N384HA

Part: LIGHT SYS — FAULTED (ZONE 200) · airframe 58,266 hrs · 9,087 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED WHILE IN CRUISE UNABLE TO RESET WITH EMER EXIT LT SWITCH. LIGHTS REMAINED ILLUMINATED WITH SWITCH IN "OFF" OR "ARM". GROUNDED - YES. OPS CHECK OF CABIN EMER LIGHTS C/O AS PER AMM 33-51-00-710-812-A. FOUND SATIS.

Part: COUPLING — LEAKING (ZONE 100) · airframe 58,034 hrs · 9,045 cycles

ETOPS - LINE SVC REPORTED FUEL DRIPPING FROM TRIM PIPE DRAIN MAST. REPLACED FUEL TRANSFER HOSE COUPLING PER AMM 28-27-47. LEAK CHK GOOD OK FOR SVC

Part: SELECTOR VALVE — LEAKING (ZONE 700) · airframe 55,692 hrs · 8,677 cycles

HYD B RESEVR LO LVL. HYD B ENG 1 PUMP NO PRESS. LEAK FOUND ON BRAKE AUTOMATIC SELECTOR VALVE. INSTALLED NEW PACKINGS ON HYD. PIPE UNIONS, IAW AMM 32-42-13-400-801-A. BLED NORMAL AND ALTERNATE BRAKE SYSTEMS. OPS TEST NORMAL AND ALTERNATES SYTEM GOOD. NO LEAKS NOTED. BLUE SYS. SERVICED. DRY MOTORED ENG 1 IAW AMM 71-00-00-720-828-A. HYD B ENG 1 PUMP. PRESS GOOD. NO FAUTS FOUND.

Part: FILLER — DAMAGED (LP COMPRESSOR) · airframe 55,372 hrs · 8,630 cycles

ETOPS - LP COMPRESSOR ANNULUS FILLER #3 ON #1 ENG DAMAGED. REMOVED/ REPLACED #3 ANNULUS FILLER ON #1 ENG PER T/C 330-723-100-R9-1-1. SECURITY CHECK GOOD. OK FOR SVC.

Part: MOTOR — FAULTY (APU STARTER) · airframe 55,248 hrs · 8,613 cycles

ETOPS - APU WILL NOT START. REMOVED AND REPLACED APU STARTER MOTOR I.A.W. AMM 49-42-51-400-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK TO CONTINUE.

Part: TRANSFER SYS — FAULTED · airframe 55,052 hrs · 8,577 cycles

ETOPS - FUEL T TANK XFR FAULT. FOUND FUEL TRIMTK ISOL VALVE (702QN) FAILED OPEN. REMOVED AND REPLACED SMA 702QN PER AMM 28-27-52. OPS/VALVES TEST OK. OK FOR SVC.

Part: CONTROL VALVE — FAULTED (NR 1 A/C PACK) · airframe 55,040 hrs · 8,575 cycles

ETOPS - AIR PACK 1 REG FAULT PACK 1 IN BYPASS MODE ECAM APPEARED AT THE GATE WITH ENGINES SHUTDOWN. PERFORMED REMOVAL OF FLOW CONTROL VALVE IAW AMM 21-51-51-000-801-A C/B PULLED AND COLLARED F02 K04 R08 R07 T08 A67 MN 024554. INSTALLED FLOW CONTROL VALVE PER AMM 21--51-51-400-801-A. RESET C/B'S F02 K04 R08 R07 T08 A67. OPS AND LEAK CHECK GOOD. A/C OK FOR SVC.

Part: O-RING — LEAKING (HYD LINE) · airframe 54,536 hrs · 8,496 cycles

ETOPS - FOUND HYDRAULIC LEAK FROM GREEN MANIFOLD- BRK LINE- LEADING EDGE FLAPS. REPLACED O-RING ON GREEN MANIFOLD LINE LABELED L.E. FLAPS PER AMM 29-11-53. LEAK CHECK GOOD OK FOR SVC.

Part: HANDSET — MALFUNCTIONED (ZONE 200) · airframe 54,355 hrs · 8,468 cycles

ETOPS - 1L FLIGHT ATTENDANT HANDSET - PA FUNCTION EXTREMELY LOW VOLUME. REPLACED HANDSET ASSY PER AMM 23-73-44. OPS CK OK. OK FOR SERVICE

Part: HYDRAULIC LINE — LEAKING (HYD MANIFOLD) · airframe 53,937 hrs · 8,403 cycles

ETOPS - GREEN HYD LOW QUANT. ECAM ON FINAL AFTER SELECTING FLAPS 2, PRESSURE NORMAL. PER CREW CONFIRMED GREEN HYD PUMPS TURN OFF BEFORE SYSTEM GOT EMPTY AND WAS STILL PRODUCING PRESSURE. FOUND LEAK AT 5105JM MANIFOLD HYD LINE. REMOVED AND REPLACED PACKING PER AMM 29-11-53. LEAK CHECK GOOD. SEVICED HYD PER AMM 12-12-29. RESET 5JR. OK FOR SVC.

Part: BLEED VALVE — STUCK (NR 1 ENGINE) · airframe 53,766 hrs · 8,673 cycles

ETOPS - FOUND ENGINE 1 BLEED VALVE STUCK OPEN WHILE PERFORMING TC# A2022-17-08-PART09-LH ITEM 4 OPS CHECK OF DOSING SIGNAL TO ISO SOLENOID FROM BLEED/ FIRE PUSH BUTTON SWITCH. REMOVED ENG 1 BLEED VALVE PER AMM 36-11-52-000-804-A. INSTALLED BLEED VALVE ON #1 ENG PER AMM 36-11-52-400-804-A LEAK CK AND OPS CK GOOD OK FOR SVC.

Part: FIRE LOOP — FAULTED (NR 2) · airframe 53,105 hrs · 8,274 cycles

ETOPS - DURING PDC FOUND ENG 2 FIRE LOOP B FAULT. REPLACED FIRE DET UNIT FOR ENG 2. OPS CHECK GOOD. TEST PASSED AMM 26-12-34

Part: BONDING STRAP — BROKEN (ENG GEARBOX) · airframe 52,534 hrs · 8,185 cycles

ETOPS - WHILE OPENING ENG #1 FAN COWL IN PREPARATION FOR BORESCOPE FOUND GEARBOX BONDING STRAP BROKEN. REPLACED BONDING STRAP PER AMM 72-61-00 A/C OK TO CONTINUE PER WORK PERFORMED

Part: FASTENER — SHEARED (OIL SIGHT GLASS) · airframe 52,214 hrs · 8,132 cycles

ETOPS - ON #2 ENG, FASTENER ON THE IDG OIL QUANTITY SIGHT GLASS SHEARED OFF. SCREW THREADS STILL IN THE BOTTOM RIGHT HOLE. REF LP 1013577-2 FOR REMOVAL AND REPLACMENT OF IDG. REMOVED #2 ENGINE S/N 41270. IDG IN SERVICEABLE CONDITION FOR S/N 42396. INSTALLED #2 IDG PER AMM 24-21-51. OPS AND LEAK CHECK GOOD OK FOR SVC.

Part: PUMP — DAMAGED (ENGINE OIL) · airframe 51,972 hrs · 8,097 cycles

ETOPS - DURING TASKCARD 330-792000-R1-1-2 FOUND DAMAGE ON PUMP & PRESSURE FILTER HOUSING. REMOVED RH ENG OIL PUMP PER AMM 78-22-51 21996. INSTALLED RH ENG OIL PUMP PER AMM 79-22-51. OPS CHECK GOOD NO LEAK DETECTED. OK FOR SERVICE.

