N379HA

Part: PA SYSTEM — INOPERATIVE (ZONE 200) · airframe 40,763 hrs · 6,477 cycles

ETOPS - FA IR PA INOP. REMOVED AND REPLACED IR-PA HANDSET PER AMM 23-73-44. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: BMC — DAMAGED · airframe 40,563 hrs · 6,444 cycles

ETOPS - AIR L WING LEAK DET FAULT ON ECAM. FOUND BMC 2 BOX DAMAGED. REMOVED AND REPLACED BMC 2 PER AMM 36-11-34. CONDITION SAME. REMOVED BMC 1 & BMC 2 OPEN C/B'S C73 & T34. LOOP CONNECTORS AT 382HF DISCONNECTED PER AMM 36-22-00-810-909-A. 382HF 275OHMS TO BMC 1 4B, INSULATION RESISTANCE OPEN 381HF 268OHMS TO BMC 1 3B, INSULATION RESISTANCE 36M OHMS. RECONNECTED 382HF LOOP CONNECTOR PER AMM 36-22-19. INSTALLED BMC 1 & 2 AND CLOSED C73 & T34 C/B. OPERATIONAL CHECK OK. PER AMM 36-11-34-400-802-A.

Part: FILTER — CLOGGED (HYD SYSTEM) · airframe 39,914 hrs · 6,335 cycles

ETOPS - FOUND EDP CASE DRAIN FILTER FLAG POPPED C/T ENGINE HYDRAULIC PUMP 4000JG1 IN REF TO 1A-ENG 1 VISUAL CHECK TASK CARD FOR #1 ENG EDP CLOGGING INDICATOR INSP. RESET CLOGGING INDICATOR FLAG AND REMOVED AND REPLACED AFFECTED FILTER PER AMM 29-11-43-600-809-A. ENGINE RUN COMPLETED, NO LEAKS DETECTED. OK FOR CONT SVC.

Part: ACTUATOR — FAULTED (JETTISON VALVE) · airframe 39,623 hrs · 6,282 cycles

ETOPS - A/C WONT TAKE FUEL. BITE TEST OF FCMC + FUEL VALVES TEST FAULTS LH FUEL JETTISON VALVE ACTUATOR. REMOVED OF LH FUEL JETTISON VALVE ACTUATOR PER AMM 28-31-51-000-801-A. INSTALLED ACTUATOR PER AMM 28-31-51 OPS CHECK GOOD. OK FOR SERVICE.

Part: BMC — FAULTED (NR 1) · airframe 39,119 hrs · 6,199 cycles

ETOPS - AIR WING L DET FAULT - AFTER GROUND POWER DROP. REPLACED BMC1 PER AMM 36-11-34-00-802-A. BITE TEST GOOD. OK FOR SVC.

Part: ENGINE — MAKING METAL (NR 2) · airframe 39,014 hrs · 6,180 cycles

ETOPS - AFTER LANDING ENG 2 - OIL CHIP DETECTED. PERFORMED DETAILED INSPECTION OF #2 EMCD. MAGNETIC FINES FOUND AND COLLECTED. WITHIN LIMITS PER AMM 79-00-00-200-822-A. REMOVED AND REPLACED OIL SCAVENGE FILTER PER AMM 79-22-45-920-801-A. RAN # 2 ENG PER AMM 79-22-45-920-801. LEAK CK GOOD NO LEAKS NOTED. OK FOR SVC.

Part: PIN — WORN (CHECK VALVE) · airframe 37,837 hrs · 5,997 cycles

ETOPS - #2 ENG IP CHECK VALVE ANTI ROTAION PIN WORN. REPLACED #2 ENG IP CHECK VALVE PER AMM 36-11-41. LEAK CHECK & OPS CHK GOOD. OK FOR SVC.

Part: PIN — WORN (CHECK VALVE) · airframe 37,837 hrs · 5,997 cycles

ETOPS - #1 ENG IP CHECK VALVE ANTI ROTATION PIN WORN. REMOVED AND REPLACED #1 ENG IP CHK VALVE PER AMM 36-11-41. OPS CHK GOOD

Part: HEAT EXCHANGER — LEAKING (NR 1 ENGINE) · airframe 37,486 hrs · 5,942 cycles

ETOPS - #1 ENG AOHE AND AIR FLOW CONTROL S/N: 3200674-1588 LEAKS OIL FROM HEAT EXCHANGER. REPLACED AOHE PERR AMM 79-21-41-400 LEAK CHECK GOOD . OPD CHECK GOOD. OK FOR SVC

Part: SLIDE — NO TEST (L3 DOOR) · airframe 36,798 hrs · 5,834 cycles

WHILE PERFORMING T/C 330-335100-01-1 FOUND 3L SLIDE FAULTING. REMOVED AND REPLACED SLIDE PER AMM 25-62-42-000-801-A01 AND 25-62-42-400-801A OPS CHK GOOD. OK FOR SVC

Part: HANDSET — DAMAGED (INTERPHONE) · airframe 35,103 hrs · 5,574 cycles

ETOPS - 2L DOOR INTERPHONE HANDSET HANGING ON BY THREADS. REMOVED & REPLACED 2L DOOR HANDSET PER AMM 23-73-44. OPS CHECK OK. OK FOR SVC.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 34,235 hrs · 5,440 cycles

ETOPS - DURING PRE DEPARATURE FOUD LEFT ENGINE BLUE HYDRAULIC SYSTEM EDP LEAKING BEYOND LIMITS. REPLACED LEFT BLUE HYDRAULIC PUMP IAW 29-12-51.OPS CHECK AND LEAK CHECK GOOD PER AMM 29-12-51. SERVICE BLUE HYDRAULIC SYSTEM IAW 12-12-29 OK TO RETURN TO SERVICE.

