N375HA

Part: CONTROLLER — FAULTED · airframe 42,160 hrs · 6,659 cycles

ETOPS - BTB > DURING ENGINE 2 START UP GOT ENG OVSPD PROT FAULT FOLLOWED BY: FO AOA HEAT, FO PITOT HEAT, FO TAT HEAT, FO STATIC HEAT. REMOVED AND REPLACED PHC 2 PER AMM 30-31-34. BITE CHECK OK. OPS CHECK W/ PROBE/ WINDOW HEAT SWITCH OK. CHK'D WIRING ON PHC 2 -- ALL GOOD ON GND- NO FAULT W/ WIRING

Part: FILTER — CLOGGED (APU OIL SYS) · airframe 41,625 hrs · 6,574 cycles

ETOPS - APU AUTOSHUTDOWN PRIOR TO TOW TO GATE. APU LUBE AND SCAVANGE FILTERS INDICATED AS CLOGGED. REMOVED AND REPLACED LUB AND SCAVANGE FILTERS PER AMM 49-91-41. LEAK CHECK GOOD. OPS CHECK GOOD OF APU. OK FOR SERVICE.

Part: DRAIN — BROKEN (ENG CASE) · airframe 41,280 hrs · 6,518 cycles

ETOPS - INSPECTION FOUND ENGINE 1 REAR CASE DRAIN FILTER BROKEN. REAR CASE DRAIN TUBE REPLACED AS PER AMM 70-51-00-910-802A. INSTALLATION CHECKED SATISFACTORY.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 41,132 hrs · 6,495 cycles

ETOPS - AIR ENG 1 BLEED FAULT AFTER TAKEOFF RESET SUCCESSFUL. REMOVED AND REPLACED #1 ENG PRV PER AMM 36-11-12. OPS & LEAK CHECK OK. OK FOR SERVICE.

Part: TRANSDUCER — FAULTED (APU) · airframe 41,041 hrs · 6,480 cycles

ETOPS - APU FAULT. APU SHUTDOWN , 2 START TATTEMPTS. PERFORMED TSM TASK 49-62-00-810-844-A. REMOVED AND REPLACED APU INLET PRESSURE TRANSDUCER PER A330 AMM 49-23-17. OPS CHK GOOD. OK FOR SVC.

Part: FILTER — INOPERATIVE (HYD SYSTEM) · airframe 41,000 hrs · 6,472 cycles

ETOPS - FOUND YELLOW ENGINE-PUMP CASE-DRAIN FILTER ASSY INOP. REMOVED AND REPLACED YELLOW ENGINE-PUMP CASE-DRAIN FILTER ASSY IAW AMM 29-13-43-000-804-A AND 29-13-43-400-804-A. LEAK CHECK GOOD. OK TO RETURN TO SERVICE.

Part: A/C PACK — ODOR (ZONE 100) · airframe 40,657 hrs · 6,419 cycles

ATB, BURNING PLASTIC ODOR NOTED .SUSPECTED ODOR FROM PACKS.PER TSM 05-50-00-810-829-A AND AMM 36-10-00-615-804-A, PERFORMED HP ENG RUN AND NO FOUND ANY SMELL AND PLASTIC SMELLS. PERFORMED BLEED SYS AND PACK SYS DECONTAMINATION FOR 60 MIN WITH HOT AIR. OK FOR SERVICE.

Part: SHAFT — SHEARED (STARTER) · airframe 40,523 hrs · 6,400 cycles

ETOPS - APU FAULT. FOUND STARTER SHAFT SHEARED. REMOVED AND REPLACED STATER PER AMM 49-42-51. REPLACED STARTER CLUTCH MODULE AS PRECAUTIONARY PER AMM 49-42-41. OPS AND LEAK CHECK GOOD.

Part: ACTUATOR — FAULTED (FUEL TRANSFER) · airframe 40,323 hrs · 6,368 cycles

ETOPS - FUEL AFT TRANSFER FAULT. BTB. FOUND RH INNER TANK INLET VLV ACTUATOR FAULTING 603QL2. REPLACED PER AMM 28-26-53. CHK OK

Part: FUSE — INOPERATIVE (APU) · airframe 39,964 hrs · 6,311 cycles

ETOPS - APU AUTO SHUTDOWN (2-ATTEMPTS). FOUND FUSE FIN 6KA1 INOP-REMOVED AND REPLACED FUSE PER AMM 49-42-00 AND ACCOMPLISHED PRECAUTIONARY STARTER CHANGE DUE TO PREVIOUS SHUTDOWNS PER AMM 49-42-51. OPS CHECK GOOD.

Part: FUEL LINE — LEAKING (NR 1 EING) · airframe 39,264 hrs · 6,209 cycles

ATB - FUEL LEAK #1 ENG. FOUND TUBE PN:FW53576 BETWEEN THE #1 ENG FUEL PUMP AND LP FUEL FILTER LEAKING. REMOVED DAMAGED TUBE. REPLACED TUBE P/N: FW53576 PER AMM 70-12-01-400-002-A. ENG IDLE RUN AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: RADIO — MALFUNCTIONED (HF COMMS) · airframe 38,966 hrs · 6,162 cycles

ETOPS - #1 HF RADIO UNABLE TO CHANNELIZE. TRIED SEVERAL DIFFERENT FREQUENCIES. REMOVED AND REPLACED HF 1 COUPLER PER AMM 23-11-36. BITE TEST OK. OPS CHECK GOOD. OK FOR SERVICE

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 38,724 hrs · 6,126 cycles

ETOPS -AFTER T.O ECAM AIR ENG2 BLEED FAULT RESET PER MOC. RESET SUCCESSFUL. REPLACED PRV ON THE #2 ENG PER AMM 36-11-52. OPS/ LEAK CHK OK.