Part: SERVO VALVE — LEAKING (RT MLG) · airframe 51,365 hrs · 50,403 cycles

OTHER - DURING WALK AROUND FOUND LEAK AT RH MLG. REMOVED AND REPLACED RH MLG SERVO VALVE PER AMM 32-43-27 UP TO AND INCLUDE STEP 4(B) PENDING C/B, BLEED, LEAK CK. 22236. CLOSED C/B, BLEED ALT BRAKES OPS CHECK GOOD, NO LEAKS NOTED. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,924 hrs · 7,783 cycles

APU START-APU AUTO SHUTDOWN ON START. REMOVED AND REPLACED APU STARTER PER AMM 49-42-51. OPS CHECK GOOD, OK FOR SERVICE. NO LEAKS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,549 hrs · 7,563 cycles

ETOPS - AFTER LANDING ENG 2 OIL CHIP DETECTED ILLUMINATED. PERFORMED TSM 79-80-00. REPLACED SCAVENGE OIL FILTER PER 79-22-45-920-801-A. OPS CHECK, LEAK CHECK OK. OK FOR SVC.

Part: NONE — NONE · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FR 40 RHS FASTENER HOLE & H260 FOUND WITH CRACK INDICATION. CORRECTIVE ACTION: ACCOMPLISHED AS PER PRI 605591-14. REPAIR INSTRUCTIONS ACCOMPLISHED IN ACCORDANCE WITH ER/A 605591-14. (2629504)

Part: NONE — NONE · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FR 40 LHS FASTENER HOLE #H262 FOUND WITH CRACK INDICATION. CORRECTIVE ACTION: ACCOMPLISHED AS PER ATTACHED AIRBUS DOSSIER 811717 DATED 23 JAN 2023 & SB 57-3129 REV 03. REPAIR INSTRUCTIONS ACCOMPLISHED IN ACCORDANCE WITH ER/A 605704- 14. (2629496)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION BET FR 59 - 62 -Y1959. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR59 TO FR62, -Y1959 REPLACED. (2626727)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION BET FR 62 TO 72, Y1959. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR62 TO FR72, Y1959 REPLACED. (2626725)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 MAIN DECK LONGITUDINAL BEAM FOUND BADLY CORRODED AT LOCATION FRAME 75 - FR 78, -Y445 (RIGHT SIDE). CORRECTIVE ACTION: MAIN DECK LONGITUDINAL BEAM AT FRAME 75 - FRAME 78, -Y445 (RIGHT SIDE) REPLACED. (2627128)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION FR 80/82, BETWEEN - Y1137-1. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT FR 80/82, BETWEEN -Y1137.1 AND -Y1447.8( RIGHT HAND SIDE) REPLACED. (2626729)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHHIP 384 FOUND SEAT TRACK CORROSION AT RH -Y2426 FR 25.5 TO 37.5. CORRECTIVE ACTION: ABOVE SEAT TRACK REPLACED. INSTALLATION CHECK SATISFACTORY. (2627181)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 MAIN DECK LONGITUDINAL BEAM FOUND BADLY CORRODED AT LOCATION FRAME 75 - FRAME 80/82, -Y450 (RIGHT SIDE). CORRECTIVE ACTION: MAIN DECK LONGITUDINAL BEAM AT FRAME 75-FRMA 80/82, -Y450(RIGHT SIDE) REPLACED. (2626735)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION LEFT SIDE FRAME 80/ 82 - FRAME 79, STRINGER LEVEL 26LH, UPPER SIDE. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT LEFT SIDE FRAME 80/82 TO FRAME 79, STRINGER LEVEL 26LH, UPPER SIDE REPLACED. (2627272)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 Z SECTION LH CORNER BET Y1137.1 & Y1447.8 AT FR 80/82 FOUND CRACKED. TO REPLACE Z SECTION. CORRECTIVE ACTION: Z SECTION LEFT HAND CORNER BETWEEN Y1137.1 AND Y1447.8 AT FR 80 / 82 REPLACED. (2627170)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 MAIN DECK Z-SECTION FOUND CRACK AT LOCATION LEFT SIDE FRAME 80/ 82 - FRAME 79, STRINGER 26LH, BOTTOM SIDE. CORRECTIVE ACTION: MAIN DECK Z-SECTION AT LEFT SIDE, FRAME 80/82-FRAME 79, STRINGER 26LH REPLACED. (2626732)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH CORROSION BETWEEN FR 59 TO FR 67, Y450. CORRECTIVE ACTION: SEAT TRACK BETWEEN FRAME 59 TO FRAME 67, Y 450 REPLACED. (2627142)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION AT -Y450, BET FR 72 TO FR 75. TO REPLACE SEAT TRACK. CORRECTIVE ACTION: SEAT TRACK AT -Y450, BETWEEN FR 72 TO FR 75 REPLACED. (2627264)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH CORROSION BET FR 53.6 TO FR 54, -Y450. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR 53.6 TO FR 54, -Y450 REPLACED. (2627251)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION BET FR 67 TO FR 72 Y450. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR 67 TO FR 72, Y450 REPLACED. (2627254)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION BET FR 62 TO FR 72 - Y1959. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR 60 TO FR 72, -Y 1959 REPLACED. (2627134)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION AT Y450, BET FR 72 TO 75. CORRECTIVE ACTION: SEAT TRACK AT Y450, BETWEEN FR72 TO FR 75 REPLACED. (2626728)

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND CORRODED BET FR 59 - 67 -Y450. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR59 TO FR67, -Y450 REPLACED. (2626723)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 SEAT TRACK FOUND WITH EXFOLIATION CORROSION BET FR 55 - FR 59 - Y450. CORRECTIVE ACTION: SEAT TRACK BETWEEN FR55 TO FR59 -Y450 REPLACED. (2627247)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FOUND SEAT TRACK CORROSION AT RH -Y450 FR 25.5 TO FR 37.5. CORRECTIVE ACTION: ABOVE SEAT TRACK REPLACED IAW SRM 51-72-11 AND SRM 51-42-11. (2612095)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FOUND SEAT TRACK CORROSION AT LH Y1959 FR 25.5 TO 37.5. CORRECTIVE ACTION: SEAT TRACK REPLACED IAW SRM 51-72-11 AND SRM 51-42-11. (2612089)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FOUND SEAT TRACK CORROSION AT LH Y450 FR 25.5 - FR 37.35. CORRECTIVE ACTION: ABOVE SEAT TRACK REPLACED IAW SRM 51-72-11 AND SRM 51-42-11. (2612097)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 46,439 hrs · 7,238 cycles

SHIP 384 FOUND SEAT TRACK CORROSION AT LH Y1456 FR 25.5 - 37.5. CORRECTIVE ACTION: ABOVE SEAT TRACK REPLACED IAW SRM 51-72-11 AND SRM 51-42-11. (2612092)

Part: PUMP — BROKEN (HYD SYSTEM) · airframe 46,382 hrs · 7,229 cycles

ETOPS- NEED TO REMOVE AFT HYD PUMP FOUND RECEPTACLE ON PUMP CRACKED. REPLACED THE AFT HYD PUMP.

Part: SLIDE — FAILED (R3 DOOR) · airframe 46,364 hrs · 7,227 cycles

R3 EPSU BATTERY NO TEST. PERFORMED EPSU SYS TEST FER AMM 33-51-00 FOUND FAULT ATA 256241 ESCAPE SLIDE LT SWITCH/EPSU (16WL) DOOR 3. SLAVED IN NEW EPSU 16WL DOOR 3 IAW AMM 33-51-38. NO HELP. REMOVED AND REPLACED R3 SLIDE IAW AMM 25-62-42. EPSU TEST GOOD.

