N214HA

Part: EPSU — INOPERATIVE (ZONE 200) · airframe 22,706 hrs · 4,761 cycles

BAT/EPSU FW 11WL EXT L. GROUNDED - YES. REPLACED EMER 11WL EPSU PER AMM 33-51-38. OPS CHECK GOOD. OK FOR SERVICE.

Part: GCU — NO TEST (NR 1) · airframe 21,581 hrs · 4,534 cycles

DIV - ECAM: GEN 1 FAIL. EPGS SYSTEM TEST: GCU 1 TEST FAILED. FAULT MESSAGE IDG1(E1-400XU)SERVO VLV/GCU1 (1XU1). PERFORMED TSM 24-20-00-810-914-A. FOUND CABLE E1-400XU CONTAMINATED AND SLIGHTLY LOOSE. CLEANED AND SECURED AS REQUIRED. RESISTANCE & WIRE CHECKS ALL WITHIN LIMITS. REMOVED AND REPLACED GCU 1 PER AMM 24-22-34. OPS CHECK GOOD. OK FOR SVC.

Part: WIRE HARNESS — FAULTED (ZONE 400) · airframe 21,580 hrs · 4,533 cycles

ETOPS - ENG 1 LOOP B FAULT. REPLACED ENG 1 LOOP B FIRE HARNESS PER A321 AMM 26-12-62 OPS CHECK GOOD , OK FOR SERVICE

Part: GENERATOR — FAULTED (NR 1) · airframe 21,484 hrs · 4,514 cycles

ETOPS - ELEC GEN 1 FAULT- AT CRUISE DID NOT RESET. REMOVED & REPLACED #1 IDG PER AMM 24-21-51. OPS CHECK IS GOOD. OKAY TO CONTINUE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 21,177 hrs · 4,450 cycles

SMOKE LAVATORY SMOKE MESSAGE CONFIRMED WITH FA FALSE ALERT. FFA DID RESET AND MESSAGE CLEARED. NO SMOKE/VAPE/FIRE PRESENT

Part: WIRE HARNESS — FAULTED (FIRE DETECTION) · airframe 21,145 hrs · 4,444 cycles

ETOPS - ON CLIMB OUT MOMENTERY ECAM FOR ENG 1 LOOP B FAULT MESSAGE CLEAR ON ITS OWN AFTER A FEW MINUTES. REMOVED AND REPLACED ENGINE 1 HARNESS 4166KS PER AMM 26-12-62 AND REPLACED ENGINE 1 CORE AGB LOOP B FIN 4002WD2 PER AMM 26-12-17 OPS CHECK OK

Part: EXCITER — FAULTED (NR 1 ENGINE) · airframe 20,944 hrs · 4,403 cycles

ETOPS - ENG 1 IGN B FAULT. REMOVED & REPLACED IGNITION EXCITER PER AMM 74-11-01-000-801-A & AMM 74-11-01-400-801-A. REMOVED & REPLACED IGNITER PLUG PER AMM 74-21-01.PERFORMED OPS TEST OF IGNITION SYSTEM PER AMM 74-00-00-710-802-A. OPS TEST GOOD. NO FAULTS NOTED. A/C OK TO CONTINUE.

Part: STARTER — FAULTED (APU) · airframe 20,719 hrs · 4,357 cycles

ETOPS - APU AUTOSHUTDOWN 3 TIMES. REMOVED AND REPLACED STARTER ON APU PER AMM 49-42-51. REPLACED CLUTCH PER AMM 49-42-51. REPAIRED DAMAGED WIRE PER E105 -C30086-INI OPS CHECK GOOD OK TO CONTINUE

Part: IGNITER — FAULTED (NR 2 ENGINE) · airframe 20,460 hrs · 4,306 cycles

ETOPS - ON START ENG 2, ENGINE REATTEMPT 2ND ATTEMPT SUCCESSFUL ENG 2 IGN A FAULT. REPLACED #2 ENG A IGNITER PLUG PER AMM 74-11-01. AUDIBLE CHECK GOOD. OK FOR SVC.

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 20,460 hrs · 4,306 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT CAME ON MULTIPLE TIMES DURING CRUISE AND WOULD EXTINGUISH. FOUND THERMAL DAMAGE ON CONTACTS OF 454VC1. REPLACED ALL 4 CONTACTS OF 454VC1 PER ESPM 20-48-24. FDU 1 OPS CHECK OK PER AMM 26-12-00. PERFORMED ENGINE RUN PER AMM 71-00-00-860-823-A. NO FAULTS NOTED, OPS CHECK NORMAL. OK FOR SERVICE.