Part: BLANKET — PUNCTURED (NR 2 ENGINE) · airframe 37,888 hrs · 5,995 cycles

ETOPS - #2 ENG RH C DUCT THERMAL BLANKET PUNCTURED. LOCATED BOTTOM OF C DUCT & ROUGHLY CENTERED. REPAIRED THERMAL BLANKET PER CMM 78-30-20. OK FOR SVC.

Part: STARTER — INOPERATIVE (APU) · airframe 37,492 hrs · 5,935 cycles

ETOPS - ON MORNING WAKE UP APU FAIL TO START NO ROTATION. REMOVED AND REPLACED APU STARTER IAW AMM 49-42-51 NO FIX. NO ROTATION. REPLACED FUSE 6KA1 WITH NEW IAW A300 AMM 49-42-00-960-801 APU START SUCESSUFLLY

Part: SENSOR — FAULTED (COCKPIT TEMP) · airframe 36,927 hrs · 5,839 cycles

ETOPS - COCKPIT TEMP CANT HOLD A TEM. IT FLUCTUATES BETWEEN 50-100 DEGREES ALL FLIGHT. REMOVED AND REPLACED COCKPIT TEMP SENSOR 650HK REF AMM 21-63-17. OPS CHECK GOOD.

Part: THERMOCOUPLE — FAULTED (NR 2 ENGINE) · airframe 36,573 hrs · 5,779 cycles

ETOPS - AFTER LANDING ECAM ENG 2 MINOR FAULT. REMOVED AND REPLACED ENG 2 THERMOCOUPLE OVERHEAT RTECTOR REAR PER AMM 77-22-11-400-801-A. OPS CHECK GOOD PER TSM 77-22-00-810--805-A. NO FAULTS NOTED. OK FOR SVC.

Part: SPRING — BROKEN (AFT CARGO) · airframe 35,808 hrs · 5,663 cycles

ETOPS-DURING X2 INSPECTION FOUND MULTIPLE SPRINGS BROKEN AFT CARGO RAISED FOR IDENTIFICATION. REPLACED SPRINGS AS REQUIRED OK FOR SERVICE

Part: SPRING — BROKEN (FWD CARGO) · airframe 35,808 hrs · 5,663 cycles

ETOPS-DURING X2 INSPECTION FOUND MULTIPLE SPRINGS BROKEN FWD CARGO RAISED FOR IDENTIFICATION. REPLACED SPRINGS AS REQUIRED OK FOR SERVICE

Part: LINE — LEAKING (HYD SYSTEM) · airframe 37,863 hrs · 5,602 cycles

OTHER - ON POST FLIGHT CHK, MECHANICS FOUND HYD LEAK IN LH WHEEL WELL. FOUND L/G DOOR SUPPLY LINE CHECK VALVE LEAKING. REMOVED & REPLACED SEAL PER AMM 32-31-37-000-801-A01 / 400-801-A. LEAK CHK GOOD. PERFORMED OPERATIONAL CHECK OF LANDING GEAR DOORS PER AMM 32-31-00-710-8020A OPS CK GOOD, LEAK CK GOOD, OK FOR SVC

Part: OIL COOLER — FAULTY (APU OIL SYSTEM) · airframe 35,110 hrs · 5,556 cycles

ETOPS - APU FAULT ECAM INFLIGHT. APU FAULT INDICATED HI OIL TEMP. FOUND OIL COOLER RESTRICTED. REMOVED & REPLACED OIL COOLER PER AMM 49-91-44. OPS CHECK/LEAK CHECK OK.

Part: PCU — FAULTED (NR 1 ENGINE) · airframe 34,972 hrs · 5,535 cycles

ETOPS - ENG 1 MINOR FAULT. REMOVED AND REPLACED ENG#1 PCU PER 73-21-35. FADEC SYS TEST GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,459 hrs · 5,456 cycles

ETOPS - ENG 1 18PSI UNABLE TO PROCEED. REMOVED & REPLACED #1 ENG(PRV) BLEED VALVE(4001HA) REF AMM 36-11-52. OPS/LEAK CHK GOOD. NO DEFECTS NOTED. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,062 hrs · 5,396 cycles

ETOPS - REPORTED FROM GND HANDLING. FOUND DAMAGE AFT CGO DIAGONAL LINING PANEL LEFT OF CGO LOADING POSITION 42P. REPAIED WITH SPEED PATCH IAW AMM TASK 25-50-00-340-804A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,071 hrs · 5,397 cycles

ETOPS - YELLOW HYD SYSTEM AMBER XX'S. NO QTY INDICATION & PUMP NO TURN ON. REMOVED & REPLACED HSMU PER AMM 29-11-34. BITE TEST OK. YELLOW HYD PUMP OPS NORMAL. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,859 hrs · 5,368 cycles

ETOPS-ECAM AIR PACK 2 VALVE FAULT. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK OK. ECS TEST OK. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,834 hrs · 5,365 cycles

ETOPS-YELLOW HD SYSTEM LOW QUANTITY. REMOVED AND REPLACED MANIFOLD CHECK VALVE O-RING IAW AMM 29-13-53-400-802-A. SERVICED YELLOW HYDRAULIC SYSTEM WITH SKYDROL PE-5 TO FULL CAPACITY IAW AMM 12-12-29-03, OPS CHECK GOOD, NO LEAKS NOTED, A/C OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,418 hrs · 5,301 cycles

ETOPS - HYD Y ENG 2 PUMP LO PR ECAM. REMOVED AND REPLACED HYD Y ENG 2 PUMP AS PER A330AMM 29-13-51-000-802-A, 29-13-51-400-802-A LEAK CHECK OK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 33,251 hrs · 5,271 cycles