Part: GENERATOR — LEAKING · airframe 46,042 hrs · 7,177 cycles

ETOPS- DIRYT SOCKS SMELL ON DECENT AND WHEN AT THE GATE WITH APU ON IN SEATTLE. INSPECTED #1 AND #2 ENGINE, RAN ENGINES, NO ODORS. INSPECTED APU, NOTICED ODOR FROM APU BLEED. TROUBLE SHOT PER TSM 05-50-00-810-829-A. TYPE 1. FOUND OIL LEAKING FROM APU GENERATOR. REMOVED AND REPLACED APU GENERATOR PER AMM 24-23-51, AND COMPLETED AMM 24-23-51. OPS CHECK AND LEAK CHECKS, BOTH WERE GOOD. PERFORMED LEVEL A DECONTAMINATION OF THE ECS PER AMM 21-00-00-615-809-A. NO ODORS WERE NOTED. OK FOR SERVICE. APU GENERATOR, OFF PN 33-2423-9-0001, SN 04670. APU GENERATOR, ON PN 33-2423-9-0001, SN 04527.

Part: UNKNOWN — UNKNOWN · airframe 46,439 hrs · 7,238 cycles

SHIP 384 BELT LOADER MADE CONTACT WITH FUSELAGE UNDER BULK CARGO COMPT. CORRECTIVE ACTION: REF ER/A 602297-14. (2418961)

Part: NONE — NONE · airframe 44,993 hrs · 7,013 cycles

ATB - G HYD LEAK MESSAGE SHUT DOWN BOTH ENGINE PUMPS PER EICAM, G HYD LOW LEVEL. PERFORMED BITE TEST OF HSMU PER A330 29-31-00 FAULTED G HYD QTY XMTR G ENG 1PMP/ AND HSMU. PERFOMRED OPS CHK OF AUTOMATIC CONROL OF FIRE SHUT OFF FOR LOW LEVEL ON GREEN SYSTEM PERA330 TASK 29-11-00 PAGE 6 STEP #4 SAYS REPLACE HSMU. M PROCEDURES FOR MEL 29-30-2A REVERSED A/C BACK IN NORMAL CONFIGURATION 534768. R/R HSMU PER A330 AMM 29-11-34. OPS TEST GOOD. ALL INDICATIONS NORMAL. SERVICED HYD, AND RESET C/B 5JR. OK FOR SVC. HYDRAULIC UNIT, OFF 33-2900-9-0003 32010 ON 33-2900-9-0003 00513

Part: NONE — NONE · airframe 44,359 hrs · 6,909 cycles

SHIP 384 EMERGENCY LIGHT COVER AT 3L MISSING. CORRECTIVE ACTION: REPLACED EMER CEILING LT COVER AT 3L DOOR. (9312979)

Part: NONE — NONE · airframe 42,968 hrs · 6,661 cycles

SHIP 384 APU SQUIB DOES NOT ILLUMINATE DURING APU FIRE TEST. CORRECTIVE ACTION: CLEANED CONNECTOR AT APU FIRE BOTTLE 12WFA. OPS TEST PASSED PER AMM 26-13-00. VERIFIED SQUIB AND DISCHARGE LIGHTS ILLUMINATE DURING TEST. (8471879)

Part: NONE — NONE · airframe 42,946 hrs · 6,658 cycles

ETOPS - APU WILL NOT SHUT DOWN WITH APU MASTER SWITCH // REMOVED AND REPLACED RELAYS (FIN:5KD AND 34KD). PER: ESPM 20-46-50. REMOVED AND REPLACED APU MASTER PUSH BUTTON(FIN:14KD) PER ESPM 20-56-53. 03/04/2022 #2438457 OPS CHECK PENDING. OPS CHK APU PER AMM 49-00-00-860-801-A. OPS CHK GOOD. BITE APU PER AMM 49-00-00-740-801-4. NO FAULTS NOTED. OK FOR SVC

Part: NONE — NONE · airframe 42,876 hrs · 6,639 cycles

ETOPS - #2 ENG AFT UPPER INBD FIRE SEAL HAS 6" HOLE // REPLACED ENG2 AFT UPPER INBD FIRE SEAL PER TRENT 700 CMM 78-11-14. AC OK FOR SVC.

Part: VALVE — INOPERATIVE · airframe 42,572 hrs · 6,585 cycles

BTFS AFTER SHUTTING DOWN APU RECEIVED "FUEL TRIM LINE FAULT" EICAS MESSAGE // REMOVED AND REPLACED APU FUEL ISOLATION VALVE PER A330 AMM 28-29 AND PERFORMED OPERATIONAL TEST. OPS TEST NORMAL OK FOR SERVICE. ACTUATOR ASSY, OFF 33-2409-9-0001 S/N 00757 ON 33-2409-9-0001 S/N 01186

Part: VALVE — INOPERATIVE · airframe 42,405 hrs · 6,554 cycles

ETOPS - "FUEL TRIM LINE FAULT" ON ECAM // REMOVED & REPLACED APU ISOLATION VALVE (5QF) PER AMM 28-29-51-00 -801-A/400-801-A. OPS CHECK GOOD. NO MESSAGE ON ECAM ACTUATOR ASSY, OFF 33-2409-9-0001 S/N 01581 ON 33-2409-9-0001 S/N 00757

Part: VALVE — INOPERATIVE · airframe 42,357 hrs · 6,545 cycles

ETOPS - FUELER REPORTED END LIGHT FLASHING UNABLE TO REFUEL // GROUND SCAN SHOWS LH INLET INTR TANK ACTUATOR (603QL1) REMOVED AND REPLACED FUEL INLET VALVE (603QL1) ACTUATOR PER AMM 28-26-53. OPS AND LEAK CHK GOOD. OK FOR SVC. ACTUATOR, SINGL OFF 43-2826-9-0001 S/N 68336 ON 43-2826-9-0001 S/N 58212

Part: EPSU — INOPERATIVE · airframe 42,343 hrs · 6,543 cycles

SHIP 384 DURING EPSU TIME CHANGE, FOUND 16WL EPSU FAULTING. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU ASSY 16WL. (7245616)

Part: CONTROLLER — INOPERATIVE · airframe 42,318 hrs · 6,538 cycles

ETOPS - ENG 2 CTL SYS FAULT // ACCOMPLISHED TSM 75-33-00-810-808-A UP TO STEP 4.A(1)(B) MECH #565713 12/29/21. NEED TO CONTINUE FROM 4.A.2. ACCOMPLISHED TSM 75-33-00-810-808-A UP TO STEP 4.A.(2). RESITTANCE LIMITS OUT OF LIMITS. MECH #1825633 12/29/21. NEED TO CONTINUE FROM 4.A.(2)(B). REMOVED AND REPLACED THE #2 ENG VSV CTL - UNIT PER AMM 75-33-51. OPS/LEAK CHK OK. CONTROL, VARIAB OFF 43-7533-9-0001 S/N 09050 ON 43-7533-9-0001 S/N 14403

