND NO DEFECTS. RAN ENG'S TO POWER PER A330 71-00. PERFORMED PACK DUCT BURNOUT PER A330 AMM 21-00. ALL OPS NML. C/W NO GO ODI PREVENTION. OK FOR SVC.

Part: GENERATOR — INOPERATIVE (APU) · airframe 25,114 hrs · 3,901 cycles

ETOPS - APU GENERATOR FAILED AND UNABLE TO RESET. COMPLETED REMOVAL AND INSTALLATION OF NEW GENERATOR PER AMM 24-23-51-000-801-A/400-801A OPS CHECK GOOD. OK FOR SERVICE.

Part: TRANSFER VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 24,943 hrs · 3,872 cycles

ETOPS / FUEL AFT TRANSFER INOP STATUS AFTER START RESET FCMC #1. REMOVED AND REPLACED FUEL AFT XFR VALVE 1 (700QN1).

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 24,826 hrs · 3,855 cycles

ETOPS SIGNIFICANT SYSTEM - #1 RADAR INOP. PERFORMED OPS CK OF WXR 1 PER A330 AMM 34-41. OK FOR SERVICE. TEST OK.

Part: CHIP DETECTOR — FAULTED (NR 2 ENGINE) · airframe 24,482 hrs · 3,808 cycles

ETOPS SIGNIFICANT SYSTEM - ON ENG SHUTDOWN AT GATE AFTER FLIGHT, ENG 2 OIL CHIP DETECTED FAULT. PERFORMED TSM 79-20-00-810-824-A AND BITE CHECK OF EEC 2 CHA+B, NO FAULTS DETECTED, INSPECTED NR 2 ENG CHIP DETECTOR, NO DEFECTS NOTED. OK FOR SVC.

Part: GENERATOR — FAULTED (APU) · airframe 23,439 hrs · 3,654 cycles

ETOPS SIGNIFICANT SYSTEM - APU GEN FAULT. // PERFORMED TSM 24-20-81-810-942-A. REMOVED AND REPLACED APU GEN PER AMM 24-23-51. OPS NORMAL, NO DEFECTS NOTED. LEAK CHECK OK. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,221 hrs · 3,619 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER STARTING NR 2 ENG ECAM ENG2 OVSP PROT FAULT, ENGINE PARAMETERS NORMAL. MAINT CONTROL TOLD US TO SHUT DOWN ENG 2 AND RESTART. AFTER RESTART NO ECAM OR FURTHER MESSAGE ALL INDICATIONS NORMAL. SYSTEM TEST OF EEC 2 OK NO FAULTS NOTED A/C OK FOR SVC.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 22,643 hrs · 3,530 cycles

RCVD 2 TEMPO LAV SMOKE ALARMS ENROUTE. PERFORMED BITE OF SDF, NO FAULTS. OK FOR SVC.

Part: OIL SYSTEM — LOW (APU) · airframe 22,240 hrs · 3,468 cycles

ETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL MSG.// PERFORMED TSM 49-00-00810-815A. FAULT APU OIL LVL LOW, SERVICE APU PER AMM 12-13-49. NO LEAKS NOTED, OK FOR SVC.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO VENT) · airframe 22,198 hrs · 3,462 cycles

OPEN - ATB - INTERMITTENT FWD CARGO VENT AND BULK VENT INOP SYS INDICATIONS. ATB DUE TO DOG IN BULK CARGO.// PERFORMED VC SYSTEM 21-28-00-710-802A. SYSTEM TEST PASSED. ON CONDITION PAGE UNABLE TO CONTROL BULK CARGO TEMP. DEACTIVATED BULK CARGO ISOL VALVES PER AMM 21-28-00-040-803. OK TO CONTINUE PER MEL 21-28-4B. "M" PROCEDURES COMPLIED WITH. LIDS UPDATED. PLACARD INSTALLED. DMI# 509978.

Part: WARNING MESSAGE — FALSE ACTIVATION (OIL COOLER) · airframe 21,812 hrs · 3,393 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 1- AIR EXCHANGER FAULT MINOR FAULT.// PERFORMED ENG 1 EEC CHAN"A" AND CHAN"B" TEST PASSED TAW AMM 73-21-00-710-812 AND "AIR/OIL HEAT EXCHANGER"CONNECTORS CLEANED AND RESECURED.