ETOPS - BTB ECAM - HYD Y SYS LO PR. FOUND PLUG ON YELLOW HP MANIFOLD LEAKING REPLACED SEAL AND REINSTALLED PER AMM 29-13-53-400-803-A. LEAK CHECK GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,250 hrs · 5,149 cycles

ETOPS - FLIGHT ATTENDANT SAID ODOR SMELL LIKE A "IRON WAS ON" PRIOR TO LANDING IN AREA OF SEAT 3H/3J ALL SYSTEMS NORMAL IN COCKPIT. FOUND DUCT P/N F003055900600 TO TRIM AIR VALVE 632HK OBLITERATED. REPLACED DUCT PER AMM 21-63-51. LEAK CHECK GOOD. OPREATED PACKS AND NO BURNING SMELLS DETECTED. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,270 hrs · 5,122 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT. DURING T/S NOTICED GROUND TERMINAL LUG OFR CONNECTROR TO DETECTOR 4012WD WITH A LOOSE FITTING. TERMINAL LUG REMOVED AND REPLACED IAW ASM 71-51-04 P0004 SHEET 1. BITE TEST OF FDU 1 C/O. IAW AMM 26-12-00-740-804-A. TEST OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,266 hrs · 5,121 cycles

ETOPS - ENG 1 FIRE LOOP B ECAM: CAME ON, ON APP THU UNTIL 1500'. REPLACED TERMINAL LUGS AT DETECTOR 4012WD. IAW ESPM 20-48-00/ AMM 71-51-04. ACCOMPLIHSED #1 ENG RUN OPS CHECK FAIL. RECURRING #1 ENG FIRE LOOP B. PERFORMED T/S WM 71-51-04 AND FOUND SHORT TO GND ON 4012WD NEAR TERMINAL C (1Z001R20). REMOVED SHORT ON ENG #1 WIRE 1Z001R&B20 AND REMOVED WIRE CHAFE ON WIRE 1Z002R&B20. RETERMINATED WIRE PER AMM 70-71-26. SECURED WIRES AND OPS CHECK PER AMM 26-12-00. ALL TESTS PASS. OK FOR SERVICE

Part: CONTROL UNIT — FAULTED (VSV) · airframe 31,807 hrs · 5,045 cycles

ETOPS - BTB DUE TO ENG1 CTL SYS FAULT AFTER ENG START. REMOVED VSV CONTROL UNIT IAW AMM75-33-51-000-801-A. INSTALLED VSV CONTROL UNIT PER AMM 75-33-51-400-801-A UP TO STEP 4.E. PERFORMED LEAK AND OPS CHECK OF #1 ENG VSVC PER AMM 71-00-00-700-827. LEAK AND OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 31,013 hrs · 4,916 cycles

ETOPS - WORKING TSS #2 ENGINE LOW TGT. FOUND THERMOCOUPLE TO CASE SHORT @ POSITION 1:00 & 7:00. REMOVED AND REPLACED 1:00 AND 7:00 POSITION THERMOCOUPLE PER AMM 77-21-11, OPS CHECK GOOD NO DEFECTS NOTED.

Part: RCCB — FAULTED (NR 1 ENGINE) · airframe 29,658 hrs · 4,707 cycles

ETOPS-DUE TO N1, N2 & BB VIBRATION REPORTED ANOMALIES ON NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENG RCC IAW AMM 77-32-13. CHECKED OK. OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 29,487 hrs · 4,675 cycles

ETOPS-#1 ENG FWD HYD PUMP NOTED WITH EVIDENCE OF LEAKS AT MULTIPLE LOCATIONS ON THE PUMP CASE AND BROKEN / PROTRUDING MATING FACE GASKET. REMOVED FWD (BLUE) HYD PUMP, CLEANED, AND REPLACED SHAFT SEALS AND MOUNTING GASKET AND INSTALLED NEW HYD PUMP REF A330 AMM 29-12-51. LEAK AND OPS CHECK GOOD. PUMP, HYDRAULIC OFF 33-2912-9-0002 10643 ON 33-2912-9-0002 31041

Part: NONE — NONE · airframe 29,096 hrs · 4,610 cycles

SHIP 375 DURING ASPSU TEST FOUND ASPSU "FAULT" AND "OK" LEDS NOT COMING ON. CORRECTIVE ACTION: T/S. ASPSU(101MJ)DOOR1/DEUB( 330RH1) FAULT ON ASPSU SYSTEM TEST. WIRING CHECKS GOOD BETWEEN DEU B AND ASPSU. FOUND 28VDC AT PIN N AND P OF 101MJA. R/R ASPSU PER A330 AMM 52-71-36. (9749416)

Part: COMPUTER — INOPERATIVE · airframe 26,013 hrs · 4,075 cycles

ETOPS - IN CRUISE- RT MAIN FUEL TANK INDICATED 9,000 LB LOW. 15 MINS LATER IT CORRECTED TO ACTUAL FUEL LOAD. FF INDICATED 200 LBS HIGHER BURN FOR #2 ENG // T/S PER A330 TSM 28-42-00. BITE OF FCMC 2 SHOWS FAULT 284215 FUEL INR PROBE2 (120QTS). REPLACED FCMC2 AS PER A330 AMM 28-51-34. NO EXTERNAL LEAKS NOTED. CREW REPORTS NORMAL FUEL BURN. ALL FUEL QTY IND NORMAL AT THIS TIME. COMPUTER, FCMC OFF 43-2851-9-0001 S/N 04470 ON 43-2851-9-0001 S/N 02047