Part: NONE — NONE · airframe 41,876 hrs · 6,469 cycles

ETOPS-APU AUTO SHUTDOWN // APU FAULTS NO FUEL SUPPLY. UNABLE TO BLEED APU NO FUEL EXITS FUEL LINE AT FUEL CONTROL. FOUND APU FUEL ISOLATION VALVE 5QF DOES NOT OPEN FOUND 28 VDC PIN B OPEN WHEN MASTER SWITCH ON. SUSPECT ISOLATION VALVE ACTUATOR 5QF(AR0339941) PER A330 AWM 28-29-02 R/R ACTUATOR PER A330 AMM 38-29 NO HELP. FOUND DUMMY PLUG INCORRECT PIN CONFIG. INSTALLED NEW DUMMY PLUG BLEED APU PER A330 AMM 28-22 ALL OPS CHECK GOOD PER A330 AMM 49-00. A/C OK FOR SVC. ACTUATOR ASSY, OFF 33-2409-9-0001 S/N 01186 ON 33-2409-9-0001 S/N 01581

Part: NONE — NONE · airframe 41,635 hrs · 6,435 cycles

SHIP 384 EXIT SIGN ABOVE 3L DOOR CAME OFF. CORRECTIVE ACTION: RESECURED 3L EXIT DOOR SIGN. (7733357)

Part: NONE — NONE · airframe 41,388 hrs · 6,392 cycles

ETOPS - DUE TO REPEAT ECAM WARNING ENG 2 MINOR FAULT. NEED TO REPLACE PCU // REMOVED & REPLACED ENG #2 PCU PER AMM 73-21-35. OPS CHECK GOOD. OK FOR SVC. CONTROL, UNIT PN OFF 43-7321-9-0003 SN 80771 ON 43-7321-9-0003 SN 81750

Part: PUMP — LOW PRESSURE (RT FUEL) · airframe 41,296 hrs · 6,374 cycles

ETOPS - R STBY FUEL PUMP LOW PRESS. REMOVED AND REPLACED R STBY FUEL PUMP (112QA2) PER AMM 28-21-51-400-802-A. OPS / LEAK CHECK OK. A/C OK FOR SVC.

Part: COUPLER — INOPERATIVE (NR 2 HF ANTENNA) · airframe 41,296 hrs · 6,374 cycles

ETOPS - UNABLE TO TUNE OR SELCAL CHECK HF#2 // REMOVED AND REPLACED HF2 COUPLER PER AMM 23-11-36. OPS CHECK GOOD. HF TUNNING WORKIS NORMAL. OK FOR SVC. COUPLER, ANTENN OFF P/N 43-2311-9-0001 S/N 03440 ON P/N 43-2311-9-0001 S/N 0336

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 41,072 hrs · 6,336 cycles

SHIP 384 2L EMER EXIT SIGN LENSE NOT SECURED. CORRECTIVE ACTION: RE-SECURED 2L EMER EXIT SIGN. (7721493)

Part: EXCITER — FAULTED (ENGINE) · airframe 41,037 hrs · 6,332 cycles

ETOPS - GN A FAULT, REMOVED AND REPLACED ENG 1 A EXCITER A330 AMM 74-11-54. OPS CK GOOD.

Part: HANDLE — UNSECURE (E/E BAY DOOR) · airframe 41,012 hrs · 6,329 cycles

SHIP 384 UPON LANDING AND NOSE WHEEL TOUCHDOWN ECAM DOOR - AVIONICS DOOR OPENED. CORRECTIVE ACTION: FOUND AVIONICS DOOR HANDLE EXTENDED. INSPECTED DOOR HANDLE AND SECURED. (7721427)

Part: ENGINE — MAKING METAL (NR 1) · airframe 40,887 hrs · 6,311 cycles

ETOPS - ON TAXI IN ECAM ENG 1 OIL CHIP DETECTED - NEED TO REPLACE #1 ENGINE S/N: 42177 DUE TO EMCD DEBRIS REF L/P 7250089 // REPLACED #1 ENGINE PER CARD 7100-9401-HAL. HIGH POWER RUN COMPLETED. OPS LEAK CHECK GOOD. OFF P/N 43-7110-9-0010 S/N 42177 ON P/N 43-7110-9-0010 S/N 41785

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,861 hrs · 6,307 cycles

SHIP 384 3R EMERGENCY LIGHTS INOP. RESET AND TESTED EPSU. LIGHT OPS NORMAL.

Part: GENERATOR — DEFECTIVE (APU) · airframe 40,071 hrs · 6,190 cycles

ETOPS - BITE TEST OF GAPCU SHOWS CLASS 1 FAULT 242300 WRG: GEN APU FEEDER. TROUBLESHOOT PER TSM TASK 24-20-00-810-998-A UP TO STEP 4A.(2)(B) & FOUND FEEDERS ARE CORRECT. REMOVED AND REPLACED APU-GEN (8XS) PER AMM 24-23-51. OPS TEST GOOD. BITE TEST OF THE GAPCU GOOD. NO FAULTS. LEAK CHECK GOOD. GENERATOR, APU, OFF 33-2423-9-0001 04919 ON 33-2423-9-0001 04404

Part: LUG — CORRODED (RT WING TE FLAP) · airframe 39,668 hrs · 6,130 cycles

RT RIB 6 RT CORROSION ON FWD LUG. CORRECTIVE ACTION: CORROSION REMOVED, IAW ERA 586375-14AD REVISION ORIGINAL.

Part: LUG — CORRODED (RT WING TE FLAP) · airframe 39,668 hrs · 6,130 cycles

CORROSION FOUND ON RT RIB 6 FWD LUG. CORRECTIVE ACTION: CORROSION REMOVED BY OVERSIZING BORE AND SPOTFACING AFT FACE.

Part: FITTING — CORRODED (RIB 6) · corrosion level 2 · airframe 39,725 hrs · 6,140 cycles

SHIP 0384 RT RIB 6 FITTING WAS FOUND CORRODED. CORRECTIVE ACTION RHS RIB 6 FITTING WAS REWORKED PER ERA.

Part: ACTUATOR — DEFECTIVE (ENGINE FUEL) · airframe 39,649 hrs · 6,128 cycles

ETOPS-FUEL ENGINE 1 LP VALVE FAULT AT SHUTDOWN. REMOVED & REPLACED NR 1 ENGINE LP VALVE ACTUATOR, PER AMM 28-24-51. PERFORMED OPERATIONS CHECK, PER AMM 28-24-00. OPERATIONS CHECK OK. NO FAULTS NOTED. OK FOR SERVICE. ACTUATOR, TWIN OFF 33-2820-9-0003 90898 ON 33-2820-9-0003 45860.

Part: PRIORITY VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 39,532 hrs · 6,106 cycles

ETOPS SIGNIFICANT SYSTEM, NR 1 ENGINE BLEED NOT CLOSED. REPLACED THE NR 1 ENGINE PRV IAW AMM 36-11-52-804-A/ 36-11-52-400-804-A. OPS CHECK AND LEAK CHECK OK.

Part: OIL COOLER — LEAKING (NR 1 ENGINE OIL) · airframe 39,532 hrs · 6,106 cycles

ETOPS SIGNIFICANT SYSTEM - #1 ENG LEAKING FUEL FROM AOHE DRAIN LINE. // REPLACED #1 ENG AIR/OIL HEAT EX-CHANGER PER AMM 79-21-57-400-803-A UP TO STEP 4.A.(12),LEAK CHECK PENDING. LEAK CHECK COMPLETED IN REF W/ A330 AMM 79-21-57-400-803-A. NO LEAKS NOTED. T/R COWLS CLOSED OK FOR SERVICE.