Part: LENS — LOOSE (EXIT SIGN) · airframe 21,762 hrs · 3,381 cycles

3L DOOR EXIT LIGHT COVER LOOSE.// RE-SECURED 3L DR EXIT LIGHT COVER. SECURITY CK GOOD

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 21,735 hrs · 3,376 cycles

ETOPS SIGNIFICANT SYSTEM - "ENG. 1 MINOR FAULT". // PERFORMED BITE CHECK OF BOTH EEC'S. NO FAULTS DETECTED. COULD NOT DUPLICATE FAULT. OK FOR SVC.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 21,735 hrs · 3,376 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM "ENG 1 AIR EXCHANGER FAULT".// TROUBLESHOT FAULT MESSAGE FOR FLIGHT REPORT PER A330 TSM 79-20-00-810-809-A. OPERATIONALLY CHECKED AIR EXCHANGER VALVE. NO FAULTS NOTED. VISUALLY CHECKED ALL CANNON PLUGS AND PINS ATTACHED TO AIR EXCHANGER. ALL CHECKS NORMAL. COULD NOT DUPLICATE FAULT. OK FOR SVC.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 21,638 hrs · 3,360 cycles

ETOPS SIGNIFICANT SYSTEM - ON LANDING. ENG 1 AIR EXCHANGER FAULT. ENG 1 MINOR FAULT.// PERFORMED TROUBLE SHOOT PER TSM 79-20-00-810-809-A. VISUAL INSPECTED AIR OIL/HEAT EXCHANGER, NO DAMAGE FOUND. PERFORMED FADEC SYSTEM TEST PER AMM 73-21-00. SYSTEM TEST OK. NO FAULT DETECTED. AIRCRAFT OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 21,638 hrs · 3,360 cycles

ETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL. SERVICED 3 QT OF APU OIL PER AMM 12-13-49. C/W VISUAL INSPECTION OF APU & NO LEAK NOTED, RAN APU & OPS CHK GOOD. OK FOR SVC.

Part: FILTER — ACTIVATED (APU) · airframe 20,652 hrs · 3,213 cycles

AFTER STARTING APU. APU FAULT ECAM MESSAGE, SHUT DOWN THE APU IAW ECAM. ECAM MESSAGE, LUBE PUMP FILTER & GEN SCAV FILTER 5100KT9. INSPECTED BOTH OIL LUBE FILTER AND GEN SCAV FILTERS IAW TSM 49-62-00-810-916-A. NO FINDINGS OF METAL. DPI ON LUBE FILTER TRIPPED. RESET CHECK. REPLACED FILTER ELEMENTS. OK FOR SERVICE.

Part: LIGHT — MISSING (GALLEY) · airframe 19,988 hrs · 3,115 cycles

AFT GALLEY EMERGENCY LIGHT STRIP MISSING A PORTION. REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-52, OPS CHECKED NORMAL. OK FOR SERVICE.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 19,937 hrs · 3,107 cycles

DIVERSION TO NEAREST AIRPORT DUE TO G HYD FAILURE, LANDED BELOW 400K WEIGHT. FOUND GREEN HYD SYS HP MANIFOLD 5102JM OUTBOARD BLEEDER PLUG ORING DAMAGED. REMOVED AND REPLACED ORING PER AMM 29-11-53, RE-SERVICED GREEN SYSTEM, RAN ALL ELEC AND ENGINE DRIVEN PUMPS, CHECKED ALL ACCUMULATORS, NO LEAKS NOTED, RESET FREE-FALL SYS, MC ADVISED, NO STATUS MSG PRESENT.

