N230HA

Part: PUMP — FAULTED (HYD SYS) · airframe 16,475 hrs · 3,639 cycles

ETOPS - AT CRUISE ECAM B SYS LO PR, FOLLOWED BY B RSVR LO LVL. ECAM ACTIONS COMPLETED, (SHUTDOWN B ELEC PUMP) NO FURTHER ACTIONS. REMOVED AND REPLACE BLUE ELECTRIC PUMP PER AMM 29-12-51. PERFORMED TEST OF BLUE ELEC PUMP PER AMM 29-12-00. TEST OK. NO LEAKS NOTED. OK FOR SERVICE

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 14,006 hrs · 3,146 cycles

ETOPS - IN CRUISE AT FL320 ENG 2 FIRE LOOP B FAULT. REMOVED RH ENG AFT FIRE/OVERHEAT DETECTOR 4001WD2 PER AMM 26-12-17-000-803A. INSTALLED RH ENG FIRE/OVERHEAT DETECTOR 4001WD2 PER AMM 26-12-17-400-803-A. OPS CK GOOD. SECURITY CK GOOD.

Part: PACKING — LEAKING (ENGINE CONE) · airframe 13,835 hrs · 3,111 cycles

ETOPS - FOUND OIL STAINING @ BOTH ENG'S INLET CONE WEEP HOLES WHILE ACCOMPLISHING HAL CARD E1128-321-21-008-1. REPLACED BOTH ENGS FAN SHAFT COVERS PACKING PER AMM 72-15-00-960-801-A.LEAK CHK OK.

Part: DIVERTER — CLOGGED (ZONE 100) · airframe 13,770 hrs · 3,094 cycles

DIV - ALL LAVS STOPPED FLUSHING IN FLIGHT. FL 360 2 HOURS INTO THE FLIGHT. ATTEMPTED RESET OF VACUUM SYSTEM VIA A5 CB ON AFT GALLEY OVHD PANEL PER MAINT DIRECTION WITHOUT SUCCESS. FOUND EXCESSIVE BUILD UP OF WASTE ON DIVERTER, FLUID LEVEL SENSOR, AND WASTE TRANSMITTER. REMOVED/WASHED OUT BUILD UP FROM WASTE TANK. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SVC.

Part: SENSOR — FAILED (TOILET) · airframe 13,749 hrs · 3,090 cycles

DIV - ALL LAVS NOT FLUSHING ALL THE WAY UP TO FC. REMOVED AND REPLACED WASTE LIQUID LEVEL SENSOR (41MG) PER AMM 38-31-63. OPS CHECK GOOD. LEAK CHECK GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 13,605 hrs · 3,061 cycles

ETOPS - ENG #2 DURING THE WALKAROUND OIL WAS DISCOVERED DRIPPING CONTINOUSLY. REMOVED & REPLACED #2 ENGINE ENGINE DRIVEN PUMP PER AMM 29-13-51. OPS CHECK GOOD PER #2 ENGINE RUN. NO LEAKS NOTED. OK FOR SERVICE.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 13,459 hrs · 3,027 cycles

ETOPS-BTB DUE TO ECAM: CAB PR SYS 1 FAULT. SWAPPED CPC 1 & CPC 2. OPS CHK NORMAL PER AMM 21-31-00.

Part: SMOKE DETECTOR — NO DISCREPANCY (LAVATORY) · airframe 13,321 hrs · 2,998 cycles

SMOKE LAVATORY SMOKE OCCURRED AT FL290 JUST PIROR TO THE ETP AT 0248Z TRANSIET ALERT DUE TO PASSENGER VAPING IN THE FORWARD LAV NO SMOKE OR FIRE PRESENT. PERFORMED OPERATIONAL CHECK OF LAV SMOKE DETECTION IN ACCORDANCE WITH AMM 26-17-00-710-001-A OPERATIONAL CHECK GOOD OK TO CONTINUE.

Part: SENSE LINE — MISINSTALLED (ZONE 100) · airframe 12,606 hrs · 2,851 cycles

ETOPS - WHILE PERFORMING T/C E36-24-01-32 FOUND HPV SENSE LINE & UNION CROSS THREADED. INSTALLED NEW MUSCLE SENSE LINES FOR HPV PER AMM 36-11-49 OPS CHECK & LEAK CHECK GOOD IDLE RUN SUCCESSFUL

Part: WIRE HARNESS — DAMAGED (NR 1) · airframe 12,500 hrs · 2,829 cycles

ATB - AIR TURN BACK DUE TO ENG 1 SYS FAULT ON CLIMB OUT. REMOVED AND REPLACED WO3 HARNESS PER AMM 73-21-63 OPS CHECK GOOD. PENDING BIFFLE INSTALL. INSTALLED BIFFLE PER AMM 73-21-63. OK FOR SVC.