Part: EXCITER — FAULTED (APU) · airframe 34,152 hrs · 5,428 cycles

ETOPS - APU - FAULT AUTO SHUT DOWN. REMOVED AND REPLACED EXITER- IGNITION PER AMM 49-41-38-00-801-A TROUBLESHOOTING DONE PER TSM 49-41-00-810-813-A. OPS CHECK GOOD. AC OK TO CONTINUE SERVICE.

Part: TRANSDUCER — FAULTED (NR 1 HIGH PRESS) · airframe 33,577 hrs · 5,335 cycles

ETOPS - AIR ENG L HPV NOT OPEN ANNUNCIATION UPON DESCENT. REMOVED AND REPLACED ENGINE #1 BLEED TRANSFERRED PRESSURE-TRANSDUCER, PE RAMM 36-11-15. BITE TEST AND LEAK CHECK GOOD. OK FOR SVC. REMOVED AND REPLACED #1 ENGINE HP VALVE, PER 36-11-51. OPS AND LEAK CHECK GOOD. OK FOR SVC.

Part: IGNITION LEAD — ARCED (NR 2 ENGINE) · airframe 33,567 hrs · 5,333 cycles

ETOPS - WHILE WORKING TSI FOR ENG 2 IGN FAULT SAW ARCING AT 4002EH2 IGNITION LEAD. REMOVED IGNITION LEAD PER AMM 74-21-52-000-801-A. INSTALLED IGNITION LEAD PER AMM 74-21-52. OPS TEST GOOD. OK FOR SVC

Part: APU — SHUTDOWN · airframe 33,347 hrs · 5,299 cycles

ETOPS - APU AUTOSHUTDOWN 3 UNSUCCESSFUL STARTS. REMOVED & REPLACED GEV SCAV FILTER PER AMM 49-91-41-960-801. OPS & LEAKS CHK GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,297 hrs · 5,290 cycles

ETOPS - DURING WALK-AROUND INSPECTION FOUND DAMAGE ON #1 ENGINE FAN BLADE (LABELED #1). REMOVED AND REPLACED #1 ENGINE #1 FAN BLADE PER A330 AMM 72-31-41-400-801-A OPS CHECKS OK PERFORMED #1 ENGINE IDLE RUN, NO DEFECTS NOTED A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,206 hrs · 5,277 cycles

ETOPS - APU AUTO SHUTDOWN AT RON SPOT PRIOR TO TOW TO GATE. SHUTDOWN REPORT SHOWS LUBE AND GEN SCAV FILTERS. REMOVED AND REPLACED APU GEN SCAVENGE OIL FILTER AND LUBRICATION FILTER IAW 49-91-41 (AMM). LEAK TEST GOOD,NO LEAK FOUND. APU START AND OPERATE NORMALLY, OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,457 hrs · 5,160 cycles

ETOPS - FOUND FILLER #20 SEAL AND FILLER #11 SEAL DAMAGED ON #1 ENGINE. REMOVED AND REPLACED #20 ANNULUS FILLER AND #11 ANNULUS FILLER PER AMM 72-31-41-400-802-A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 31,178 hrs · 4,961 cycles

ETOPS - DURING PDC FOUND #1 ENG OIL QTY LOW READING 13.3 UNITS. FOUND EXTERNAL OUL VENT TUBE LEAKING AT FITTING ON #1 ENG CORE 9 O CLOCK POSITION. TORQUED CONNECTOR PER AMM 72-51-49-400-801-A. ENG RUN GOOD. NO LEAKS NOTED.

Part: FMU — FAULTY · airframe 30,833 hrs · 4,908 cycles

ETOPS - FUEL LEAKING FROM #2 ENG DRAIN MAST. REMOVED AND REPLACED #2 ENG FMU PER AMM 73-21-52. RAN ENGINE, OPS CHECK LEAK CHECK GOOD. PRECAUTIONARY CHANGED #2 ENG FUEL EJECTOR PER AMM 71-71-42. RAN ENG #2 OPS CHECK LEAK CHECK GOOD. OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 30,778 hrs · 4,894 cycles

ETOPS - AT ENG SHUTDOWN AIR ENG 2 BLEED NOT CLOSED. ENG 2 BLEED FAULT AMBER. REMOVED AND REPLACED #2 ENG PRV BLEED VALVE PER AMM 36-11-52-400-804-A OPS AND LEAK CHECK GOOD OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 29,715 hrs · 4,739 cycles

OTHER - UPON LANDING AND DECELRATION #5 TIRE WAS DEFLATED TO ZERO PRESSURE. AIRCRAFT WAS DIFFICULT TO MANUVER AND WE WERE UNABLE TO TAXI. SHUT A/C ENGINES DOWN AND TOWED TO GATE. FOUND #5 TIRE WITH BLOW OUT. PERFORMED A330 AMM TASK 05-51-15-200-801-A. NO DAMAGE OR TROUBLE FOUND. R/R #5 WHEEL ASSY IAW A330 AMM 32-41-11.