Part: SKIN — DAMAGED · airframe 26,042 hrs · 4,080 cycles

SHIP 375 FOUND L/H ELEVATOR T/E UPPER LEFT SURFACE MISSING APPROX 32" OF FILLER MATERIAL. CORRECTIVE ACTION: REF A330 SRM 55-21-11-283-015. OK TO TO APPLY TEMP REPAIR. C/W REP INSP OF LH ELEV UPPER LEFT T/E PER A330 SRM 51-77-12-911-011. SPEED TAPE INTACT. (7731461)

Part: COMPUTER — DEFECTIVE · airframe 25,832 hrs · 4,048 cycles

ETOPS - #1 ENGINE VIBRATION MONITOR INOP // REPLACED CSU P/N 065-50001-0200 S/N OFF 04253. NO HELP. PER A330 AMM 27-51. (PAUL SERBICK 576703). REMOVED AND REPLACED #2 SFCC PER A330 AMM 27-51-34 OPS CHECK NORMAL NO FAULTS DISPLAYED. PERFORMED BITE TEST ON #1 AND #2 EIVMU IAW A330AMM 73-25-34-740-820A TEST OK ON BOTH EIVMU.(STUECK, MARK L 812635) COMPUTER, SLAT/ OFF 33-2751-9-0004 04776 ON 33-2751-9-0004 12241 UNIT, COMMAND S OFF 33-2751-9-0001 04253 ON 33-2751-9-0001 01128

Part: NONE — NONE · airframe 25,587 hrs · 4,003 cycles

ETOPS - APU FAULT UPON LANDING AUTO SHUT DOWN WILL NOT START.// T/S PER A330 TSM 49-00-00-810-881-A. FOUND IGNITION PLUG (59KA31 )IGNITION EXCITER FAULT. R/R EXCITER PER A330 AMM 49-41-13. R/R 5 O'CLOCK POSITION IGNITER PER A330 AMM 49-41-41. TESTS GOOD. OK FOR SVC. EXCITER, IGNITION OFF P/N 33-4941-9-0002 S/N 10784 ON P/N 33-4941-9-0002 S/N 02008

Part: NONE — NONE · airframe 25,209 hrs · 3,940 cycles

SHIP 375 AFTER PARKING AND SHUT DOWN, A/C DOOR WARNING OF PSI IN CABIN. CORRECTIVE ACTION: NO FAULTS FOUND ON LAST LEG AND GROUND REPORT. PERFORMED OPS TEST OF CPC 1&2 PER AMM 21-31-00 AND FOUND NO FAULTS. (6764843)

Part: BUTTON — DIM (FCP) · airframe 24,898 hrs · 3,890 cycles

ETOPS - MULTIPLE PUSH BUTTON SWITCH DIM ON FCP // REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS CHECK GOOD. CAT III LAND TEST PASSED. OK FOR SVC. UNIT, FLIGHT CO OFF P/N 43-2281-9-0002 S/N 01748 ON P/N 43-2281-9-0003 S/N 04154

Part: SEAL — FOD (L2 DOOR) · airframe 24,531 hrs · 3,831 cycles

ATO - LOAD SQUAL @ 2L DOOR. // CLEANED & INSPECTED 2L DOOR. FOUND EXCESSIVE SEALANT ON CENTER SCUFF PLATE SEAM. REMOVED EXCESSIVE SEALANT. PRESSURIZED A/C, NO SQEALS OR LEAKS NOTED ON 2L OR 2R DOORS. A/C IS OK FOR SERVICE IAW A330 AMM 05-53-00.

Part: FILLER — MISSING (RT ELEVATOR) · airframe 24,656 hrs · 3,851 cycles

SHIP 375 FILLER MATERIAL MISSING ON UPPER RIGHT ELEVATOR TRAILING EDGE. CORRECTIVE ACTION: REF A330 SRM 55-21-11-283-015 ,OK TO TO APPLY TEMP REPAIR. SPEED TAPE APPLIED TO RH ELEVATOR TRAILING EDGE UPPER SURFACE REF SRM 51-77-12-911-011. (7265064)

Part: PIN — MALFUNCTIONED (L3 DOOR SLIDE) · airframe 23,567 hrs · 3,691 cycles

SHIP 375 3L DOOR SLIDE DISARM LEVER SAFETY PIN DOES NOT LOCK INTO SLOT. CORRECTIVE ACTION: LUBRICATED PIN LOCKING MECHANISM. (4085866)

Part: PIN — UNSECURE (L3 DOOR) · airframe 23,560 hrs · 3,690 cycles

SHIP 375 3L DOOR SAFETY PIN WILL NOT STAY IN. CORRECTIVE ACTION: OPS CHECK 3L DOOR SAFETY PIN. FOUND PIN PROPERLY ENGAGES. (4085850)

Part: OIL COOLER — DEFECTIVE (NR 1 ENGINE) · airframe 23,344 hrs · 3,655 cycles

ETOPS - ON PDC, FOUND #1 ENG AIR/OIL HEAT EXCHANGE 4073265 LEAKING OIL INTERNALLY. // REMOVED #1 ENG AIR/OIL HEAT EXCHANGER PER AMM 79-21-51-000-803-A 13 FEB 2021 INSTALLED #1 ENG AIR OIL HEAT EXCHANGER PER AMM 79-21-51. OPS CHECK AND LEAK CHECK GOOD. COOLER, OIL-AIR OFF 43-7921-9-0001 41387 ON 43-7921-9-0001 41492

Part: SEAT TRACK — CORRODED (FRAMES 37.4-76) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y450, FR 76-FR 37.4 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SKIN — CORRODED (FRAMES 77-80) · airframe 22,954 hrs · 3,598 cycles

AFT FUSELAGE SKIN BETWEEN FR 77-FR 80, BETWEEN STRINGER 40L AND STRINGER 43L FOUND MULTIPLE FASTENER HEADS CORRODED. CORRECTIVE ACTION: REFER TO NRC 100-017 SVO: 37226895 FOR PAINTING STRIPPING CARRIED OUT. ALL CORRODED FASTENERS REMOVED AND REPLACED, AS PER SRM. INSPECTED, NO CRACKS.