Part: FIRE LOOP — FALSE INDICATION (ZONE 400) · airframe 20,385 hrs · 4,292 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT 3X IN CRUISE. CLEARED ON ITS OWN. REMOVED & REPLACED ENG 1 FIRE LOOP B IAW AMM 26-12-17, OPS TEST OK. NO FAULT NOTED. OK FOR SVC

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 20,380 hrs · 4,291 cycles

ETOPS - SPURIOUS ENG1 FIRE LOOP B ECAM. ECAM ILLUMINATED 4 TIMES DURING FLIGHT. REMOVED AND REPLACED ENG1 AGB LOOP B PER AMM 26-12-17, PERFORMED FDU BITE TEST PER AMM 26-12-00 TEST OK. A/C OK FOR SVC.

Part: RADOME — DAMAGED (ZONE 100) · airframe 20,350 hrs · 4,285 cycles

FOUND BIRD STRIKE ON RADOME DAMGE BEYOND LIMITS. REMOVED AND REPLACED RADOME IAW AMM 53-15-11. OPS CHECK GOOD . OK TO CONTINUE

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 20,135 hrs · 4,245 cycles

ETOPS-ECAM - ENG 1 FIRELOOP B FAULT. REMOVED AND REPLACED ENG 1 FIRE LOOP B HARNESS (4166KS). PER AMM 26-12-62-400-802-A. FIRELOOP TESTS OK. OK FOR SVC.

Part: IGNITER — DAMAGED (NR 1 ENGINE) · airframe 20,104 hrs · 4,239 cycles

ETOPS - DURING ENG 1 BORESCOPE INSP OF THE COMBUSTION CHAMBER AND HPT NOZZLE GUIDE VANES, IGNITER PLUG WAS REMOVED AND FOUND DAMAGED. REPLACED IGNITER REF AMM 74-21-01. CHECKS OK

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 19,992 hrs · 4,216 cycles

ETOPS - BTB FOR AN ENG 1 FIRE LOOP FAULT CLEARED AFTER 10 MINUTES . REMOVED AND REPLACED ENGINE 1 AGB LOOP B PER A321 AMM 26-12-17-000-802-A AND 26-12-17-400-802A. FDU BITE CHECK PASS PERFORMED ENGINE RUN ON EGNINE #1 NO FAULTS AC OK TO CONTINUE

Part: WIRE HARNESS — LOOSE (NR 1 FIRE LOOP) · airframe 19,912 hrs · 4,201 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT APPEARED SEVERAL TIMES DURING FLIGHT. CLEARED AFTER 30-60 SEC. GROUND CHECK HARNESS 4166KA FOUND LOSE AND DAMAGED CLAMP NEAR 4001WD2 REMOVED AND REPLACED CLAMP CHECKED OK. OPS TEST FDU #1 TEST OK PER: AMM 26-12-00. CHECKED 454VC1 PIN3 & PIN4 RESISTENT AND INSULATION CHECK OK. 2WD1 B PIN J TO PIN K RESISTANT 1.5K NO SHORT TO GROUND.ENGINE RUN CHECK OK.

Part: WIRE HARNESS — FAULTED (ZONE 400) · airframe 19,808 hrs · 4,180 cycles

ETOPS - ENG 1 FIRE LOOP A ECAM FOR ABOUT 1 MINUTE ON CLIMB OUT. GROUND CHECK 452VCA PIN 1 TO PIN 2 FOR 4002WD1 AND 452VCA PIN 3 TO PIN 4 FOR 4001WD1 INSULATION AND RESISTANCE CHECK OK. REMOVED AND REPLACED HARNESS 4165KS ON ENG #1 PER AMM 26-12-61. OPS CHECK OK FOR SERVICE.

Part: PACKING — FAILED (HYD SYSTEM) · airframe 19,591 hrs · 4,138 cycles

ATB - GREEN HYD RES LOW LEVEL ECAM REACHING 32,000'. THEN GREEN LOW HYD LO PRES ECAM. AIR TURN BACK TO HNL. FOUND BROKEN PACKING AT #1 ENG PUMP PRESSURE SWITCH. INSTALLED NEW PACKING PER AMM 29-13-17/802-A. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SVC.