Part: UNKNOWN — UNKNOWN · airframe 29,069 hrs · 4,640 cycles

ETOPS-DURING PDC WALK AROUND FOUND FUEL DRIPPING FROM #2 ENG FUEL DRAIN MAST. ACCOMPLISHED TSM 71-00-00-810-915-A PH. A(4)(A). PERFORMED ENG #2 IDLE RUN, NO LEAKS NOTED. AFTER ENG SHUT DOWN, LEAK NOTED. REMOVED AND REPLACED #2 ENG FUEL DRAIN EJECTOR. IN REFW/ A330 AMM 71-71-42-400-804-A. SEC AND CONDITION GOOD. NO LEAKS NOTED. OK FOR SVC

Part: NONE — NONE · airframe 27,565 hrs · 4,397 cycles

ETOPS - #2 HF RADIO WILL NOT TUNE. BITE TEST PASS PER AMM 23-11-00. DUE TO MULTIPLE WRITES UP OF HF #2, REMOVED & INSTALLED NEW HF COUPLER & TRANSCEIVER PER AMM 23-11-36 & AMM 23-11-33. OPS TEST HF#2 PASS PER AMM 23-11-00. BITE TEST HF#2 PASS PER AMM 23-11-00. CALLED SFO ARINC, RECEIVED & TRANSMIT LOUD AND CLEAR. OK FOR SERVICE. COUPLER, ANTENN OFF 43-2311-9-0001 04877 ON 43-2311-9-0001 04554, TRANSCEIVER, HF OFF 43-2311-9-0002 05127 ON 43-2311-9-0003 00160.

Part: NONE — NONE · airframe 27,225 hrs · 4,329 cycles

SHIP 379 1R DOOR SHOWS OPEN ON ECAM WHEN CLOSED. CORRECTIVE ACTION: FOUND DOOR 1 RH PROX SWITCH TARGET ARM BRACKET MOVES STICKY. LUBRICATE TARGET ARM AND OPS CHECKDOOR CLOSED/ LOCKED AND OPENED 10 TIMES GOOD AND VERIFIED INDICATIONS ARE GOOD ON ECAM AND FAP PANEL.PERFORMED SPCU SYSTEM TEST, TEST OK, NO FAULTS NOTED. (8459670)

Part: NONE — NONE · airframe 26,125 hrs · 4,141 cycles

SHIP 379 1R DOOR INDICATES OPEN WHEN CLOSED. CORRECTIVE ACTION: FOUND 12MJ PROX SENSOR OUT OF LIMIT. ADJUSTED PER AMM 52-71-11. NO FAULTS NOTED ON PSCU BITE. (8452803)

Part: NONE — NONE · airframe 26,105 hrs · 4,139 cycles

SHIP 379 INSTALLED PHOTO STRIP AND CHECKED OK PER A330 AMM 25-21. CORRECTIVE ACTION: T/S. PSCU BITE TEST PASSED. NO FAULTS NOTED. (8485085)

Part: NONE — NONE · airframe 26,007 hrs · 4,117 cycles

SHIP 379 1R DOOR CLOSED AND INDICATING OPEN. CORRECTIVE ACTION: T/S. OPS CHK OK. NO FAULTS NOTED. (7716091)

Part: VALVE — INOPERATIVE · airframe 25,348 hrs · 3,995 cycles

ETOPS - FUEL OUTR TK INLET VLV1 (500QU1) FAULT // REMOVED AND REPLACE INLET VALVE 1 ACT. PER AMM 28-25-57-400-801-A. OPS CHK OK ACTUATOR, SINGL OFF 43-2826-9-0001 S/N 53084 ON 43-2826-9-0002 S/N 40125

Part: LIGHT — ABNORMAL · airframe 24,665 hrs · 3,881 cycles

SHIP 379 4L DOOR PRESSURE WARNING LIGHT ON THROUGHOUT DESCENT FOR APPROX 10 MIN ONCE STARTED DOWN FROM FL 400. CORRECTIVE ACTION: T/S. PERFORMED BITE TEST OF PSCU. TESTS OK. NO FAULTS ON POST FLIGHT REPORT. (8455883)

Part: PRESSURE SYSTEM — ABNORMAL · airframe 24,082 hrs · 3,782 cycles

SHIP 379 PRESSURE WARNING LIGHTS ON ALL CABIN DOOR ILLUMINATED ON APPROACH. CORRECTIVE ACTION: NO PFR DATA. OP TEST OF CPC1 AND CPC2 PASS. (7730202)

Part: NONE — NONE · airframe 23,705 hrs · 3,719 cycles

SHIP 379 - DIV - TO LAX DUE TO 2L DOOR HIGH PITCHED NOISE WITH HISTORY. CORRECTIVE ACTION: INSPECTED DOOR AREA AND FOUND NO DAMAGE ON SEAL. DUE TO HISTORY, APPLIED SPEED TAPE ON DOOR SCUFF PLATE. REPAIR IS ACCEPTABLE FOR 900 FLIGHT HOURS. DEFERRED TO MON LOG. (7739511) REPLACED 2L SCUFF PLATE.(7739511)