Part: CONTROL UNIT — MALFUNCTIONED (DOORS) · airframe 22,954 hrs · 3,598 cycles

PFR FAULTS: CLASS 2, HARD, PSCU (5MJ), SOURCE: PSCU. CORRECTIVE ACTION: PSCU FIN 5MJ REPLACED, IAW AMM 52-71. BITE TEST OF THE PSCU CARRIED OUT, AMM 52-71-00-740-801 TEST PASSED.

Part: SKIN — CORRODED (FRAME 76) · airframe 22,954 hrs · 3,598 cycles

CORROSION, AFT FUSELAGE SKIN AT FR 76, BETWEEN STRINGER 48L AND STRINGER 51L FOUND MULTIPLE FASTENER HEADS CORRODED. CORRECTIVE ACTION: REFER TO NRC 100-017 SVO: 37226895 FOR PAINT STRIPPING CARRIED OUT. ALL CORRODED FASTENERS REMOVED, AS PER SRM. INSPECTION FOUND NIL CRACK & NIL CORROSION. FASTENERS INSTALLED, AS PER SRM REL 108.00 REFER TO NRC 100-017 SVO: 37226895 FOR SURFACE PROTECTION AND PAINTING. REFER TO NDT REPORT NR HAWAIIAN AIR/0112/20 FOR WORK CARRIED OUT.

Part: SEAT TRACK — CORRODED (FRAMES 47-53.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-2462 FR 47-FR 53.2 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 26-37.4) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-450, FR 26-FR 37.4 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PERFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 26-37.4) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y2462 FR 26-FR 37.4 EXFOLIATED. CORRECTIVE ACTION: MAIN DECK COMPARTMENT SEAT TRACK AT Y2462, FR 26-FR 37.4. REPLACED AS PER SRM, APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 38-39.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-1456, FR 38-FR 39.2 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 19-26) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y450 FR 19-FR 26 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 47-53.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK BETWEEN FR 47-FR 53.2 (-Y450) EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK BETWEEN FR 40-47 (Y1959) EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 47-53.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK BETWEEN FR 47-FR 53.2 RT -Y1959 FOUND EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PEFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 28-37.4) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-1959, FR 28-FR 37.4 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND APPLIED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 38-39.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y450, FR 38-FR 39.2 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-450, FR 40-FR 47 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PEFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 38-39.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-450 FROM FR 38-FR 39.2 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PERFORMED BONDING RESISTANT CHECKS, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-1959 FR 40-FR 47 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 59-68) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 59-FR 68 (Y450) FOUND EXFOLIATED AT MULTIPLE LOCATION. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 53.2-54) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK FROM FR 53.2-54 RT, Y-1959 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 30-35) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT -Y1552.5 FR 30-FR 35 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 53.2-54) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK FROM FR 53.2-FR 54 LT, Y1959 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: ROLLER — CORRODED (AFT CARGO) · airframe 22,954 hrs · 3,598 cycles

AFT CARGO ROLLER TRACK ASSEMBLY FOUND CORROSION 1/2" X 1/2" SIZE AT FR 60 -Y1470. CORRECTIVE ACTION: AFT CARGO ROLLER TRACK ASSEMBLY REPLACED, AS PER AMM 25-51.

Part: SEAT TRACK — CORRODED (FRAMES 59-62) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 59-FR 62 (Y1959) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 47-53.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK FROM FR 47-53.2 LT , Y1959 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. CARRIED OUT APPLICATION OF CORROSION INHIBITOR ON SEAT TRACK AND CARRIED OUT BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 62-72) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 62-FR 72 (Y1959) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PEFORMED BONDING RESISTANCE CHECK.

Part: ROLLER — CORRODED (FWD CARGO) · airframe 22,954 hrs · 3,598 cycles

FWD CARGO ROLLER TRACK ASSEMBLY FOUND CORROSION SIZE 1" X 1/4" AT FR 37.3 (Y140). CORRECTIVE ACTION: FWD CARGO ROLLER TRACK ASSEMBLY REPLACED, AS PER AMM 25-51.

Part: SEAT TRACK — CORRODED (FRAMES 38-39.2) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK AT Y-1959, FR 38-FR 39.2 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 53.2-53.3) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK FROM FR 53.2-53.3 RT, Y-950 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 68-72) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 68-FR 72 (Y450) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PEFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 53.2-53.3) · airframe 22,954 hrs · 3,598 cycles

FOUND SEAT TRACK BETWEEN FR 53.2-FR 53.3 LT, Y450 EXFOLIATED. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 59-62) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 59-FR 62 (-Y1959) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT APPLICATION OF CORROSION INHIBITOR ON SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 68-72) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 68-FR 72 (-Y450) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 59-68) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 59-FR 68 (-Y450) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 55-59) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 55 TO 59 (-Y450) FOUND EXFOLIATED AT MULTIPLE LOCATION. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PEFORMED BONDING RESISTANCE CHECK, AS PER AMM 20-28.

Part: SEAT TRACK — CORRODED (FRAMES 55-59) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 55-FR 59 (Y450) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 68-72) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 68-FR 72 (-Y1959) FOUND EXFOLIATED AT MULTIPLE LOCATIONS. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR ON SEAT TRACK AND PEFORMED BONDING RESISTANCE CHECK.