Part: O-RING — DAMAGED (HYD MANIFOLD) · airframe 19,933 hrs · 3,106 cycles

DIVERTED DUE TO GREEN HYDRAULIC SYSTEM QUANTITY LIGHT ON. REPLACED A DAMAGED GREEN HYDRAULIC SYSTEM HP MANIFOLD 5102JM OUTBOARD BLEEDER PLUG O-RING.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 19,884 hrs · 3,098 cycles

EXIT SIGN AT THE R3 DOOR FELL OFF INFLIGHT. ATTACHED THE EXIT SIGN. SECURITY CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 18,920 hrs · 2,952 cycles

NR 2 ENGINE LP VALVE FAULT ECAM MESSAGE. PERFORMED A BITE TEST OF FCMS IAW AMM 28-51-00, NO DEFECTS NOTED.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · corrosion level 2 · airframe 18,525 hrs · 2,897 cycles

ETOPS SIGNIFICANT SYSTEM - FUEL FLOW INDICATIONS + TOTALIZER DO NOT INDICATE ON FUEL. PERFORMED RESET OF FCMC 1 & 2. INDICATIONS NORMAL. OK FOR SVC.

Part: SEAM — LEAKING (RT WING) · airframe 18,254 hrs · 2,858 cycles

PRIOR TO DEPARTURE GROUND CREW FOUND A FUEL LEAK FROM THE RIGHT WING. FUEL LEAK FROM RIGHT WING SEAM BETWEEN FWD SPAR AND UPPER WING SUFRACE 5 - 6 INCHES INBD FROM RIB 11. RIGHT WING SEAM REPAIRED. LEAK CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 17,321 hrs · 2,698 cycles

OVERHEAD AISLE EMERGENCY LIGHT AT ROW 25 LEFT MISSING LENS. INSTALLED NEW LENS.

Part: SIGN — DETACHED (CABIN) · airframe 16,647 hrs · 2,599 cycles

R3 DOOR EXIT SIGN DETACHED. SECURED THE SIGN.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 15,175 hrs · 2,385 cycles

L3 DOOR EXIT SIGN DETACHED FROM CEILING. REPLACED THE EXIT SIGN.

Part: ACTUATOR — MALFUNCTIONED (NR 2 A/C PACK) · airframe 14,886 hrs · 2,343 cycles

NR 2 A/C PACK REGULATOR FAULT. NR 2 PACK RAM AIR DOOR CLOSED ECAM MESSAGE. PERFORMED TROUBLESHOOTING IAW TASK 21-63-00-810-886-A. RESET THE CIRCUIT BREAKERS FOR PACKS 1 & 2, AND SYSTEM TESTED IAW AMM 21-63-00, FOUND CLASS 3 FAULT ON THE NR 2 PACK AIR INLET FLAP ACTUATOR. OPERATED PACKS AND VISUALLY CHECKED THE INLET FLAP ACTUATORS, OPS OK. NO ECAM MESSAGE. ACFT OK FOR SERVICE.

Part: LIGHT — UNSECURE (ROW 17A) · airframe 14,304 hrs · 2,259 cycles

ROW 17A EMERGENCY LIGHT NOT SECURE. SECURED THE EMERGENCY LIGHT.

Part: LIGHT — UNSECURE (CABIN) · airframe 14,304 hrs · 2,259 cycles

EMERGENCY LIGHT LOOSE ADJACENT TO 45HJ. EMERGENCY LIGHT SECURED.

Part: BRAKE — LOCKED (MLG) · airframe 14,215 hrs · 2,240 cycles

ABORTED TAKEOFF DUE TO ACFT PULLED HARD LEFT AT BEGINNING OF T/O ROLL APPEARS NR 1 & NR 5 WHEEL BRAKES LOCKED UP ABORTED AT APPROXIMATELY 70-80 KNOTS. REF LOG 8115523 NR 1 BRAKE "GRABBING". REMOVED & REPLACED NR 5 BRAKE ASSY PER AMM 32-42-27. OPS NORMAL NO DEFECTS FOUND DURING BITE MAX REPORTED BRAKE TEMP ON NR 1 AND NR 5 WAS 390 DEGREES C. OK TO CONTINUE PER MEL 32-42-1 DEACTIVATED NR 1 BRAKE ASSY PLACARD INSTALLED LIDS UPDATED.