Part: NONE — NONE · airframe 23,676 hrs · 3,715 cycles

SHIP 379 CORROSION, CRACK AND DISBOND DAMAGE WERE FOUND ON THE AIR INTAKE BOX CASING. CORRECTIVE ACTION: APU AIR INTAKE BOX CORRODED AREA REPAIRED IAW ERA 588870-14. (1981534)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK Y-450 FR47-FR53.2. CORRECTIVE ACTION: REPLACED AS PER AIB DWG. ALSO REF ER/A 588871-14. (1979208)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK Y-2462, FR47-FR53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK IAW SRM 51-44-11. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978081)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION ON SEAT TRACK AT Y1959 FR 59-64. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980343)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION ON SEAT TRACK AT LOCATION -Y953, FR55-58. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980357)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION ON SEAT TRACK BETWEEN FR58 AND FR68. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980346)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK Y-1959 FR47-FR53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978098)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK AT Y1959 FR47-53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK IAW SRM 51-44-11. SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978087)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION ON SEAT TRACK AT -Y1959 FR 59-62. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED. (1980353)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND WEB ASSY FORWARD OF DR 1R AT FR 14 CORROSION BEYOND LIMITS. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980341)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK AT Y-1959 FR53.2-54. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980351)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK AT Y1959 FR 53.2-54. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980349)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT FRAME 33, -Y1959. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING RESISTANCE CHECK CARRIED OUT. (1980345)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK AT Y1959 FR40-47. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP ON NEW SEAT TRACK IAW SRM 51-44-11. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING CHECK CARRIED OUT. (1978092)

Part: NONE — NONE · corrosion level 2 · airframe 23,676 hrs · 3,715 cycles

SHIP 379 FOUND CORROSION AT SEAT TRACK AT Y-1959 FR 40-47. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP ON NEW SEAT TRACK SRM 51-44-11. NEW SEAT TRACK INSTALLED SRM 51-42-11. BONDING CHECK CARRIED OUT. (1978095)

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 23,259 hrs · 3,642 cycles

SHIP 379 2L EXIT SIGN FELL OFF. CORRECTIVE ACTION: INSTALLED EXIT SIGN. (7721857)

Part: WARNING MESSAGE — FALSE ACTIVATION (R1 DOOR) · airframe 23,086 hrs · 3,611 cycles

SHIP 379 1R DOOR UNARMED INDICATION ON 1L PANEL DURING FINAL DESCENT. SELF CLEARED. CORRECTIVE ACTION: PERFORMED BITE OF CIDS. TEST OK. VERIFIED 1R DOOR DAMPENER HAS SUFFICIENT PRESSURE. (5882279)

Part: GENERATOR — ABNORMAL (APU) · airframe 22,862 hrs · 3,571 cycles

DUE TO APU GEN FAULT T/S PER TASK 24-20-00-810-986-A. PERFORM RESISTANCE CHECKS PER THIS TSM TO CONFIRM FAULT PER STEP 4A. IF NO TROUBLE IS FOUND IN THE WIRING CHECKS PLEASE REPLACE APU GEN. ACCOMPLISHED TSM 24-20-00-810-986-A. RESISTANCE CHECK OF APU GEN PMG FAILS RESISTANCE READING PINS 13-14 RESISTANCE IS 28OHMS. OTHERS PINS OKAY WITHIN LIMITS. EXCITER FIELD PINS 9-10 RESISTANCE CHECK 7.6 OHMS. RESISTANCE CHECK BETWEEN GAPCU PINS 9,10,11,12,13 TO APU GEN PINS 14, 13, 12, 9, 10 CHECK OK AND NO SHORTS TO GROUND. NEED TO REPLACE APU GEN. REMOVED AND REPLACED APU GEN PER AMM 24-23-51 UP TO STEP SUBTASK 710-050-A(F)(1). COMPLETED REMAINING STEPS PER AMM 24-23-51-400-801-A. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: RECEPTACLE — SHEARED (HUB CAP) · airframe 22,488 hrs · 3,504 cycles

SHIP 379 - ATO - ON T.O. ROLL AT 70KTS ECAM, BRAKES RELEASED, BRAKE #4 RELEASED. CORRECTIVE ACTION: FOUND TACH DRIVE SPLINE RECEPTACLE ON HUB CAP #4 TIRE SHEARED. REPLACED WITH NEW HUB CAP. REMOVED AND REPLACED #4 MLG TIRE.