Part: HYDRAULIC LINE — LEAKING (ZONE 400) · airframe 19,338 hrs · 4,088 cycles

ETOPS - FOUND #2 ENG PYLON HYDRAULIC PRESSURE LINE LEAKING DURING WALKAROUND. REPLACED #2 ENG HYDRAULIC PYLON PRESSURE LINE REF AMM 29-13-49. ALL OPS AND LEAK CHECKS GOOD. OK TO CONTINUE SERVICE.

Part: HYDRAULIC LINE — LEAKING (ZONE 400) · airframe 19,328 hrs · 4,086 cycles

ETOPS - FOUND #2 ENG PYLON HYDRAULIC PRESSURE LINE LEAKING DURING WALK AROUND. REPLACED #2 ENG HYDRAULIC PYLON PRESSURE LINE REF AMM 29-13-49. ALL OPS AND LEAK CHECKS GOOD. OK TO CONTINUE SERVICE.

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 19,031 hrs · 4,027 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED ENG 1 LOOP B HARNESS ASSLY (4166KS) PER AMM 26-12-62 BITE TEST GOOD. PERFORMED ENGINE RUN AS PRECAUTION NO FAULTS NOTED.

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 18,940 hrs · 4,009 cycles

ETOPS - ENG 1 FIRE LOOP B FAULT 2X IN CRUISE & 1X ON DESCENT CLEARED BOTH TIMES AFTER 30 MIN. REPLACED FDU 1 REF AMM 26-12-34. OPERATIONAL CHECKS GOOD. RAN ENGINE AS PRECAUTIONARY AND NO DEFECTS OR FAULTS. OK TO CONTINUE SERVICE.

Part: FUEL CAP — MISSING · airframe 18,793 hrs · 3,980 cycles

ETOPS - FUELER REPORT FUEL CAP DIFFICULT TO REMOVE. FOUND CAP DEFORMED. REMOVED AND REPLACED FUEL CAP.

Part: FIRE LOOP — FALSE ACTIVATION (ZONE 400) · airframe 18,770 hrs · 3,976 cycles

ETOPS - ENG 1 LOOP CAUTION. REPEATEDLY (7 TIMES) DURING FLIGHT. GROUND REMOVED AND REPLACED HARNESS FIRE ASSEMBLY (4165KS) TEST OK PER AMM 26-12-61-400-802A. (RQ 19537 NOV/26/2024. PERFORMED #1ENG RUN. NO FAULTS NOTED. OK FOR SVC.

Part: FIRE LOOP — INTERMITTENT (ZONE 400) · airframe 18,760 hrs · 3,974 cycles

ETOPS - ENG 1 FIRE LOOP A FAULT INTERMITTENT THROUGHOUT FLIGHT OCCURED 4 TIMES (IN CLIMB , CRUISE, AND DESCENT). PERFORMED TSM 26-12-00-810-852-A BITE MESSAGE FOR "CHECK ENG 1 AGB LOOP A" REMOVED AND REPLACED ENG 1 COER AGB LOOP A PER AMM 26-12-17-00-802 & 26-12-17-400-802 FAULT CLEARED & TEST PASS AC OKAY TO CONTINUE

Part: TERMINAL — CRACKED (FIRE LOOP) · airframe 18,420 hrs · 3,906 cycles

ETOPS - WHILE TROUBLESHOOTING ENG 1 LPA FIRE LOOP FOUND 4181KS TERMINAL CRACKED AND 4165KS INTERMITTENT SHIRT TO GND. REPLACED ENG 1 4181KS PER AMM 26-12-61. REPLACED ENG 1 HARNESS 4165KS PER AMM 26-12-61-400-802. OPERATIONAL CHECK OK PER AMM 26-12-00710-001-A & 26-12-00-710-002-A

Part: FIRE LOOP — FALSE INDICATION (ZONE 400) · airframe 15,500 hrs · 3,227 cycles

ETOPS - INFO TO MX: ENG1 FIRELOOP A FAULT DURING CLB. ECAM CLEARED. BITE FDU1 NO FAULTS. CHECK FDU1 J-K 1.493 OHMS, J TO GND OPEN, K TO GND OPEN PER ASM 26-12-01. REPLACED FDU1 PER AMM 26-12-34 OPS CHECK OK.