Part: CONTROLLER — MALFUNCTIONED (CONTROL STICK) · airframe 12,689 hrs · 2,017 cycles

F/O SIDE STICK FCPC 1 FAULT. REMOVED AND REPLACED FLT CONTROL STICK CONTROLLER IAW AMM 27-92-41 UP TO STEP 4G,

Part: UNKNOWN — ODOR (CABIN) · airframe 12,612 hrs · 2,002 cycles

FA'S IN AFT GALLEY AREA REPORTED A TEMPORARY "ELECTRICAL BURNING" SMELL THEY COULD NOT LOCATE EXACT LOCATION BUT PWRD OFF ALL AFT OVENS AND SMELL WENT AWAY. OPERATED ALL 7 AFT GALLEY OVENS, COULD NOT DUPLICATE "ELECTRICAL BURNING" ODOR. NO DEFECTS NOTED, OK FOR SVC. VERIFIED W/ OUTBOUND FLT CREW PRESENT.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 12,356 hrs · 1,967 cycles

DOOR 3R EXIT SIGN COVER FELL OFF. RE-ATTACHED EXIT SIGN COVER.

Part: ENGINE — MAKING METAL (APU) · airframe 7,735 hrs · 1,211 cycles

ACFT RETURNED TO GATE, APU AUTO SHUTDOWN. OIL CHIP DETECTION MESSAGE 499111. TROUBLESHOT IAW TSM 49-62-00-810-915-A, REPLACED SCAVANGE/LUBE FILTERS IAW AMM 49-91-41, COLLECTED OIL SAMPLES, NO METAL NOTED. INSPECTED CHIP DETECTOR, AND FOUND SMALL METAL PARTICLES, COLLECTED SAMPLES. CLEANED CHIP DETECTOR, OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 4,095 hrs · 647 cycles

FM MESSAGES ON MCDU NR 1. PERFORMED RESET OF BOTH FMGEC 1 & 2, AFS BITE IAW 22-96-00, TEST OK. OK FOR SERVICE.

Part: FUEL SYS — MALFUNCTIONED (NR 1 ENGINE) · airframe 3,393 hrs · 538 cycles

EXCESSIVE FUEL FLOW ON NR 1 ENGINE DURING CLIMBOUT + 3-4000 LBS AN HOUR. THEN NORMAL DURING CRUISE/LEVEL OFF NR 1 FUEL USED 1200 LB > THAN NR 2 ENG (CONT) 3 + 20 HRS AFTER DEPARTURE NR 1 ENG FUEL FLOW CYCLING BETWEEN 5- 9000 LBS AN HOUR DURING CRUISE FUEL USED 3,000LBS, THAN NR 2 ENG IN ALL OTHER ENGINE PARAMETER NORMAL STABLE. CLEANED AND INSPECTED NR 1 ENG FUEL TRANSMITTER, CONNECTOR. PERFORMED TSM 73-30-00-810-805-A. WET MOTOR AND ENGINE IDLE RUN CHECK OK. BITE EEC 1 CHA AND B. NO FAULTS NOTED, OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (APU) · airframe 2,846 hrs · 438 cycles

APU START SUCCESSFUL. APU FAULT AFTER INFLIGHT START. TROUBLESHOT IAW TSM 49-62-00. CHECKED LUBRICATION, OIL FILTER AND GENERATOR OIL FILTER DIFFERENTIAL PRESSURE INDICATORS. CHECK OK. PERFORMED APU TEST IAW AMM 49-62 TEST OK. INDICATION NORMAL. UNABLE TO DUPLICATE DISCREPANCY.

Part: COMPUTER — MALFUNCTIONED (BLEED AIR SYS) · airframe 1,865 hrs · 279 cycles

BLEED AIR LOW TEMP ECAM LT ENGINE DURING INITIAL CLIMB, PERFORMED ECAM ACTIONS, JETTISON FUEL FOR NORMAL LANDING. REMOVED AND REPLACED NR 1 BMC IAW AMM 36-11-34. BITE TEST OK PER AMM 36-11-00. ACCOMPLISHED TSM 36-21-00-810-914-A. NO FAULTS NOTED ON GROUND.

Part: ADIRU — OUT OF ALIGNMENT · airframe 1,446 hrs · 215 cycles

AFTER ADIRS ALIGNMENT ECAM AUTO FLT FM1 FAULT. ALIGNED ADIRS. RESET FMGEC 1 & 2. GROUND OPS CHECKED OK, AMM 22-96-0.