Part: BRAKE — MALFUNCTIONED · airframe 22,473 hrs · 3,502 cycles

ATO - BTB- ON T.O. ROLL AT 70KTS ABORT ECAM: BRAKES RELEASED, BRAKE 4 RELEASED // APPLIED MEL 32-42-1 #4 MLG BRAKE DEACTIVATED "M" PROCEDURES C/W. DMI # 518076 A/C OK FOR SVC. MEL & PLACARD INSTALLED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 21,859 hrs · 3,394 cycles

WHILE INSTALLING EPSU BATTERIES, EPSU BOX WOULD NOT TEST AT DOOR 1R (12WL). CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY, PER W/C 3351-4002-HAL. REMOVED 1R AND 4R DOOR SLIDE AND PERFORMED WIRING CHECKS. R & R 1R DOOR SLIDE, PER AMDS CARD 2561-9403. RII C/W.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 21,859 hrs · 3,394 cycles

WHILE INSTALLING NEW EPSU BATTERIES "PUSH TO TEST" AT 4R DISPLAYED BLINKING INTERIOR & EXTERIOR LIGHTS FAULT (18WL). CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY, PER W/C 3351-4002 HAL. REMOVED & REPLACED 4R SLIDE, PER AMDS CARD 2561-9403 RII C/W.

Part: SPLINE — BROKEN (HUB CAP) · airframe 21,598 hrs · 3,348 cycles

ATO-ON TO ROLL AT APPROXIMATELY 80 KIAS, ECAM BRAKES RELEASED, BRAKE 4 RELEASED. PREVIOUS WRITE UPS 7277029 AND 7277033 LOG-PAGE UPDATED AT 08DEC20 1031 UTC. PERFORMED TSM 32-40-00-810-929-S. FOUND HUB CAP DRIVE SPLINE BROKEN OFF HUB CAP. REMOVED AND REPLACED HUB CAP, REF AMM 32-41-15-400-801-A. OK FOR SERVICE.

Part: SPLINE — BROKEN (HUB CAP) · airframe 21,598 hrs · 3,348 cycles

ATO-ON T/O ROLL, AT APPROXIMATELY 80 KIAS, ECAM BRAKES RELEASED. BRAKE 4 RELEASED. PREVIOUS WRITE UP NR 7277029. FOUND TACHOMETER-WHEEL SPEED (14GG2)/BSCU (3GG) ON BSCU SYS TEST. OK TO CONTINUE, PER MEL 32-42-1. NR 4 BRAKE DEACTIVATED W/O BRAKE REMOVAL. PLACARD INSTALLED/LIDS UPDATED. DMI 517134. MLG HUB CAP HAS BEEN REPLACED. FOUND HUB CAP DRIVE SPLINE BROKEN. OK TO CLEAR DMI. REACTIVATED NR 4 BRAKE. OPERATIONS AND LEAK CHECK GOOD. LIDS CLEARED, PLACARD REMOVED.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 21,497 hrs · 3,329 cycles

ETOPS-ON WALK AROUND, FOUND FUEL LEAKING FROM NR 1 ENGINE. FOUND LP FUEL LINE TO DRAINS COLLECTOR TANK CHAFED THROUGH AT A HOSE CLAMP BY FUEL PUMP. REMOVED & REPLACED FUEL LINE SECTION TO DRAIN COLLECTOR TANK. PERFORMED ENGINE IDLE RUN, LEAK CHECK OK.

Part: ENGINE — VIBRATION (NR 2) · airframe 21,252 hrs · 3,289 cycles

ENG NR 2 VIB INDICATORS AMBER (X) LOG-PAGE UPDATED AT 18SEP20 2344 UTC. WHILE PERFORMING TSM 73-25-81-810-916-A, REMOVED AND REPLACED NR 2 ENGINE REMOTE CHARGE CONVERTER, PER AMM 77-32-13--400-802-A. OPS CHECK OF INDICATION FAILED. REQUIRES FURTHER TROUBLESHOOTING AS 1649860 9/18/20. REINSTALLED ORIGINAL RCC, PER AMM 77-32-13. REMOVED AND REPLACED NR 2 EIVMU, PER AMM 73-25-34. NR 2 ENG VIB INDICATION NORMAL, OK FOR SVC. UNIT, ENGINE, I OFF 43-7325-9-0001 04578 ON 43-7325-9-0001 04272 LOG-PAGE UPDATED AT 18SEP20 2344 UTC.

Part: GENERATOR — OUT OF LIMITS (APU) · airframe 21,211 hrs · 3,284 cycles

DURING SERVICE CHECK APU GEN FAULT LIGHT NO OUTPUT POWER FROM APU, RPTD BY CHACON. GENERATOR APU, OFF 33-2423-9-0001 04304 ON 33-2423-9-0001 05088, CHECKS GOOD. VERIFIED NO VF NEEDED PER HAL MOPM, A02(5000VE). REPALCED APU GEN IAW A330 AMM 24-23. OPS AND LEAK, FOR R & R PULLED C/B'S C72(742VU) A03(5000VE), APU GEN RESISTANCE OUT OF LIMITS. WAITING FOR AP GEN TO APPROVE, PER TSM HAL A330 24-23 SHOT WIRES AT APU GEN PIN 9 & 10. FOUND, POS: AC TASK HRS: 0002.0 TASK ELAPSE TIME HRS: 0002.0 RII: N, CORR BY JIMENEZ 00873124 LAX 11SEP20 ATA 2424, GEN, 00111745 LAX 11SEP20, CLOSED FLT/CHK MTC. NON ROUTINE LINE.