Part: SEAT TRACK — CORRODED (FRAMES 55-59) · airframe 22,954 hrs · 3,598 cycles

SEAT TRACK BETWEEN FR 55-FR 59 (-Y1959) FOUND EXFOLIATED AT MULTIPLE PLACES. CORRECTIVE ACTION: CARRIED OUT REPLACEMENT OF SAID SEAT TRACK, IAW SRM. APPLIED CORROSION INHIBITOR AND PERFORMED BONDING RESISTANCE CHECK.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE)

REPORTED BY PILOT 00401401 HNL 19AUG20. AIRCRAFT HAD A SOUR OIL TYPE SMELL ON DEPARTURE THAT SLOWLY DISSIPATED AS WE CLIMBED TO FL 320. THE SMELL RETURNED ON DESCENT. FOUND #2 ENGINE OIL OVERSERVICED, DRAINED 2 QTS OIL FROM #2 ENGINE OIL TANK (16 JUL 20). ACCOMPLISHED ECS DECON AMM 21-00-00, ENGINE 1 AND 2 RUN ACCOMPLISHED AND APU. NO DEFECTS NOTED, OK FOR SERVICE. LOG-PAGE UPDATED @ 19AUG20 1037 UTC.

Part: VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 22,939 hrs · 3,595 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 1 BLEED NOT CLOSED. INSTALLED ENG #1 PRV PER AMM 36-11-52. OPS CHECK, LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FIRE WARNING) · airframe 33,602 hrs · 3,542 cycles

DURING ENG FIRE TEST MASTER CAUTION LIGHT WONT COME ON WITH SECOND #2 ENG WARNING. // PERFORMED BITE TEST OF ENG & OVERHEAT DETECTION PER AMM 26-12-00, NO DEFECTS NOTED, OK FOR SERVICE.

Part: COVER — MISSING (FLAP TRACK) · airframe 22,240 hrs · 3,486 cycles

DURING PDC FOUND COVER ON FLAP TRACK FAIRING 631CB MISSING. APPLIED SPEED TAPE AND DEFERRED PER CDL 57-07 UNTIL FLAP TRACK FAIRING COVER IS AVAILABLE TO REPLACED. LP 7240659

Part: COVER — MISSING (FLAP TRACK) · airframe 22,236 hrs · 3,485 cycles

OPEN - ON PDC FOUND COVER ON FLAP TRACK FAIRING (631 CB) MISSING. (RIGHT WING).

Part: SKIN — DAMAGED · airframe 19,943 hrs · 3,143 cycles

ETOPS SIGNIFICANT SYSTEM - PER LINE SERVICE, GROUND AIR CONDITION HOSE DETACHED FR. A/C & DAMAGED PANEL 192JB. IN 3 PLACES. FOUND DENT PERFORATION OF OUTER SKIN PANEL IN SANDWICH AREA, 19 1/2" AFT OF FWD EDGE. DAMAGE 1 1/2"L X 1/2" .065" DEPTH. PERFORMED INSPECTION PER FIGURE 33 53-35-00-283-001. PERFORMED TEMPORARY REPAIR 53-35-00-300-002. FIGURE 001.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,301 hrs · 3,053 cycles

ETOPS SIGNIFICANT SYSTEM - ON LANDING ECAM FOR R THRUST REV FAULT. PERFORMED TEST OF THRUST REVERSER DEPLOYMENT AND STOWAGE ON RT TR PER AMM 78-31-00-740-802-A, NO DEFECTS NOTED. OK FOR SVC.

Part: FUEL LINE — CHAFED (NR 1 ENGINE) · airframe 17,868 hrs · 2,836 cycles

ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE FUEL LINE FROM HEAT EX-CHANGER CHAFED THRU, LEAKING. REMOVED AND REPLACED FUEL LINE AT HEAT EX-CHANGER IAW AMM 73-11. IDLE RUN LEAK CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 17,408 hrs · 2,768 cycles

ETOPS SIGNIFICANT SYSTEM - 1 MINUTE AFTER TAKE OFF AT ABOUT 1,500 FT EXAM FUEL R CTRL PUMP LO OR ILLUMINATED,TURNED OFF R CTRL PUMP.// PER TSM TASK 28-26-00-810-826A. PERFORMED FCMC SYSTEM TEST OK. VISUAL INSPECTED GFI CONNECTOR NO TROUBLE FOUND. R CTR FUEL PUMP TEST OK PER AMM 28-51-00-710-801.A/C OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,868 hrs · 2,678 cycles

ETOPS SIGNIFICANT SYSTEM - AIR BLEED 1 FAULT ON TAXI OUT. RESET ENG 1 BLEED PER MOC. ENG 1BLEED FUNCTION NORMAL. PERFORMED BITE OF BUC 1. NO FAULTS EXISTING. SUSPECT FAULT COINCIDED WITH PACK FAULT, REF LOG 5385779 AND 0863736. OK FOR SER.

Part: EXCITER — MALFUNCTIONED (APU) · airframe 16,852 hrs · 2,678 cycles

ETOPS SIGNIFICANT SYSTEM - BRAKE RIDER REPORTS APU WON’T START. REMOVED AND REPLACED IGNITER PLUGS. NO HELP PER AMM 49-41-41. TROUBLESHOT PER TSM 49-41-00-810-804-A 'APU AUTO SHUT DOWN NO FLAME IGNITION EXCITER FAULT'. REMOVED AND REPLACED APU EXCITER BOX PER AMM 49-41-38. APU OPS CHECK NORMAL. A/C OK FOR SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (BLEED AIR SYS) · airframe 16,776 hrs · 2,668 cycles

ETOPS SIGNIFICANT SYSTEM - DURING TAXI OUT OBSERVED ECAM: AIR ENG 1 BLEED FAULT. PER MOC PERFORMED RESET, FAULT CLEARED. REMOVED AND REPLACED ENG 1 PRESSURE TRANSDUCER PER AMM 36-11. OPS CK GOOD.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 16,560 hrs · 2,636 cycles