Part: BYPASS VALVE — MALFUNCTIONED (NR 2 PACK) · airframe 17,823 hrs · 3,784 cycles

ATB - DUE TO ETOPS VERIICATION FLIGHT UNSATISFACTORY PLUS ISSUES WITH MULTIPLE ECAMS. PFR FAULT AIR PACK 2 REGUL FAULT ATA 21-61 CARRIED OUT TROUBLESHOOTING OF AIR PACK 2 IAW TSM 21-61-00-810-817-A. CARRIED OUT OPERATIONAL TEST OF PACK TEMP-CONTROL SYS IAW A321 AMM 21-61-00-710-001. P2 BY-PASS VALVE (30HH)FOUND FAULTY FOR REPLACEMENT. PERFORMED REPLACEMENT OF PACK 2 TURBINE BYPASS VALVE, IAW AMM 21-61-53-000-001-A AND 21-61-53-400-001-A. SYSTEM OPS CHECKS GOOD. OK TO CONTINUE.

Part: WARNING LIGHT — ILLUMINATED (APU) · airframe 17,666 hrs · 3,753 cycles

AFTER APU START ON ARRIVAL "LOW OIL LEVEL" FLASHING (2ND WRITE-UP IN 2 DAYS). REMOVED AND REPLACED APU ASSY PER AMM 49-11-11. OPS CHK AND LEAK CHK GOOD.

Part: INTERPHONE — MALFUNCTIONED (AFT GALLEY) · airframe 17,264 hrs · 3,673 cycles

ETOPS - AFT GALLEY INTERPHONE VOLUME TOO LOW. REMOVED AND REPLACED INTERPHONE IN REF TO AMM 23-73-44 OPS CHECK GOOD OK TO CONTINUE.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 17,187 hrs · 3,658 cycles

1L DOOR SLIDE FELL OFF DOOR. REMOVED AND REPLACED 1L SLIDE ASSY PER AMM 25-62-44. OPS CHECK GOOD. OK FOR SVC.

Part: GENERATOR — FAULTED (APU) · airframe 17,105 hrs · 3,641 cycles

ETOPS - APU GEN FAULT. REMOVED AND REPLACED GAPCU, CONDITION SAME, REPLACED ORIGINAL GAPCU PER AMM 24-41-34 AND TSM 24-23-00-810-813-A. REMOVED AND REPLACED APU GENERATOR PER AMM 24-23-51, OPS AND LEAK CHECK GOOD, APU OIL LVL GOOD. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,001 hrs · 3,425 cycles

ETOPS - ENG 1 FIRE LOOP A ECAM FAULT. REMOVED & REPLACED ENG 1 FIRE LOOP A HARNESS (4165KS) PER AMM 26-12-61. FAULT CLEARED FDU 1 TEST OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,789 hrs · 3,383 cycles

ETOPS - ECAM: ENG 1 FIRE LOOP A FAULT. FOUND AGB LOOP A CLAMP BROKEN, REPAIRED PER M105 FILE # R0363. PERFORMED OPS TEST OF FDU 1 PER AMM 26-12-00. OPS TEST GOOD. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,723 hrs · 3,368 cycles

ETOPS - INFO TO MAINT: ECAM ENG 1 FUEL FILTER PARTLY CLOGGED DURING INITIAL CLIMB OUT. EXTINGUISHED AFTER ABOUT 3 MIN. NOTED BY MX. REMOVED AND REPLACED THE #1 ENG FUEL FILTER ELEMENT AND FUEL FILTER DIFFERENTIAL PRESSURE SENSOR PER AMM 73-11-06 / 73-34-21. OPS / LEAK CHK OK. A/C OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,212 hrs · 3,254 cycles

ETOPS - ECAM APU AUTO SHUTDOWN OCCURED WHILE TAXINING TO GATE. WE ATTEMPTED 3 START ATTEMPTS PER MOC. REMOVED APU STARTER PER AMM 49-42-51. REMOVED AND REPLACED STARTER MOTOR CLUTCH PER AMM 49-42-52. REPLACED APU STARTER PER AMM 49-42-51. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 15,155 hrs · 3,241 cycles

ETOPS - DURING ENG ONE START CABIN AND COCKPIT FILLED W/ SMOKE. SHUT OFF PACK 1 AND SMOKE DISSIPATED. REMOVED & REPLACED FRONT PACKING ON INLET CONE PER AMM 72-15-00-960-801. REPLACED #1 ENG REF WO 267827 T/C 5321-72-HW1-02.