Part: PCU — MALFUNCTIONED (APU) · airframe 39,365 hrs · 6,080 cycles

ETOPS SIGNIFICANT SYSTEM - APU GEN FAULT. // REMOVED & REPLACED APU GEN IAW HAL A330 TSM 24-23. FAULT REMAINS STILL. WAITING ADDITIONAL PARTS. DELL 111745. ALSO REF TSM 24-20 -00-810-986-A PERFORMED WIRE CHECK BETWEEN GAPCU AND APU GEN PER STEP 4.A.2. ALL CK'S GOOD. PMA 679725. REMOVED & REPLACED GAPCU PER HAL A330 AMM 24-41-34. OPS GOOD. CHKD OK.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 38,206 hrs · 5,903 cycles

EXIT SIGN ABOVE DOOR 3R NEEDS TO BE RE-ATTACHED. FELL OFF DURING BOARDING. // REATTACHED EXIT SIGN AT 3R. OK FOR SVC

Part: IDG — MAKING METAL (NR 2) · airframe 36,963 hrs · 5,711 cycles

ETOPS SIGNIFICANT SYSTEM - ELECTRIC GENERATOR 2 FAULT. REMOVED AND REPLACED IDG 2 PER AMM 24-21 OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL SYS) · airframe 36,042 hrs · 5,577 cycles

ETOPS SIGNIFICANT SYSTEM - FCMC 2 FUEL FAULT ECAM. PERFORMED BITE TEST OF FCMC 2 PER AMM 28-51-00.NO FAULTS, MESSAGE EXTINGUISHED. OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,738 hrs · 5,530 cycles

ETOPS SIGNIFICANT SYSTEM - FUEL - LEFT PUMP 1 LO PR ECAM ILLUMINATED IN - CRUISE. PERFORMED FCMC 1 AND 2 BITE PER AMM 28-51-00-740-801-A, TEST OK. PERFORMED OPERATIONAL CHECK OF L1 ENGINE 1 FUEL PUMP PER AMM 28-21-00-710-801-A. OPERATIONAL CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,777 hrs · 5,381 cycles

ETOPS SIGNIFICANT SYSTEM - ON SHORT FINAL FUEL L STBY PUMP LO PRES ECAM. NO FAULTS NOTED SYSTEM 1 & 2. NO CLASS 3 MESSAGES. PERFORMED FCMC SYSTEM TEST. FCMC 1 SYSTEM TEST OK. FCMC 2 SYSTEM TEST OK. OPERATED L STBY PUMP. OPS NORMAL. NO LOW PRESS INDICATION. OK FOR SVC.

Part: FILTER — CLOGGED (NR 1 ENGINE) · airframe 34,578 hrs · 5,347 cycles

DIVERTED DUE TO THE NBR 1 ENGINE FUEL FILTER CLOG MESSAGE, AND ENG EPR MODE RECOVERABLE MESSAGE. CORRECTIVE ACTION: REPLACED NBR 1 ENGINE LP FUEL FILTER (4088327), OPU, PCU, AND ECC (4088328). LP 4088327, 4088328.

Part: WARNING LIGHT — FALSE ACTIVATION (LT FUEL PUMP) · airframe 34,524 hrs · 5,339 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM FUEL LEFT PUMP 2 LO PRESS INDICATION FOR APPROX. 2-3 MIN DURING CRUISE @ FL390. // T/S PER A330 TSM 28-21-00-810-852-A. DURING GROUND TRANSFER OF FUEL, ALL OPERATIONS WERE NORMAL AND ALL ECAM INDICATIONS WERE NORMAL. OK FOR SVC.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 34,509 hrs · 5,336 cycles

ETOPS SIGNIFICANT SYSTEM - 1 ENGINE SN 41948 IS EXPERIENCING APPARENTLY UNCOMMANDED EEC CHANNEL CHANGES REPETITIVELY. REMOVED AND REPLACED NR 1 ENG EEC PER AMM 73-21-34-000-804-A/400-804-A. PERFORMED TEST OF EEC CONFIGURATION, TEST OF FADEC SYSTEM & LAND TEST. ALL TESTS PASSED. OK FOR SERVICE.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 34,374 hrs · 5,316 cycles

DURING C CHECK, DOOR 1 RIGHT FAILED OPERATIONAL CHECK OF EMERGENCY LIGHTS. REPLACED DOOR 1 RIGHT SLIDE PACK.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 34,383 hrs · 5,317 cycles

ETOPS / NR 2 ENGINE YELLOW EDP IS LEAKING AT MOUNTING FLANGE. REF: N/R 183 FOR REMOVE AND REPLACEMENT OF NR 2 ENGINE YELLOW EDP.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,218 hrs · 5,293 cycles

ETOPS SIGNIFICANT SYSTEM - APU BLEED FAULT AFTER LANDING. RESET 3X SAME EFFECT. PER TSM 49-62-00-810-846 PERFORMED APU FUNCTION CHECK & APU BITE TEST. ALL TESTS PASS & NO CURRENT FAULTS. OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,218 hrs · 5,293 cycles

ETOPS SIGNIFICANT SYSTEM - APU BLEED FAULT AFTER LANDING. RESET 3X SAME EFFECT. PER TSM 49-62-00-810-846 PERFORMED APU FUNCTION CHECK & APU BITE TEST. ALL TESTS PASS & NO CURRENT FAULTS. OK TO CONTINUE.

Part: COVER — MISSING (FLAP TRACK) · airframe 34,209 hrs · 5,292 cycles

LEFT NR 3 FLAP TRACK FAIRING COVER MISSING. INSTALLED SPEED TAPE UNTIL COVER CAN BE REPLACED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PRESSURE) · airframe 33,788 hrs · 5,228 cycles

ETOPS SIGNIFICANT SYSTEM - INFO TO MX AFTER LEVEL OFF HAD ECAM FUEL R2 PRESS LOW. LASTED APPROX. 2 MIN AND 45 SEC. FIXED ITSELF AND HAD NO RECURRENCE.// CHECKED TANK FOR WATER NONE NOTED. PURGED PRESSURE SWITCH LINE REF A330 AMM 28-21-00. RAN PUMP FOR 30 MIN NO FAULTS AT THIS TIME. A/C OK FOR SERVICE.

Part: SCUFF PLATE — DAMAGED (R4 DOOR) · airframe 33,495 hrs · 5,186 cycles

AIRCRAFT 384, ATB, RETURNED TO LAX DUE TO A PRESSURIZATION LEAK AT DOOR 4R, UNABLE TO HOLD CABIN PRESSURE. CORRECTIVE ACTION: REMOVED DOOR 4R SCUFF PLATE AND SCRAPPED OFF OLD SEALANT AND CLEANED AREA. INSTALLED NEW SCUFF PLATE AND SEALANT. PRESSURIZED AIRCRAFT, NO LEAKS FOUND.

Part: SCUFF PLATE — DAMAGED (R4 DOOR) · airframe 33,499 hrs · 5,186 cycles

ATB- PRESSURE LEAK AT 4R DOOR. UNABLE TO HOLD CABIN PRESSURE.// PRESSURIZED A/C PER A330 AMM 05-53-00 FOUND DOOR 4 RIGHT LEAKING AT BOTTOM CORNERS OF DOOR. PERFORMED REMOVAL OF DOOR 4 RIGHT SCUFF PLATE AND SCRAPPED OFF AND CLEANED OLD SEALANT PER A330 AMM 53-45-15. NEW SEALANT AND SCUFF PLATE INSTALL NEEDS TO BE C/W. INSTALLED AFT 4R DOOR SCUFF PLATE PER A330 AMM 53-45-15. PRESSURIZED A/C PER A330 AMM 5-53. NO LEAKS FOUND. OK FOR SVC.