WHILE ON THE LINE IN HNL, MAINTENANCE FOUND DAMAGE COMMON TO THE INNER SKIN OF THE AFT CARGO DOOR (P/N: F5237231500000, FTN: 4E4870). THE DAMAGE CONSISTS OF A DENTED GOUGE LOCATED BETWEEN FR 63 AND FR 63A ON THE AFT CARGO DOOR. THERE IS AN EXISTING REPAIR COMMON TO THE SAME INNER SKIN BETWEEN FR 62 AND FR 62A AS SEEN IN FIGURE 2 OF THE ER/A AND DISPOSITIONED PER ER/A 542637-14. ACCOMPLISHED PERMANENT REPAIR PER SRM 52-30-00-300-008 AND ER/A 572854-14. LP 4961016

Part: LIGHT — BROKEN (COCKPIT) · airframe 16,221 hrs · 2,588 cycles

ON PARKING - ELECTRICAL SPARK FROM ABOVE CAPTAIN'S SEAT WITH AUDIO "POP" AND VISIBLE SPARK. INSPECTED FLIGHT DECK WITH VERBAL FROM CREW. FOUND BROKEN DOME LIGHT ABOVE CAPT SEAT. RELAMPED CAPT SIDE DOME LIGHTS WITH MPN 8GH004554-28 PER AIPC 33-12-08-01A ITEM 110 AND AMM 33-12-11. OPS CHK OK. OK FOR SVC.

Part: UNKNOWN — ODOR (CREW REST) · airframe 16,221 hrs · 2,588 cycles

LOWER CREW REST SMELLS OF SMOKE, ELECTRICAL. INSPECTED CREW REST LIGHTS/CIRCUIT BREAKERS, EYEBALL VENTS, DOORWAY AND SURROUNDING AREA. NO BURNING SMELLS NOTED. OK FOR SVC.

Part: HEATER — ODOR (CABIN) · airframe 10,684 hrs · 2,563 cycles

ON CLIMB FLIGHT ATTENDANTS SMELLED ELECTRICAL ODOR TURNED OFF FLOOR HEATERS DISSIPATED IN FEW MINS. VERIFIED 2L FLOOR HEATER CAUSING ELECTRICAL BURNING SMELL OK TO CONTINUE PER MEL. MAINTENANCE PROCEDURES C/W, PLACARD INSTALLED, LIDS UPDATED. C/B H07 PULLED AND COLLARED.

Part: AUTOPILOT SYS — DISCONNECTED (COCKPIT) · airframe 15,949 hrs · 2,547 cycles

SEVERE TURBULENCE ENCOUNTERED DURING CRUISE AT FL 390 FOR APPROX 4 SECONDS, SPEED MACH .81 VIOLENT BUT MINOR PITCH AND ROLL DEVIATIONS RESULTING IN AUTOPILOT DISCONNECT. DEVIATIONS +/- 15 KNOTS. ACCOMPLISHED AMM TASK 05-51-17-200-801-A FOR EXCESSIVE TURBULENCE. ACMS LOAD REPORT 15/35 REPORTS VRTA LOADS ARE ACCEPTABLE AND DO NOT REQUIRE FURTHER INSPECTIONS. ACCOMPLISHED TASK 05-51-44-200-801-A FOR THE PITCH AND ROLL LOAD. NO FURTHER INSPECTIONS NOTED. NO LOAD 15/35 REPORT AUTO GENERATED. AFS SYSTEM TEST OK, PER AMM 22-96-00-740-801-A. A/C OK FOR SVC.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 15,695 hrs · 2,507 cycles

EMERGENCY LIGHTS COME ON IN FLIGHT AND WON'T RESET. RESET POWER.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 15,562 hrs · 2,486 cycles

THE L3 DOOR EXIT SIGN LENS DETACHED FROM THE WALL. REPLACED THE EXIT SIGN LENS.

Part: GENERATOR — FAULTED (APU) · airframe 15,465 hrs · 2,470 cycles

APU GENERATOR FAULT. REPLACED THE APU GENERATOR IAW AMM 24-23-51. OPS & LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN SMOKE) · airframe 13,319 hrs · 2,157 cycles

WARNING MESSAGE FOR SMOKE CABIN REST CAME ON MOMENTARY IN COCKPIT. SMOKE TEST OF LDCU AND TEST PASSED. OK FOR SERVICE IAW AMM 26-16-00.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 13,298 hrs · 2,154 cycles

WARNING MESSAGE, SMOKE CABIN REST, ILLUMINATED MOMENTARILY IN COCKPIT. LDCRM AIR FLOW LOW ANNUNCIATOR ILLUMINATED AND STAYED ON. PERFORMED A TEST OF THE LDCRM SMOKE DETECTION SYSTEM, ALL TESTS PASSED. RESET VC, NO FAULTS NOTED, OK FOR SERVICE.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 13,114 hrs · 2,124 cycles

WHILE RUNNING EPSU TEST BEFORE SLIDE REPLACEMENT, RECEIVED AN ESCAPE SLIDE LIGHT, EPSU 11WL DOOR 1 FAULT. RED EXTERIOR LED ALSO CAME ON DURING TEST OF EPSU. REMOVED & REPLACED THE L1 DOOR SLIDE IAW AMDS 2561-9403. SAFETY PINS REMOVED AND STOWED. DOOR ARMED. TROUBLESHOT IAW TSM 25-62-00-810-825-A. OPS CHECKED GOOD. FAULTS DISAPPEARED. OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 12,139 hrs · 1,982 cycles

EMERGENCY LIGHT LENS OVER THE R3 DOOR IS BROKEN. REPLACED THE LENS.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 12,111 hrs · 1,978 cycles

EMERGENCY EXIT LIGHT LENS OVER THE R3 DOOR DETACHED. REPLACED THE LENS IAW AMM 33-51-17. OK FOR SERVICE.