Part: ACTUATOR — FAULTED (APU) · airframe 20,779 hrs · 3,214 cycles

ETOPS SIGNIFICANT SYSTEM - APU START FAULT - 3 ATTEMPTS. REMOVED AND INSTALLED SERVICEABLE APU FLAP ACTUATOR PER AMM 49-16-51-000-801-A AND 49-16-51-400-801-A. OPS CHECK GOOD. OK TO CONTINUE.

Part: IGNITER — DEFECTIVE (NR 2 ENGINE) · airframe 20,667 hrs · 3,195 cycles

ETOPS SIGNIFICANT SYSTEM - NR 2 ENG IGN B FAULT/ INOP. PERFORMED AUDIBLE TEST ON IGNITION B SYS PER AMM 74-00. VERY WEAK POPPING. REMOVED & INSTALLED IGNITER PER AMM 74-21 OPS CHECK NORMAL.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 20,467 hrs · 3,159 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM "ENG 1 BLEED NOT CLOSED". // REMOVED NUMBER 1 ENG PRV PER AMM 36-11-57. INSTALLED NUMBER 1 ENGINE PRV PER AMM 36-11-52, OPS CHECK LEAK CHECK GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 20,467 hrs · 3,159 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM "ENG 2 BLEED NOT CLOSED". // REMOVED AND INSTALLED #2 ENG PRV PER AMM 36-11-52-400-804-A. OPS CHECK LEAK CHECK GOOD PER AMM 36-11-52.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU BLEED) · airframe 19,054 hrs · 2,943 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER LANDING ECAM - AIR APU BLEED FAULT. // BMC BITE TEST 1 AND 2 C/OUT IAW AMM 3611-00. SUBSEQUENT OPS CHECK NOW NORMAL, MSG SELF ERASED.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 18,067 hrs · 2,793 cycles

ETOPS SIGNIFICANT SYSTEM - #1 ENGINE GREEN HYDRAULIC PUMP LEAKING AT THE DRIVE PAD ATTACH POINT AND AT PUMP SPLIT LINE. // REMOVED AND REPLACED #1 GREEN HYDRAULIC PUMP GASKET AND SPLINE SEAL REF A330 AMM 29-11-51. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 18,067 hrs · 2,793 cycles

ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE GREEN HYDRAULIC PUMP LEAKING AT THE DRIVE PAD ATTACH POINT AND AT PUMP SPLIT LINE. // REMOVED AND REPLACED #1 GREEN HYDRAULIC PUMP GASKET AND SPLINE SEAL REF A330 AMM 29-11-51. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 16,750 hrs · 2,590 cycles

ETOPS SIGNIFICANT SYSTEM - APU OIL SERVICE REQUIRED. APU OIL SERVICE CARRIED OUT. 3 US QTS ADDED. APU AREA INSPECTED. NIL LEAKS FOUND. OIL CAP CONFIRMATION CHECK CARRIED OUT, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FCMC) · airframe 16,732 hrs · 2,588 cycles

ETOPS SIGNIFICANT SYSTEM - FUEL FCMC 1 FAULT ILLUMINATED ON DESCENT. // PER INTERROGATED MSG # 285134 SHOWN. FCMC GRD TEST C/OUT REF AMM 28-51-00 ALL INDICATIONS NORMAL TEST OK MSG CLEARED.

Part: SATCOM — FAULTED · airframe 16,639 hrs · 2,575 cycles

ETOPS SIGNIFICANT SYSTEM - COM SATCOM FAULT. RESET SITCOM SYSTEM PERFORMED BITE PER AMM 23-28-00 TESTED OK. OK FOR SVC

Part: TIRE — DEFECTIVE (NLG) · airframe 15,525 hrs · 2,418 cycles

ATO - SEVERE NOSE GEAR VIBRATION. BEGAN APPROX 60 KNOTS. AGGRESSIVELY WORSE W/SPEED. RTO @ 90-100 KTS. T/S IAW TSM 32-20-00-810-801-A DUE TO RTO & RTB. FOUND A HOP ON LT NLG TIRE AFTER JACKING AND SPINNING WHEELS. REMOVED & REPLACED LT & RT NLG TIRE ASSY IAW AMM 32-41. LUBED NOSE GEAR LOWER AREA IAW AMM 12-22. BOTH AXLE SLEEVES GVI GOOD. NO HISTORY FOR NOSE SHIMMY. A/C OK FOR SVC.

Part: TIRE — DEFECTIVE (NLG) · airframe 15,530 hrs · 2,419 cycles

AIRCRAFT 379 ATO - ABORTED TAKEOFF AT 90-100 KNOTS DUE TO SEVERE NOSE GEAR VIBRATION. CORRECTIVE ACTION: REPLACED LEFT AND RIGHT NOSE TIRES, AND LUBED NOSE GEAR LOWER AREAS. LP 5875735

Part: OIL SYSTEM — LOW (APU) · airframe 14,650 hrs · 2,282 cycles

ETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL ADVISORY. PERFORMED TSM 49-00-00-810-815-A. FOUND APU OIL LEVEL LOW. SERVICED APU PER AMM 12-13-49. NO LEAKS NOTED. OK FOR SVC.