Part: DUCT — DISCONNECTED (CARGO BAY) · airframe 32,428 hrs · 5,016 cycles

ETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP CYCLES BETWEEN 70* TO 80 DEGS. TRIM CYCLES BETWEEN 48* TO 124 DEGS. TEMP SELECTOR SET AT 12 O'CLOCK POSITION WHILE TEMP ELEVATES. CLEANED AND INSPECTED COCKPIT TEMP SENSOR PER AMM 21-63-17. NO DEFECTS FOUND. OPS NORMAL. FOUND DUCTING, FWD CARGO DISCONNECTED. REPLACED DUCTING AND CLAMPS 4 EACH. OPS CHECK GOOD, NO TEMP FLUCTUATION NOTED ON GROUND. OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (ZONE TEMP) · airframe 32,418 hrs · 50,134 cycles

DUCT TEMP ON CONDITION PAGE INDICATING 110, WITH TEMP IN COCKPIT INDICATING 74. REMOVED AND REPLACED THE ZONE CONTROLLER IAW AMM 21-63-34-00-801-A. ECS TESTED OK. OPS CHECKED OF ZONE CONTROL SYSTEM NORMAL. NO DEFECTS. OK FOR SERVICE.

Part: BELLOWS — FAILED (RT A/C PACK) · airframe 32,321 hrs · 5,001 cycles

BELLOWS ADJACENT TO THE RT PACK TEMPERATURE CONTROL VALVE BLOWN APART. THE RT PACK CONTROL VALVE BELLOWS WAS REPLACED AND TESTED. NO LEAKS.IAW AMM 21-52-21-000-801-A, AND 21-52-400-801-A, REV 61.05.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 29,757 hrs · 4,611 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED ENG 2 PYLON LOOP A DETECTOR FIN# 6WD2 PER AMM 26-12-16. OPS CHECK GOOD.

Part: COVER — LOOSE (CABIN) · airframe 28,818 hrs · 4,475 cycles

EMERGENCY EXIT COVER LOOSE AND DOOR 3R. RE-INSTALLED DOOR 3R EXIT COVER.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 28,797 hrs · 4,472 cycles

DOOR 2L EXIT SIGN COVER FELL OFF. SECURED EXIT SIGN COVER AT DOOR 2L.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CREW REST) · airframe 27,622 hrs · 4,300 cycles

ECAM FOR CABIN REST SMOKE ALARM ACTIVATED. CONFIRMED NO SMOKE. PERFORMED TSM 26-18-00-810-855-A. BITE TEST OF SMOKE DETECTOR IAW AMM 26-16-00-740-801.TEST PASSED, ACFT OK FOR SERVICE.

Part: EEC — MALFUNCTIONED (NR 2) · airframe 26,664 hrs · 4,157 cycles

DURING CLIMB AT 380 FOR 390, RECEIVED ECAM A/THR OFF FOLLOWED BY ECAM ENG 2 EPR MODE FAULT & ECAM ENG 1 EPR MODE FAULT. ECAM HAD US PUT BOTH ENGS IN N1 MODE BUT WE STARTED HAVING MULTIPLE ECAMS FLASH QUICKLY ACROSS THE SCREEN AND IT WAS IMPOSSIBLE TO FOLLOW. PUT ENGINES IN N1 MODE AND ECAMS CLEARED EXCEPT FOR ECAM EPR MODE RECOVERABLE. PUT ENGINES BACK IN EPR MODE AND ALL ECAMS CLEARED. DURING THE PROCESS, ENGINE POWER SEEMED TO BE CONTINUOUSLY REDUCING. USED MANUAL THROTTLES AND HAD TO GO ALL THE WAY TO TOGA POSITION, MAX PWR SETTING TO HOLD ALTITUDE & AIRSPEED AT GREEN DOT (MIN AI SPEED) NI GAUGES DID NOT SEEM TO MOVE WITH POWER CHANGES. OPERATED NORMALLY WHEN EPR RECOVERED. REMOVED AND REPLACED THE NR 2 EEC IAW AMM 73-21-34. UP TO STEP 4. D. (2). LAND 3 TEST OK IAW AMM 22-97-00. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 26,467 hrs · 4,128 cycles

CIDS 1 & 2 FAULT, RESET OF CIDS, 1 & 2 FAILED. PERFORMED CIDS 1 & CIDS 2 RESET IAW 23-73 OPS CHECKED NORMAL.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 26,384 hrs · 4,117 cycles

AIRCRAFT 0384, ABORTED TAKEOFF AT 80 KNOTS DUE TO NR 6 BRAKE SHOWING 305 DEGREES. DEFERRED PER MEL 32-42-1-HNL REPLACED NR 6 BRAKE.

Part: BRAKE — UNKNOWN (NR 6) · airframe 26,370 hrs · 4,113 cycles

REJECTED TAKEOFF AT APPROXIMATELY 80 KTS - NR 6 BRAKE SHOWED 305 DEGREES. DEFERRED NR 6 MLG BRAKE INOP, ACCOMPLISHED MPM 32-42-1, 32-11 TO 32-13. OK TO CONT, XSCRIBED TO LIDS & PLACARDED. TSM, PER TSM NO ACTION WAS REQUIRED, AS NO HISTORY AND NO MSGG.

Part: FIRE LOOP — FAULTED (NR 2 NACELLE) · airframe 26,238 hrs · 4,095 cycles

NR 2 ENGINE PYLON FIRE LOOP A MESSAGE. FOUND PYLON FIRE LOOP FAULTY. SLAVED IN A NEW LOOP, MESSAGE CLEARED.

Part: IGNITER — FAILED (APU) · airframe 26,218 hrs · 4,092 cycles

APU FAULT ECAM DURING START UP. ONLY GOT UP TO 17 PERCENT, THEN AUTOSHUTDOWN. TRIED TO START APU TWO TIMES DURING DESCENT. BOTH WITH AUTO SHUTDOWN & APU FAULT ECAM. TROUBLESHOT IAW TSM 49-00-00. FOUND IGNITER AT FAULT. REMOVED AND REPLACED BOTH APU IGNITER PLUGS IAW AMM 49-41-41. APU STARTED OK. ECAM MESSAGE CLEARED.

Part: SLIDE — UNSERVICEABLE (L3 DOOR) · airframe 25,604 hrs · 3,990 cycles

3L EMERGENCY EXIT DOOR ESCAPE SLIDE PARACHUTE PIN SPEED LACING IS LOOSE. SLIDE REPLACED.

Part: SMOKE DETECTOR — DEGRADED · airframe 25,546 hrs · 3,982 cycles

SDF SYS TEST FAILED, FAULT MESSAGE' 261615. SMOKE DETECTOR FWD LDCC (3WH) DEGRADED AND 261615 SMOKE DETECTOR FWD LDCC (3WH ) CONTAMINATION. CLASS 3 FAULT. SMOKE DETECTOR REPLACED IAW AMM 26-16-15 REV 56.02.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y1959, BETWEEN FRAMES 47-53.2 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11, REV 92, DRAWINGS F53312812, F533255687 AND F53325686.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y1959, BETWEEN FRAMES 53.2 - 54 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F5332694100.

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y1959, BETWEEN FRAMES 58.5 - 62 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F53477040006.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y1959, BETWEEN FRAMES 54.5 - 58.5 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT Y1470, FRAMES 58-60A FOUND CORRODED. REPLACED THE ROLLER TRAY IAW AMM 25-51-21, REV 56.02.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y450, BETWEEN FRAMES 54.5-58.5 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92, DRAWINGS F5347620004, F53477650004, AND F53329385002.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y2462, BETWEEN FR 53.2-54 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F53312813019.