Part: ENGINE — FIRE (NR 1) · airframe 11,909 hrs · 1,951 cycles

SUPPLEMENTAL: AIRCRAFT 375 EXPERIENCED A NBR 1 ENGINE TAIL PIPE FIRE AFTER LANDING IN SEA, PRECEDING THIS WAS A NBR 1 ENGINE CONTROL SYSTEM FAULT. CORRECTIVE ACTION: REPLACED PYLON FAIRINGS, TAIL CONE FAIRING, NBR 1 AND 2 SPOILER PANELS, LEFT INBOARD AND OUTBOARD FLAPS, NBR 2 MOVEABLE AND NBR 3 FIXED FAIRING AND ASSOCIATED PARTS. REPLACED NBR 1 ENGINE. LP 4083129.

Part: WARNING MESSAGE — ILLUMINATED · airframe 11,881 hrs · 1,945 cycles

SUP - ON FINAL TO SEATAC ECAM MESSAGE "ENG 1 CTL SYS FAULT". // REPLACED PYLON FAIRINGS, TAIL CONE FAIRING, NBR 1 AND 2 SPOILER PANELS, LEFT INBOARD AND OUTBOARD FLAPS, NBR 2 MOVEABLE AND NBR 3 FIXED FAIRING AND ASSOCIATED PARTS. REPLACED NBR 1 ENGINE.

Part: OXYGEN BOX — OUT OF POSITION (LAVATORY) · airframe 11,881 hrs · 1,944 cycles

WHILE PERFORMING A PAX OXYGEN MASK DROP TEST, FOUND THE AFT RT LAVATORY MASKS DID NOT DROP. REMOVED THE PIN, REPOSITIONED OXYGEN MASK BOX.

Part: ENGINE — FIRE (NR 1) · airframe 11,881 hrs · 1,945 cycles

ON FINAL TO SEATAC ECAM MESSAGE "ENG 1 CTL SYS FAULT" AVOID LARGE THRUST LATER RED MSG ENG 1 N2 OVR LIMIT CHANGES THEN WHEN TOUCHING DOWN FLAMES ON ENG 1 = SURGING "NO ECAM MESSAGES" NO FIRE WARNING TOWER CONFIRMED ENG 1 ON FIRE F/O PULLED FIRE HANDLE = DISCHARGED AGENT 1. // REMOVED #1 ENG #1 FIRE BOTTLE ASSY PER HAL A330 AMM 26-21-41. INSTALLED SQUIB CARTRIDGE IN BOTTLE PER HAL AMM 26-21-41. CKS GOOD. INSTALLED #1 BOTTLE #1 ENG PER HAL AMM 26-21-41. TEST GOOD.

Part: FMU — LEAKING (LT ENGINE) · airframe 10,645 hrs · 1,726 cycles

FUEL DRIPPING FROM LEFT ENGINE. REPLACED FMU, OPS AND LEAK CHECKS GOOD.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 10,201 hrs · 1,646 cycles

R3 DOOR EXIT SIGN LOOSE. SECURED THE EXIT SIGN.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 9,097 hrs · 1,453 cycles

NR 2 ENGINE CONTROL SYS FAULT ECAM DURING DESENT, ACCOMPLISHED EMAC ACTIONS. NR 2 EEC ACCOMPLISHED TASK 73-21-78-810-816A (P30 PRESSURE) NO DEFECTS NOTED. FOUND BITE TEST NR 2 EEC CHANNEL A AND CHANNEL B BITE TEST OK. OK FOR SERVICE.

Part: BLEED VALVE — FAULTED (APU) · airframe 8,871 hrs · 1,414 cycles

ETOPS, DURING START INTERMITTENT APU BLEED FAULT AT ENGINE SHUT DURING BLOCK IN AGAIN OBSERVED APU BLEED FAULT. REPLACED APU BLEED VALVE PER AMM 49-51-51 OPS CHECK LEAK CHECK OK OK FOR SERVICE VALVE, LOAD ASS OFF 33-4950-9-0002 01614 ON 33-4950-9-0002 01883

Part: CIRCUIT BREAKER — TRIPPED · airframe 8,862 hrs · 1,412 cycles

MULTIPLE CIRCUIT BREAKERS TRIPPED.

Part: WARNING LIGHT — ILLUMINATED (A/C PACK) · airframe 8,645 hrs · 1,377 cycles

NR 1 A/C PACK REGULATOR FAULT, NR 1 A/C PACK RAM DOOR CLOSED ECAM DISPLAYED DURING DESCENT. RESET AEVC AND PACK CONT 1 RESET SWITCH, SYSTEM TEST ECS,TESTED OK. IAW AMM 21-26-00-710-803. OPS NORMAL.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 7,131 hrs · 1,148 cycles

ATB - HYD YELLOW SYS LOW QUANTITY/PRESSURE. ECAM SHOWS FLUID STILL PRESENT IN YELLOW SYSTEM. O-RING ON YELLOW HP MANIFOLD IN RIGHT WHEEL WELL LEAKING. REMOVED AND REPLACED O-RING ON YELLOW HP MANIFOLD PER AMM 29-13-53-400-803-A. OPS/LEAK CK GOOD OK FOR SVC.

Part: FUEL SYS — MALFUNCTIONED · airframe 991 hrs · 158 cycles

FUEL IMBALANCE IN FLIGHT, FUEL MIGRATING. REPAIR IN WORK.