Part: PACKING — LEAKING (HYD MANIFOLD) · airframe 14,175 hrs · 2,215 cycles

ATB - HYD B ENG 1 PUMP LO PR HYD B SYS LOW PR ECAM.// BLUE HYD INDICATED 1/4 FULL AT BLOCK IN. CREW REPORTED ENG 1 EDP ISOLATED AFTER MSG. NO CAVITATION TO ENG 1 EDP NOTED, ALL DPI CHECKED OK. FOUND PACKING ON BLUE HP MANIFOLD LEAKING. REPLACED PACKING PER AMM 29-12-53. SVC BLUE HYD TO FULL PER AMM 12-12-29 OPS+ LEAK CHK OK.

Part: INDICATOR — DETACHED (TORQUE) · airframe 14,009 hrs · 2,188 cycles

F/CTL FLAPS FAULT ECAM RAN ECAM PERFORMED EMERG LANDING. PER FLT CREW. // T/S PER A330 TSM 27-50-00-810-816A. FOUND OVER TORQUE INDICATOR RELEASED ON INPUT GEARBOX 5 LH (5053CV). REQUIRES DRAIN AND FILL ROTARY ACTUATOR (5055CV) AND INPUT GEARBOX (5053CV). DRAINED AND FILLED ROTARY ACTR (5055CV) AND INPUT GEARBOX (5053CV) IAW MM 12-13. PER FIM 27-50-00-810-816 PARA 5A. OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 13,489 hrs · 2,107 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER APU START APU OIL LEVEL MESSAGE APPEARED. OIL SERVICED NOW OK FOR SERVICE. SECOND CHECK OF CAP CARRIED OUT 2 QUARTS UPLIFTED.

Part: BRAKE — OVERHEATED (NR 6) · airframe 12,632 hrs · 1,958 cycles

IMMEDIATELY AFTER LIFT OFF, BEFORE GEAR UP COMMAND WAS GIVEN, ECAM CAUTION FOR HOT BRAKES DISPLAYED, NR 6 BRAKE TEMP 315, ALL OTHER BRAKES LESS THAN 200. LEFT GEAR EXTENDED UNTIL NR 6 TEMP BELOW 300,THEN RETRACTED GEAR. PUMPED BRAKES, NO BRAKE DRAG, OPS CHECKED GOOD, OK FOR SERVICE.

Part: OXYGEN BOTTLE — DEFECTIVE (CABIN) · airframe 11,798 hrs · 1,822 cycles

OPEN - LAV F/L81 FLIGHT ATTENDANTS REPORTED "POPPING, RATTLING" SOUND FROM OXYGEN MASK COMPARTMENT AND AN UNFAMILIAR ODOR. SUSPECT O2 MASK DISCHARGE.REMOVED & REPLACED EMERGENCY OXYGEN CONTAINER IN LAV F PER AMM 35-21-41. OPS CHECK OK. OK FOR SVC.

Part: OIL SYSTEM — LOW (APU) · airframe 11,085 hrs · 1,711 cycles

APU HIGH OIL UPLIFT / OIL ADD EXCEEDANCE FLAG AT APU OIL ENTRY DURING A SERVICE CHECK. ADDED 2 QTS OF OIL AT SERVICE CHECK. VERIFIED OIL FILLER CAP O-RING SERVICEABLE. RAN APU FOR 5+ MINUTES IAW AMM 49-00 & COMPLIED WITH A VISUAL LEAK INSPECTION DURING & AFTER RUN. NO LEAKS OR DISCREPANCIES FOUND. OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (LP VALVE) · airframe 11,057 hrs · 1,707 cycles

NR 2 ENG FUEL LP VALVE FAULT ECAM MESSAGE ILLUMINATED TWICE, SHORTLY AFTER TOP OF CLIMB. MESSAGE CLEARED BOTH TIMES. NO ECAM MESSAGE SHOWED ON ARRIVAL. MESSAGE 282451, CLASS 1, HARD, NR 2 ENGINE LP VALVE, SFCC 1,SHOWED ON PFR. FOLLOWED TSM 28-24-00-810-824-A. REPLACED THE NR 2 ENGINE LP VALVE ACTUATOR IAW AMM 28-24-51, P401. PERFORMED LP VALVE OPS TEST IAW AMM 28-24-00-710-803-A, TESTED SATISFACTORY. OK FOR SERVICE.

Part: DAMPER — BROKEN (CONTRO STICK) · airframe 11,032 hrs · 1,704 cycles

CAPTAIN`S CONTROL STICK, SEEMS TO HAVE DECREASED CONTROL FEEL WHEN APPLYING LT AILERON VS APPLYING RT AILERON. FIRST OFFICER`S STICK HAD NORMAL FEEL. REMOVED THE CAPTAIN`S STICK IAW AMM 27-92-41. THE INTERNAL DAMPENER FOUND BROKEN. REPLACED THE CAPTAIN`S STICK IAW AMM 27-92-41-400-817-A THRU STEP F(1), OPS CHECKED OF SIDE STICK ASSEMBLY, OPS CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING DEVICES OF THE SIDE STICK CONTROLLER AND RUDDER PEDALS CHECKED OK IAW AMM 22-10-00-710-803A. OPS CHECK OF TAKEOVER AND PRIORITY FUNCTION CHECKED OK IAW AMM 27-96-00-710-804A. OPS CHECK OF VHF SYSTEM CHECKED OK IAW AMM 23-12-00-710-801A. LAND CAT III TEST CHECKED OK IAW AMM 22-97-00-740-801A. AND AMM 27-92-41-400-817A

Part: UNKNOWN — SMOKE · airframe 10,408 hrs · 1,607 cycles

ON LANDING, & ROLLOUT, TOWER ADVISED SMOKE COMING FROM THE MAIN LANDING GEAR AREA LEFT SIDE. INSPECTED, AND FOUND OK. TAXIED TO GATE, OPS NORMAL. INSPECTED THE LT MLG TIRES AND BRAKES. NO DEFECTS NOTED. CONDITION AND SECURITY CHECKED OK.