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FRAMES 58.5 - 62 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F53477040.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y450, BETWEEN FRAMES 40-47 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F57112816.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,546 hrs · 3,982 cycles

LOG 2904330: SEAT TRACK -Y450 BETWEEN FR54.5 AND FR 58.5 CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11 REV 92 & IAW DRAWINGS F53476200004, F53477650004, F53329385002

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y1959, BETWEEN FRAMES 54.5 - 58.5 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F53476200004.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT -Y1265, FR 62-63 FOUND CORRODED. REPLACED ROLLER TRAY IAW AMM 25-51-21 REV 56.02.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT -Y140, FRAMES 58 - 68 FOUND CORRODED. REPLACED THE ROLLER TRAY IAW AMM 25-51-21, REV 56.02.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FRAMES 54.5-58.5 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F53476200.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT Y1470, FRAMES 58 - 60A FOUND CORRODED. REPLACED THE ROLLER TRAY IAW AMM 25-51-21, REV 56.02.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, ZONE 260, SEAT TRACK AT Y450, BETWEEN FRAME 54.5 - 58.5 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F53476200004.

Part: SEAT TRACK — CORRODED (FRAMES 71-75) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y450, BETWEEN FRAMES 71.5 - 75 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 92, AND DRAWING F5347804008.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT Y1470, FRAMES 58-65 FOUND CORRODED. REPLACED ROLLER TRAY IAW AMM 25-51-21, REV 56.02.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y450, BETWEEN FRAMES 53.2 - 53.4 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F53326973000.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y450, BETWEEN FRAMES 47-53.2 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F53334771.

Part: ROLLER TRAY — CORRODED (AFT CARGO) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, AFT CARGO ROLLER TRAY AT Y301, FRAMES 65 - 68 FOUND CORRODED. REPLACED THE ROLLER TRAY IAW AMM 25-51-21, REV 56.02.

Part: FITTING — CORRODED (FRAME 17) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, EIGHT FLIGHT ATTENDANT SEAT HARD POINTS FORWARD OF FRAME 17 BETWEEN -Y1456 AND -Y1959 FOUND CORRODED. REPLACED CENTER HARD POINT FITTING, IAW SRM 51-42-11 REV 92 DRAWING F2531071300 AND F25310721000.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y450, BETWEEN FRAMES 47-53.2 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F53334771.

Part: SEAT TRACK — CORRODED (FRAMES 71-73) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FR 71.5-73.5 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 REV 92. LP 2900471.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FRAMES 53.2-54 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y1959, BETWEEN FRAMES 53.2-54 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F53326941000 .

Part: SEAT TRACK — CORRODED (FRAMES 67-71) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT -Y450, BETWEEN FRAMES 67.5-71.5 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 REV 92 AND DRAWING F5347721420700.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FR 62-71.5 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 REV 92.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, SEAT TRACK AT Y2462, BETWEEN FRAME 62-71.5 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 REV 92 AND DRAWING F53477040006. LP 2903000.

Part: SEAT TRACK — CORRODED (FRAMES 58-67) · airframe 25,579 hrs · 3,986 cycles

DURING H CHECK, ZONE 260, SEAT TRACK AT +Y450, BETWEEN FR 58.5-67.5 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 REV 92. LP 2899161.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,536 hrs · 3,981 cycles

SEAT TRACK -Y 1959 FR33(+4IN) HAS OUT OF LIMITS CORROSION. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,536 hrs · 3,981 cycles

SEAT TRACK -Y 2462 FR32 HAS CORROSION EVIDENT. CORROSION ASSESSED AS OUT OF LIMITS, REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED · airframe 25,546 hrs · 3,982 cycles

SEAT TRACK CORRODED, CORROSION REMOVED IAW SRM 51-74-00 REV 92. CORROSION ASSESSED AS OUT OF LIMITS IAW 53-00-15 REV 92. SEAT TRACK REPLACED IAW SRM 51-72-11 REV 92 AND DRAWING F53271910000.

Part: SEAT TRACK — CORRODED (FRAME 32) · airframe 3,982 hrs · 25,546 cycles

SEAT TRACK -Y 2462, FRAME 32 HAS CORROSION. CORROSION REMOVED IAW SRM 51-74-00 REV 92. FOUND TO BE OUT OF LIMITS IAW 53-00-15 REV 92. SEAT TRACK REPLACED IAW SRM 51-72-11 REV 92 AND DRAWING F53276421004.

Part: SEAT TRACK — CORRODED (FRAMES 58-67) · airframe 25,536 hrs · 3,981 cycles

DURING H CHECK, ZONE 270, FRAMES 58.5 - 67.5, +450 SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK LP 2890483

Part: LIGHT — LOOSE (ROW 22 AB) · airframe 25,366 hrs · 3,952 cycles

EMERGENCY LIGHT LOOSE AT ROW 22 AB. SECURED THE EMERGENCY LIGHT.

Part: PUMP — LEAKING (APU FUEL) · airframe 25,210 hrs · 3,923 cycles

DURING PDC, FOUND FUEL LEAKING FROM TRIM LINE, APU FUEL DRAIN MAST P BOX FULL OF FUEL. REMOVED AND REPLACED THE TRIM TANK TRANSFER PUMP IAW AMM 28-27-48. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 25,205 hrs · 3,922 cycles

IMMEDIATELY AFTER DOORS CLOSED, WHITE SMOKE THAT SMELLED LIKE A HOT PACK MOMENTARILY CAME FROM FO SIDE VENT. TURNED OFF PACKS NO ODOR IN CABIN. INSPECTED THE E/E COMPARTMENT FOR OBVIOUS DEFECTS, NONE FOUND, RAN BOTH PACKS NO ODOR NOTED, VISUAL INSPECTION OF APU NO LEAKS NOTED, PERFORMED COCKPIT AND CABIN TEMP CONTROL TEST IAW AMM 21-63-00-730-801A, TEST PASSED, NO FAULTS NOTED ON GROUND. OK TO CONTINUE.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 25,055 hrs · 3,896 cycles

L3 DOOR EXIT SIGN DETACHED. INSTALLED EXIT SIGN.

Part: LIGHT — LOOSE (CABIN) · airframe 24,498 hrs · 3,808 cycles

EMERGENCY PATH LIGHTING COMING LOOSE AT SEATS 22AB. RE-SECURED PATH LIGHTING.

Part: LIGHT — ILLUMINATED · airframe 24,430 hrs · 3,795 cycles

R3 DOOR EXIT LIGHT ILLUMINATED IN FLIGHT. RESET EXIT LIGHT, OPERATIONAL CHECK OK. LP 8097266

Part: SIGN — ILLUMINATED · airframe 24,430 hrs · 3,795 cycles

R3 DOOR EXIT LIGHT ILLUMINATED IN FLIGHT. RESET SEAT BELT ON SIGN, OPERATIONAL CHECK OK.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 23,225 hrs · 3,607 cycles

SMOKE DETECTOR LAV FAULT. PERFORMED BITE TEST OF CIDS 1 & 2. FAULT CLEARED PER AMM 23-35-00. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 21,502 hrs · 3,347 cycles

FM1 FAULT. DOWNPOWERED ACFT PERFORMED AFS BITE TEST. TEST PASSED. ACFT OK FOR SERVICE.

Part: DUMP VALVE — CRACKED (FUEL TANK) · airframe 18,149 hrs · 2,843 cycles

TRIM TANK APPEARS TO HAVE EMPTIED INTO RT TANK ONLY. CROSS FED OUT RIGHT TANK TO REBALANCE. FOUND JETTISON VALVE CRACKED. R & R RT JETTTISON VALVE IAW AMM 28-31-41-000-801-A. OPS AND LEAK CHECKS GOOD.