Part: STATOR VANE — FAULTY (UNKNOWN) · airframe 14,987 hrs · 3,205 cycles

ETOPS - ENG 1 COMPRESSOR VANE FAULT ON ECAM. REMOVED AND REPLACED ENG 1 HPC STATOR VANE PRIMARY ACTUATOR PER AMM 75*31-02. OPS CHECK GOOD. OK TO CONTINUE SERVICE.

Part: ROD — DAMAGED (ENGINE) · airframe 14,823 hrs · 3,171 cycles

ETOPS - DURING #1 ENGINE CHANGE FOUND ROD DAMAGED. REMOVED AND REPLACED #1 ENGINE ROD PER IPC 29-11-86-03A,OK TO CONTINUE SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,605 hrs · 3,125 cycles

OTHER - DIRTY SOCK SMELL DESCENDING THROUGH 4000' FT. PERFORMED ENG #1 AND #2 RUN, ISOLATED 1 AND 2 PACKS, APU BLEED NOTED NO SMELL TSM 71-00-00-810-847-A.

Part: TRANSDUCER — DAMAGED · airframe 13,523 hrs · 2,907 cycles

ETOPS - PASSING 10,000 FT ENG 2 FADEC SYS FAULT ECAM. PERFORMED TSM 77-11-00-710-059-A. FOUND CONNECTOR P64 ON N2 SPEED TRANSDUCER LOOSE AND TRANSDUCER PINS DAMAGED. REMOVED AND INSTALLED TRANSDUCER IAW AMM 77-11-23. OPS CHECK GOOD NO FAULTS NOTED OK TO CONTINUE

Part: ALTERNATOR — FAULTED · airframe 12,687 hrs · 2,739 cycles

ETOPS-ENG 2 FADEC SYS FAULT DURING APPROACH. PERFORMED GROUND SCAN OF EEC CH1A AND CH2B GOT "PMA SIG FAIL", FOUND CANNON PLUG TO ENG 2 PMA NOT CONNECTED PROPERLY AND PIN AND SOCKET DAMAGED. REMOVED AND REPLACED W03 HARNESS PER AMM 73-21-63, OPS CHECK GOOD OK TO CONTINUE SERVICE. REMOVED & REPLACED PERMANENT MAGNET ALTERNATOR PER AMM 73-21-04 OPS CHECK GOOD. OK TO CONTINUE SERVICE.

Part: SENSOR — FAULTED (NR 2 ENG SPEED) · airframe 12,651 hrs · 2,731 cycles

ECAM IN AIR "ENG 2 FADEC SYS FAULT" PER FPR ENG 2B-0452-N2 SPEED SENSOR FAIL. PERFORMED T/S IAWTSM 77-11-00-810-812-A. DURING FAULT CONFIRM IAW CHART NO ASSOCIATED MESSAGES. DURING ENG START UP ECAM WARNING AF ABORTED START DUE TO BOWED MOTOR OVERSPEED. PERFORM T/S IAW TSM TASK 71-00-00-810-888A. DURING INSPECTION FOUND CHAFING ON HARNESS TO N2 SPEED SENSOR. INSPECTION OF WIRE HARNESS, CHAFING ON OUTER SHEATHING ONLY. WIRES NOT COMPROMISED, RETAPED N2 SPEED SENSOR HARNESS AND RECONNECT CONNECTOR. REPLACED N2 SPEED SWITCH IAW AMM 77-11-23-000-801/77-11-23-400-801-A. OPS & LEAK CHECKED GOOD.

Part: OUTFLOW VALVE — CRACKED

REMOVED AND REPLACED AIR INLET SKIN CHECK VALVE PER AMM 21-26-56. REPLACED DUCTS DUE TO CRACKS P/N D2122891000001 & D212289090001 AND SILENCER P/N D2122953400001 PER 21-26-81. OPS AND LEAK CHECKS GOOD.