Part: TRANSFER SYS — MALFUNCTIONED (CENTER FUEL TANK) · airframe 9,746 hrs · 1,507 cycles

500 LBS OF FUEL IN CENTER TANK DID NOT FEED. ON PFR, FOUND MESSAGE FCMC 1, RESET AND SYSTEM TEST OF FCMC AND FUEL VALVES TEST PERFORMED IAW AMM 28-51-00-740-801A, AND 28-51-00-710-801A, BOTH TESTS PASSED. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (FUEL) · airframe 9,707 hrs · 1,501 cycles

ECAM FAULT, FUEL FCMC 2 FAULT. RESET FCMC 2, AND MESSGAE CLEARED. PERFORMED SYSTEM TEST IAW AMM 28-51-00-740-801-A. TEST PASSED, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,650 hrs · 1,494 cycles

DURING PRE FLIGHT F/A NOTED A FAINT BURNING ODOR IN THE LDCRM. INSPECTED LDCRM FOR THE ODOR. NO SMOKE ODOR DETECTED. OK FOR SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 9,237 hrs · 1,431 cycles

EXIT SIGN AT SEAT 37L BROKEN, RE-SECURED EXIT SIGN.

Part: WARNING MESSAGE — UNKNOWN · airframe 7,141 hrs · 1,124 cycles

ENROUTE, BOTH FMGEC -EFOB ON F-PLN PAGE BEGAN TO FLUCTUATES REGULARLY BY AS MUCH AS 2000 LBS. FUEL BURN NORMAL. INDICATIONS CAUSED REFILE OF ALTERNATE AIRPORT FOR EFOB CALCULATIONS. PFMD VIS FUEL LEAK FROM TKS AND ENGS -NO FUEL LEAK FOUND. PFMD AFS TEST SHOWS FAULT "FMGEC1" CLASS 1 MSG. SWAPPED FMGEC1 AND 2 AND PFMD AFS TEST AND SHOWS FMGEC1 CLASS 3 MSG. IAW AMM 22-96-00. NOTIFIED MC AND OBSERV FURTHER. A/C STILL OK TO CONT IN SVC. ALSO A/C OK TO LLM OPS.

Part: IDG — LOW (NR 2 ENGINE) · airframe 6,316 hrs · 1,003 cycles

ETOPS SIGNIFICANT SYSTEM - IDG 2 SYS FAULT. SERVICED NR 2 IDG AND PERFORMED BITE TEST OF THE ELECTRIC POWER GEN SYS (EPGS) AND GCU AND GAPCU PER TASK AMM 24-41-00 OPS CHECK GOOD. OK FOR SVC. BITE TEST PASSED.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 5,734 hrs · 910 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE AT SEAT 26GE. FOUND WIRES WERE CROSSED. PUT WIRES IN THE CORRECT POSITION. LP 8983037

Part: LIGHT — INOPERATIVE (CABIN) · airframe 899 hrs · 5,689 cycles

OVERHEAD EMERGENCY LIGHT INOP AT 26GE. OK TO CONTINUE PER MEL 33-51-1A.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 5,176 hrs · 816 cycles

RETURNED TO DEPARTURE DUE TO THE LOSS OF YELLOW HYDRAULIC QUANTITY. REPLACED YELLOW SYSTEM HP MANIFOLD O-RING.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 5,172 hrs · 812 cycles

DURING CRUISE, LOST YELLOW HYD QUANTITY ATB. FOUND O-RING ON YELLOW SYSTEM HP MANIFOLD BLOWN OUT FROM FITTING. REMOVED AND REPLACED ORING. OPS TEST OF YELLOW HYD SYSTEM PER AMM 29-13-00-00-710-801-A. NO LEAKS NOTED OPS CHECK OK. SVC HYD SYSTEM. OK FOR SERVICE

Part: BOLT — MISSING (NR 4 WHEEL) · airframe 4,321 hrs · 684 cycles

NR 4 MAIN TIRE TIE BOLT MISSING. REMOVED AND REPLACED THE NR 4 MAIN TIRE AND WHEEL ASSY IAW AMM 32-41. OK FOR SERVICE.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 2,466 hrs · 403 cycles

DURING WALK AROUND, A DENT WAS FOUND ON THE LEFT NR 1 SLAT TOP SKIN LOCATED AT WFX 6584 COMMON TO THE FREE EDGE DUE TO A BIRD STRIKE. DENT MEASURED 2.35" X 1.75" AND .250" DEEP. PERMANENT REPAIR IAW SRM 57-40-00 FIG 222 AND ER/A 547433-14.