Part: RELAY — FAILED

WHILE ACFT WAS SITTING, GOT ECAM FAULT "FUEL CTR TO INNER FAULT" WITH CMC CLASS 1 FUEL INR HI LEVEL 2, 21QJ2. TEST IAW 28-26-00 AND REPLACED RELAY 9QL2. OP'S CHECK AND BITE CHECK IAW AMM 28-26-00. ALL OPS AND BITE CHECKED NORMAL.

Part: TRANSFER VALVE — LEAKING (FUEL SYS)

TRIM TANK FUEL TRANSFER TO RT TANK, INNER TANK ONLY W/ NO INDICATION ON ECAM, NO TRIM TANK TRANSFER MSG SHOWN. THIS CAUSED A FUEL IMBALANCE WHICH CREW NOTICED AT 4500 LBS, RT WING HEAVY. TEST TO RT INNER TANK INLET VALVE 5603QA2.

Part: FILTER — CLOGGED (APU OIL SYS) · airframe 18,149 hrs · 2,834 cycles

DUE APU SHUTDOWN AND MESSAGE OF OIL FILTER CLOG ON REPORT. R & R BOTH APU LUBE AND SCAVANGE FILTERS IAW AMM 49-91-41. PERFORMED OPS AND LEAK CHECK. NO FAULTS FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 17,200 hrs · 2,683 cycles

AIRCRAFT PERFORMED AN AIR TURNBACK TO DEPARTUE DUE TO THE "CAB PR SYS 1 FAULT" ECAM MESSAGE APPEARED. PERFORMED AN OPS TEST OF THE PRESSURE CONTROL AND MONITOR SYSTEM, OPS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 17,210 hrs · 2,684 cycles

ECAM CAB PR SYS 1 FAULT. PERFORMED TSM TASK 21-31-00-810-802A. OPS TEST OF PRESSURE CONTROL AND MONITORING. OPS CHECK GOOD. NO FAULT NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 16,701 hrs · 2,605 cycles

NAV ADR2 FAULT, ACCOMPLISHED TSM 34-10-00-810-995. NO FAULTS NOTED. ACCOMPLISHED AFS BITE AND LAND 3 CAPABILITY TEST, 22-96-00 & 22-97-00. NO FAULTS NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 16,691 hrs · 2,604 cycles

AIRCRAFT 384 ATB, RETURNED TO DEPARTURE DUE TO NAV ADR 2 FAULT. ACCOMPLISHED TSM 34-10-00-810-995, NO FAULTS NOTED. ACCOMPLISHED AFS BITE AND LAND 3 CAPABILITY TEST, 22-96-00 AND 22-97-00 NO FAULTS NOTED. F/O PITOT PROBE AND PITOT LINE WERE CHECKED, INSPECTED AND FLUSHED, ALL CHECKED GOOD AND NO DEBRIS FOUND. PERFORMED RESET OF THE 3 FCPC PUSHBUTTON SWITCHES ON THE OVERHEAD PANEL, WITH 3 HYDRAULIC SYSTEMS DEPRESSURIZED, ORIGINAL FAULTS CLEARED. ACCOMPLISHED AIRSPEED INDICATION, ALL CHECK NORMAL.

Part: PACKING — DAMAGED (HYD SYSTEM) · airframe 16,313 hrs · 2,543 cycles

LOST BLUE HYDRAULIC QUANTITY DURING CRUISE. FOLLOW ECAM CHECKLIST, BLUE HYDRAULIC PUMPS TURNED OFF RIGHT AWAY. CAPTAIN STATED BLUE HYD PUMPS TURNED OFF WHILE PRODUCING NORMAL PRESSURE & RESERVOIR STILL HAD FLUID. FOUND DAMAGED PACKING ATB SYS HP MANIFOLD 6103JM FITTING. REPLACED PACKING IAW AMM 29-12 & NO LEAKS NOW. ENGINE & ELEC PUMPS OPERATE NORMALLY. SERVICED BLUE HYD SYS TO FULL. OK FOR SERVICE.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 14,789 hrs · 2,307 cycles

DAMAGE FOUND ON LOWER INNER SKIN PANEL OF AFT CARGO DOOR. PERFORMED 10X MAG INSPECTION IAW ERA 529306-14, ENSURED NO LOOSE FASTENERS, DVI ACCOMPLISHED, DENTS ARE SMOOTH AND NO MATERIAL WAS REMOVED. REPAIR IDENTIFIED IAW SP 900-5-1 NR 04. OK FOR CONTINUED FLIGHTS.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 14,789 hrs · 2,307 cycles

DAMAGE FOUND ON LOWER INNER SKIN PANEL OF AFT CARGO DOOR. PERFORMED 10X MAG INSPECTION IAW ERA 529306-14, ENSURED NO LOOSE FASTENERS, DVI ACCOMPLISHED, DENTS ARE SMOOTH AND NO MATERIAL WAS REMOVED. OK FOR CONTINUED FLIGHTS.

Part: IGNITER — INOPERATIVE (APU) · airframe 13,642 hrs · 2,118 cycles

AUTO SHUTDOWN OF APU, AFTER FUELING WAS COMPLETED, THREE START ATTEMPTS. REPLACED BOTH IGNITORS AND LEADS IAW AMM 49-41. APU STARTS NORMAL.

Part: ADIRU — FAULTED (NR 2) · airframe 8,113 hrs · 1,281 cycles

ON TAKEOFF, F/O AIRSPEED FAILED. ACCOMPLISHED BITE TEST, IAW AMM 22-96-00-704-801, FAULT ADIRU 2 (1FP2). SWAPPED ADRIU FROM POSITION NR 3 TO POSITION NR 2 AND INSTALLED NR 3 IAW AMM 34-12-34-400-801-A, ALL TEST PASSED, OK FOR SERVICE.

Part: APU — FAULTED · airframe 6,480 hrs · 1,050 cycles

APU AUTO SHUTDOWN. FOUND APU FAULT FCU, APU FUEL SUPPLY PRESSURE, APU ROTATION BLEED, APU FUEL LINE IAW MM 28-22-00-820-801-A, GROUND OPS CHECKED OK.

Part: EPSU — NO TEST (ZONE 200) · airframe 1,634 hrs · 295 cycles

ODOR OF BURNING RUBBER AT DOOR 4L. EMERGENCY POWER SUPPLY UNIT AT 4L WOULD NOT TEST REMOVED AND REPLACED PER AMM 33-51-38. RAN ENGINE 1 & 2 ON ENGINE BLEED ON PACKS FULL HOT AND COLD, NO FAULTS FOUND. OK FOR CONTINUED SERVICE.

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 633 hrs · 112 cycles

ETOPS SIGNIFICANT SYS - NICK ON NR 24 BLADE NR 1 ENGINE, 6.5" FROM TIP, ZONE C, .3125 X .7500 OF AN INCH. BENDED NR 24 BLADE IAW MM. BLENDING FPI 9006-3, NR 2. INSPECTED AND FOUND NO INDICATIONS. COMPLIED WITH TEST 11 IAW AMM 71-00-00-700-838-A. ENGINE VIBRATIONS WITHIN LIMITS, ER-A. 43-497939-14, REV A COMPLETED. OK FOR SERVICE.

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 633 hrs · 112 cycles

ETOPS SIGNIFICANT SYS - NICK ON NR 1 ENGINE BLADE NR 19, 20.75" FROM THE TIP, ZONE B .1875 X .038 OF AN INCH. BLENDED NR19 FAN BLADE IAW MM. BLENDING, FPI IAW PS 900-6-3 NR 2. INSPECTED AND FOUND NO INDICATIONS, ER A-43-497939-14 REV A COMPLETED. OK FOR SERVICE.