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE)

ATB-AFTER T/O SKIN AIR INLET VALVE ECAM. THROUGH 4000' FEET IN CLIMB LOUD EXPLOSION SOUND, VIBRATION, AND PRESSURE FLUCTUATIONS. TROUBLESHOOTING PER TSM AND BORESCOPE INSPECTION ARE IN-PROGRESS

Part: VALVE — INOPERATIVE · airframe 10,653 hrs · 2,215 cycles

ATB ETOPS - ACFT RETURNING TO OAK, CREW REPORTED ECAM, SKIN AIR OUTLET VLV MSG LIMITING ACFT TO FL10. PERFORMED AEVC TEST PER AMM 21-26-00-710-001-A. FOUND OUTER SKIN VALVE IN AMBER XXX. PUT THE OUTER SKIN OUTLET VALVE IN 45 DEGREES FOR DMI# 205115. REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53-400-001-A, OPS CHECK OK, NO FAULT NOTED. OK FOR SERVICE.

Part: NONE — NONE · airframe 10,258 hrs · 2,126 cycles

ETOPS - R TK PUMP 2 LO PR // REMOVED AND REPLACED PRESSURE SWITCH FIN #28QA WITH NO HELP AMM 28-21-00 PB400CONF00. NT 3263701 REMOVED AND REPLACED RIGHT TANK PUMP 2 PER AMM 28-21-51. OPS CHECK GOOD. NO LEAKS DETECTED. OK FOR SERVICE.

Part: ALTIMETER — STUCK (FIRST OFFICER'S) · airframe 7,919 hrs · 1,622 cycles

ETOPS - F/O EFIS CONTROL PANEL ALTIMETER STUCK IN STANDARD// REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS CHECK GOOD. PENDING LAND CAT 3 CAPABILITY TEST. AFS BITE TEST AND LAND CAT 3 CAPABILITY TEST PASSED.

Part: PRESSURE SENSOR — FAULTY (OIL SYSTEM) · airframe 5,754 hrs · 1,132 cycles

ETOPS SIGNIFICANT SYSTEM - MX STATUS MSG "ENG 1 FADEC". // PERFORMED FADEC 1 SYS TEST, #1 OIL PRESS SENSOR FAULTING. REMOVED & REPLACED ENG 1 OIL PRESS SENSOR PER AMM 79-33-21. MX STATUS CLEARED OK FOR SERVICE.

Part: FCU — MALFUNCTIONED (AUTOPILOT SYS) · airframe 5,675 hrs · 1,116 cycles

ATB - ETOPS SIGNIFICANT SYSTEM - FCU ALT SEL-INOP, V/S WORKS. OPEN C/B/DEC-INOP. FCU RESET ACCOMPLISHED WITH NO CHANGES. // REMOVED AND REPLACED FCU PER AMM 22-81-12. AFS TEST PASSED. LAND CAT 3 TEST PASSED. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 4,813 hrs · 942 cycles

1R ESCAPE SLIDE RAFT DEPLOYED BY CATERING SERVICE. // INSTALLED 1R ESCAPE SLIDE RAFT PACK PER AMM 25-62-44-400-803-A. SECURITY CHECK OK. OK FOR SERVICE.

Part: ENGINE — STALLED (NR 1) · airframe 4,529 hrs · 886 cycles

SUP - ATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: ENGINE — DAMAGED (NR 1) · airframe 4,529 hrs · 886 cycles

ATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 4,487 hrs · 877 cycles

ETOPS - FUEL R TK PUMP 1 LO PR // R&R RIGHT TK PUMP 1 PER AMM 28-21-51, PERFORMED OPS/LEAK CHECK WITH SATISFACTORY RESULTS. OK TO CONT. SVC.

Part: UNKNOWN — MALFUNCTIONED (AUTOLAND SYS) · airframe 3,345 hrs · 652 cycles

ETOPS SIGNIFICANT SYSTEM - AUTO LAND UNSAT, AP DISCONNECTED AT 75'. PERFORMED OPERATIONAL TEST OF THE AFS PER AMM 22-96-00-710-001-A AND OPERATIONAL TEST OF THE LAND CAT III CAPABILITY PER AMM 22-97-00-710-001-A. BOTH TEST OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,946 hrs · 574 cycles

ETOPS SIGNIFICANT SYSTEM - ECAM AIR ENG 1 BLEED ABNORMAL PR COMPLIED WITH ECAM PACK 1 OFF. PERFORMED BITE TEST IAW AMM 36-11-00. TEST OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,781 hrs · 542 cycles

ETOPS SIGNIFICANT SYSTEM - DURING DESCENT ECAM MESSAGE AIR ENG 1 BLEED ABNORMAL PR ECAM ACTIONS COMPLETED PACK 1 OFF. PERFORMED RESET AND BITE TEST OF BMC 1 AND 2 IAW AMM 36-11-00 NO FAULTS NOTED. OK FOR SERVICE.