Part: FADEC — FAULTED (NR 1) · airframe 12,500 hrs · 2,829 cycles

ETOPS - ENG 1 FADEC SYS FAULT. REMOVED AND REPLACED N2 SPEED TACHOMETER PER AMM 77-11-23-400-801-A PENDING OPS CHECK. REMOVED AND REPLACED ENG 1 ECC PER AMM 73-21-34 UP TO STEP 5(2)A. COMPLETED REMAINING STEPS OF 73-21-34. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,338 hrs · 2,397 cycles

ETOPS - APU AUTO SHUTDOWN. PERFORMED TSM 49-00-81-810-825-A. CONFIRMED FAULT "IGNITION UNIT SHOWS OPEN CIRUIT." REMOVED AND REPLACED IGNITION UNIT, ELECTRICAL LEAD, AND IGNITER PLUG PER AMM'S 49-41-38, 49-41-41, AND 49-41-43. OPS CHECK GOOD, MESSAGE CLEARED. OK FOR SERVICE.

Part: TRANSDUCER — FAULTED (UNKNOWN) · airframe 10,060 hrs · 2,342 cycles

WHEEL TIRE PRESS LOW #2 ECAM 70-80PSI AT CRUISE DIVERTED TO HNL. REPLACED # 2 MLG TIRE PRESSURE TRANSDUCER REF AMM 32-49-16. OPS CHECKS GOOD. OK TO CONTINUE SERVICE. PLACARD REMOVED, MIC SHEET UPDATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,956 hrs · 2,322 cycles

ETOPS-ENG 1 OIL CHIP DETECTED. REMEOVED AND REPLACED #1 ENG PER AMM 71-00-51

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,945 hrs · 2,320 cycles

ETOPS - ENG 1 OIL CHIP DETECTED ECAM AFTER LANDING. PERFORMED MAGNETIC CHIP INSPECTION PER AIRBUS TSM 79-35-00-810A-808A. NO DEBRIS FOUND ON CHIP DETECTOR OR OIL FILTER. REMOVED AND REPLACED OIL FILTER. NO LEAKS NOTED NO DEFECTS NOTED. OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,940 hrs · 2,319 cycles

ETOPS - ENG 1 OIL CHIP DETECTED. PERFORMED MAGNETIC CHIP INSPECTION PER AMM 79-00-00-281-802A. NO DEBRI FOUND-CHECK GOOD. INSPECTED MAIN OIL FILTER & REPLACED PER AMM 79-21-06-960-801A. OPS CHECK GOOD. ENG IDLE RUN SATISFACTORY. A/C OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,555 hrs · 2,233 cycles

ETOPS - FOUND NACELLE ANTI-ICING DUCT DAMAGE. REMOVED AND REPLACED NACELLE ANTI-ICING DUCT PER AMM 30-21-49-000-807-A, OPS CHECKS GOOD, OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,549 hrs · 2,231 cycles

ETOPS - ENGINE 1 DIFF 1 BORESCOPE PLUG FOUND DAMAGED DURING BORESCOPE INSPECTION. #1 ENGINE REPLACED. ENG 1 VERIFICATION FLIGHT DUE TO ENG REPLACEMENT COMPLETED SUCESSFULLY. NO DEFECTS NOTED OK TO CONTINUE SVC.

Part: EEC — FAULTY (UNKNOWN) · airframe 9,140 hrs · 2,149 cycles

ETOPS - ENG 2 FUEL VALVE FAULT (FUEL VALVE NOT OPEN) ON ECAM AFTER ACCOMPLISHED OF TASK CARD # E73-23-01-32 (EEC SOFTWARE DATA LOAD). REMOVED AND REPLACED ENG #2 EEC PER AMM 73-21-01. ENGINE IDLE TEST GOOD, NO FAULTS NOTED. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,909 hrs · 2,102 cycles

ETOPS - WHILE PERFORMING BORESCOPE, FOUND #2 IGNITER PLUG WORN. REMOVED AND REPLACED #2 IGNITER PLUG PER AMM 74-21-01. OPS CHECK GOOD, OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 8,353 hrs · 1,985 cycles

MOMENTARY ENG 2 FIRE LOOP B FAULT ECAM IN CRUISE. NO FAULTS NOTED ON ECAM. PERFORMED BITE TEST OF FDU. NO FAULTS NOTED. OK FOR SVC IAW AMM 26-12-00.