Part: MOTOR — MALFUNCTIONED (ELEVATOR) · airframe 1,539 hrs · 302 cycles

-ATB- F/CTL ELAC 2 PITCH FAULT UNABLE TO RESET. REPLACED RELAY-PITCH ACT MOTOR 1 SUPPLY(36CE1) PER TSM 27-93-00-810-836A. CONDITION SAME. PERFORMED ALL WIRING CHECKS PER TSM 27-93-00-810-836-A.(7). CONTINUITY AND INSULATION CHECKS GOOD. PERFORMED THS - ACTUATOR LOAD SENSING DEVICE PER AMM 27-44-51 AND BITE EFCS 1&2 TEST CHECKED GOOD. NO DEFECTS NOTED OK FOR SERVICE.

Part: SWITCH — CLOSED (LUBE PUMP) · airframe 1,403 hrs · 275 cycles

ETOPS SIGNIFICANT SYSTEM - APU AUTO SHUTDOWN ON GROUND.// PERFORMED APU BITE CHECK. FAULT CODE 499141 & 499114. PERFORMED TSM TASK 49-00-81-810-849-A. MINUTE PARTICLES FOUND IN GEN SCAV FILTER. REMOVED AND REPLACED APU GEN PER AMM 24-23-51. CONDITION SAME. PERFORMED TSM TASK 49-90-00-810-812-A. DURING APU OPERATION FOUND LUBE PUMP DP SWITCH CLOSED (FAULTY). NO DEBRIS FOUND IN FILTER. REMOVED AND REPLACED LUBE PUMP DP SWITCH PER AMM 49-9-14. OPS CHECK GOOD OK FOR SERVICE.

Part: SMOKE WARNING — NONE · airframe 1,211 hrs · 238 cycles

INTERMITTENT (3 SECONDS) LAV SMOKE INDICATION ON ECAM. (SUSPECT PASSENGER VAPING - COULD NOT CONFIRM.// INSPECTED DETECTOR,OK PERFORMED GROUND SCAN NO FAULTS. ACP LAV SMOKE TEST PER 26-14-00-710-001. TEST OK.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENGINE) · airframe 1,046 hrs · 206 cycles

ETOPS SIGNIFICANT SYSTEM - BTB ENG 1 OIL CHIP DETECTED. DURING ENG START.// PERFORMED TSM 79-35-00-810-806-A FOR RELATED GROUND REPORT ENG1A-0571- LOSS OF ODM. PERFORMED TSM 77-31-00-810-807-A FOR RELATED GROUND REPORT ENG1D-0730 PHMU INTERNAL SNSR INTERFACE. NO FAULT NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (CHIP DETECTOR) · airframe 1,016 hrs · 200 cycles

ETOPS SIGNIFICANT SYSTEM - UPON ENGINE START ENG 1 OIL CHIP DETECTED ECAM DISPLAYED.// INSPECTED ALL CHIP DETECTORS PER AMM 79-00-00-281-802-A. ALL CHECK OK. RAN #1 ENGINE AND NO ECAM MESSAGES, NO LEAKS NOTED. OK FOR SVC.

Part: WARNING LIGHT — FALSE ACTIVATION (CHIP DETECTOR) · airframe 964 hrs · 190 cycles

ETOPS / ECAM UPON # 2 ENGINE START ENG 1 OIL CHIP DETECTED (BTB)// INSPECTED #1 ENGINE CHIP DETECTORS (ALL)PER AMM 79-00-00-281-802. A .WITH NO FAULTS NOTED. RAN # 1 ENG AND NO MESSAGES. NO LEAKS NOTED. OK FOR SVC

Part: WARNING MESSAGE — FALSE ACTIVATION (CHIP DETECTOR) · airframe 891 hrs · 176 cycles

ETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 1 OIL CHIP DETECTED- DISPLAYED.// INSPECTED ALL CHIP DETECTORS WITH NO FINDINGS. IDLE RAN ENGINE AND NO MESSGAE. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 828 hrs · 164 cycles

DURING NR 2 ENGINE START, ECAM FOR NR 1 ENGINE OIL CHIP DETECTOR. DURING NR 2 ENGINE CRANKING, MESSAGE DISAPPEARED. STARTED NR 1 ENGINE, ALL INDICATIONS NORMAL.. PERFORMED TSM 79-35-00-810-808-A, NR 1 ENGINE OIL CHIP DETECTOR ECAM REPORTED BY CREW WITH NO ECAM ALERT IN PFR. PULLED THE NR 1 ENGINE CHIP DETECTORS, NO DEFECTS FOUND. GROUND SCAN OF THE NR 1 AND 2 ENGINES, NO FAULTS.

Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 704 hrs · 140 cycles

ETOPS SIGNIFICANT SYSTEM - UPON AIRCRAFT POWER UP FIRE DET ENG 1 AGB ON ECAM. REMOVED AND REPLACED ENG 1 AGB FIRE LOOP PER AMM 26-12-17-000-802 AND AMM 26-12-17-400-802.

Part: NOSE COWL — DENTED (NR 1 ENGINE) · airframe 702 hrs · 139 cycles

OPEN - DURING NR 1 ENG BIRD STRIKE INSPECTION FOUND DENT ON NOSE COWL LIP AT APPROX 2 O'CLOCK POSITION. FWD LOOKING AFT. REPAIR IN WORK.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 610 hrs · 121 cycles

ETOPS SIGNIFICANT SYSTEM - BTB ECAM ENG 1 IL CHIP DETECTED. PERFORMED TSM 79-35-00-810-808-A CHECK MAIN ENG NR 1 OIL FILTER PER AMM 79-00-00-210-809. NO PARTICALS NOTED. REMOVED AND REPLACED OIL FILTER AS PRECAUTION. CHECK MAGNETIC CHIP DETECTORS (5 EA). NO DEFECT NOTED. IDLE RUN ENG NR 1 FOR 5 MIN. NO LEAK NOTED. MSG CLEARED. OK FOR SVC.

Part: CARBON SEAL — DAMAGED (NR 2 ENGINE) · airframe 1,042 hrs · 203 cycles

SUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE CHIP DETECTOR. FOUND AFT CARBON SEAL BAD. REMOVED AND REPLACED NR 2 ENGINE. OP'S AND LEAK CHECK OK.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 1,042 hrs · 203 cycles

NR 2 ENGINE OIL CHIP DETECTOR ACTIVATED. FOUND AFT CARBON SEAL BAD. REMOVE AND REPLACED THE NR 2 ENGINE.

Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 421 hrs · 85 cycles

ATB - ON CLIMB OUT F/O ND DISPLAYED "GPS PRIMARY LOST" CHECKED NAVIGATION ERROR W/GROUND BASED VOR AND NAV ERROR +/- 6-7 / +1.0 DME. MCDUS SHOWED ACCUR HIGH, GPS PRIMARY, GPS MONITOR WAS NAV WITH 9 SATS EACH. PERFORMED AMM 34-55-00 BITE TEST OF VOR AND PERFORMED OPS CHECK VOR GOOD ON GROUND.

Part: METERING UNIT — MALFUNCTIONED (NR 1 ENGINE) · airframe 134 hrs · 27 cycles

NR 1 ENGINE OIL CHIP DETECTED DURING ENGINE START, SHUTDOWN THE ENGINE. PERFORMED TSM 79-35-00-810-808-A, EXAMINED THE W03 HARNESS & P10 CONNECTOR ON PHMU & P36 CONNECTOR ON OIL DEBRIS MONITORING SENSOR, NO DEFECTS NOTED. EXAMINED PINS & SOCKETS ON P10 ON THE PHMU SIDE & P36 ON THE ODM SIDE, NO DEFECTS NOTED. PERFORMED RESISTANCE & CONTINUITY CHECKS OF ODM SIGNAL WIRES FROM P10 TO P36, NO DEFECTS NOTED IAW TSM 79-35-00-810-808-A, FIGURE 79-35-00-991-00600-A21, SHEET 1. REMOVED AND REPLACED THE ODM IAW AMM 79-35-21-000-801-A, AND AMM 79-35-21-400-801. LEAK CHECKED OK IAW TEST 3, AMM 71-00-00-720-811-A. DURING TEST 6 PREP, FADEC SYSTEM STATIC TEST, THE NR 1 ENGINE OIL CHIP DETECTOR ECAM REMAINS. PHMU REMOVED AND REPLACED IAW AMM 77-31-01. RAN BOTH ENGINES STABILIZED FOR 5 MINUTES, NO FAULTS OR ECAM MESSAGES NOTED. OK FOR SERVICE.