Part: RADAR — FAULTY (WX SYSTEM) · airframe 8,266 hrs · 1,968 cycles

ETOPS - DMI# 206909 WX RDR 2 GCS DOES NOT WORK ( WEATHER RADAR SYSTEMS TRANSCEIVER (AIRCRAFT WITH DUAL TRANSCEIVERS) (MAY BE INOPERATIVE). REMOVED AND REPLACED WEATHER RADAR TRANSMITTER PER AMM 34-41-33 BITE TEST OKAY NO FAULTS DETECTED PLACARD REMOVED MIC SHEET CLEARED

Part: WIRE HARNESS — FAULTY · airframe 7,750 hrs · 1,866 cycles

ETOPS - DMI 206624 - [ENG 1 FUEL FILTER CLOG] FILTER REPLACED 50FH ( FUEL FILTER CLOG CAUTIONS ON ECAM E/W PW100G ENGINES (ONE MAY BE INOPERATIVE PROVIDED ASSOCIATED FILTER IS CHANGED BEFORE THE NEXT FLIGHT AND THEN EVERY 50 FLIGHT HOURS) ) REMOVED AND REPLACED W03 HARNESS, PER AMM 72-21-63 AND REMOVED AND REPLACED W04 HARNESS, PER AMM 73-21-64. PERFORMED IDLE ON BOTH ENGINES, NO FAULT NOTED. OPS CHECK GOOD. DMI# 206627, PLACARD REMOVED. MIC SHEET UPDATED. CLEARS BOTH DMI #206624 AND #206627

Part: UNKNOWN — UNKNOWN · airframe 7,687 hrs · 1,853 cycles

ETOPS - RECEIVED MULTIPLE ENG 1 FUEL SENSOR FAULT AND ENG 1 FUEL FILTER CLOG MESSAGES THROUGHOUT THE FLIGHT. ITEM ALREADY ON DEFERRAL, REMOVED AND REPLACED WC08 WIRING HARNESS PER AMM 73-31-21, OPS CHECK GOOD OK TO CONTINUE SERVICE

Part: NONE — NONE · airframe 7,641 hrs · 1,844 cycles

ETOPS - ENG 1 FUEL FILTER CLOG ECAM INFLIGHT. REMOVED AND REPLACED FUEL FILTER IAW AMM 73-11-06-400-801-A. OPERATIONAL CHECK PERFORMED. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: WIRE HARNESS — DAMAGED · airframe 7,629 hrs · 1,842 cycles

ETOPS- ENG 1 FUEL SENSOR FAULT HAPPENED 8 TIMES. FOUND DAMAGE ON WC08 WIRING HARNESS AFT OF FUEL FLOW SENSOR CONNECTOR (P27) REMOVED & REPLACED WC08 HARNESS PER AMM 73-31-21. NO FAULTS NOTED.

Part: PRESSURE SENSOR — FALSE INDICATION · airframe 7,619 hrs · 1,840 cycles

ETOPS-ENG 1 FUEL SENSOR FAULT FUEL FILTER SENSOR CAME ON 15 TIMES THROUGHOUT THE FLIGHT CLEARED ITSELF EVERYTIME. REMOVED AND REPLACED FUEL PRESSURE SENSOR IAW AMM 73-34-21-400-801-A AND 73-34-21-000-801-A. OPS CK GOOD.

Part: WIRE HARNESS — FAULTED (FIRE LOOP A) · airframe 7,000 hrs · 1,716 cycles

ETOPS, NR 1 ENGINE FIRE LOOP A FAULT MESSAGE ILLUMINATED, 15 MINUTES AFTER DEPARTURE AND REMAINED ON. AIRCRAFT DIVERTED TO HNL. REPLACED THE FIRE LOOP A, FIRE ELECTRICAL HARNESS IAW AMM 26-12-61-400-802-A, AND REPLACED FWD FIRE DETECTOR IAW AMM 26-12-17-400-A. OPS TESTED GOOD.

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 6,970 hrs · 1,709 cycles

ETOPS - ECAM ENG 1 FIRE LOOP A FAULT PRIOR ENGINE START. REMOVED AND REPLACED LOOP-A FIRE DETECTORS CABLES PER AMM 26-12-61, AND REMOVED AND REPLACED FDU1 PER AMM 26-12-34. REMOVED AND REPLACED FWD AGB LOOP A PER AMM 26-12-17. FOUND FIRE ELECTRICAL HARNESS LOOP A FRAYED. REMOVED AND REPLACED HARNESS PER AMM 26-12-61. OPS CHECK GOOD PERFORMED IDLE RUN NO FAULTS NOTED. OK TO CONTINUE SERVICE.

Part: NONE — NONE · airframe 5,897 hrs · 1,488 cycles

ETOPS - ON TAXI IN APU AUTO SHUTDOWN // R/R EXCITER BOX IAW AMM 49-41-38 PB 401 OPS CHECK OKAY, A/C OK FOR SERVICE

Part: NONE — NONE · airframe 4,132 hrs · 964 cycles

BTB AFTER ENGINE STARTS FWD CRG HEAT / FWD CRG VENT // PERFORMED RESET AND BITE TEST IAW AMM 21-28-00. NO FAULTS NOTED AT THIS TIME.