N208HA
Registered owner: HAWAIIAN AIRLINES INC, HI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Hawaiian Airlines | Operator | 2021-09-23 – 2021-09-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
ATB: ENG #1 HYD GREEN LO PRESSURE. GROUNDED - YES. REPLACED#1 ENG PUMP PRESSURE SWITCH (FIN 1074GK) PER AMM 29-11-17. 17261 05/29/26 PENDING WIRING, OPS & LEAK CHECK. PENDING WIRING, OPS && LEAK CHECK. REPAIRED WIRING TO 1074GK PER ESPM 20-53-22 OPS CHECK PENDING 27031. PERFORMED OPS CHECK PER AMM 29-11-00-710-001-A. OPS CHECK GOOD.
DIV - AVIONICS DOOR OPEN IN FLIGHT MESSAGE A/C NOT PRESSURIZING NORMALLY. PERFORMED VISUAL INSPECTION OF AVIONICS DOOR. PERFORMED PRESSURIZATION TEST FOR AIR LEAKS PER AMM 05-53-00. NO DEFECTS NOTED. OK TO CONTINUE.
ETOPS - FUEL LEAK COMING OUT LH AND RH WING DRY BAY WEEP HOLES. REPAIRED BOTH LEFT & RIGHT WING DRY BAY FUEL LEAKS IN ACCORDANCE WITH SRM 51-76-12. PERFORMED LEAK TEST PER AMM 28-11-00. NO LEAKS NOTED.
ETOPS - ENG 2 IGN A FAULT DURING START. REMOVED AND REPLACED IGN A IGNITER PLUG ON ENG 2 PER AMM 74-21-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE
ETOPS - MCDU'S DON'T MATCH WHEN IT COMES TO FUEL PREDICTION, TIME PREDICTION, AND VERTICAL PATH ERROR. FO'S MCDU APPEARS TO SHOW TIME: 4 MINUTES EARLIER, FUEL BURN: 400 MORE POUNDS, ABOVE DESCENT PATH: 400 FEET. REMOVED AND REPLACED FQIC PER AMM 28-42-34-04. NO DEFECTS NOTED OK FOR SERVICE.
ATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUE
ETOPS-BTB: APU FAIL. REPLACED APU IGNITOR PLUG AND LEAD REF AMM 49-41-41 AND 49-41-43, OPS TEST NORMAL. OK FOR SVC.
ETOPS - BEFORE TOW OPERATIONS, ATTEMPTED TO START APU, "APU AUTO SHUT SHUTDOWN" MESSAGE SHOWN ON ECAM. APU GRANDSCAN CONFIRMS "OIL FILTER SWITCHES" FAULT. CLEAN CONNECTORS P5 & P9 IAW TSM 49-90-00-810-812-A. APU START NOT SUCCESSFUL. REMOVED & INSPECTED PRESSURE SWITCHES IAW AMM 49-91-14. NO DEFECTS NOTED. REINSTALLED- APU START NOT SUCCESSFUL. REMOVED & REPLACED OIL FILTERS IAW AMM 49-91-41. APU START NOT SUCCESSFUL. REMOVED & REPLACED IGNITION EXCITERIAW AMM 49-4-38-400-003-A. REMOVED & REPLACED BOTH OIL FILTER SWITCHES IAW AMM 49-91-14400-002-A. OPS CK GOOD. APU GROUNDSCAN-NO FAULT DETECTED. A/C OK FOR SVC
ETOPS - FOUND APU OIL FILTERS CLOGGED. REMOVED AND REPLACED APU OIL FILTERS PER AMM 49-91-41-200-002-A. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.
ETOPS - PACK 2 FAULT PRIOR TO DEPARTURE. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK / LEAK CHECK OK.
ETOPS - APU FAULT ON TAXI OUT BTB. ITEM ALREADY ON DMI, REPLACED AND RESECURED PINS/ JUMP CONNECTORS PER AMM 49-16-00-003-A OPS CHK OF APU GOOD OK TO REMAIN ON DMI.
ABORTED TO @ 30-40 KTS PSEU AND STICK PUSHER FAIL MSG. PERFORMED SLAT DISAGREE BITE PER FIM 27-80 TASK 803. COULD NOT DUPLICATE FAULT. OK TO CONTINUE
ETOPS - #1 ENG OIL NEAR FAN BLADES (OIL BLADES). REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING IDLE POWER TEST GOOD. LK CK GOOD. OK FOR SERVICE IAW AMM 72-15-00-960-801-A
ETOPS - APU AUTO SHUTDOWN TWICE DURING PREFLIGHT. PERFORMED BITE TEST, FAULTED GEN SCAV AND LUBE FILTERS. REMOVED AND REPLACED BOTH FILTERS IN REF W/ AMM 49-91-41-200-002-A. APU OPS CHECK GOOD. LEAK CHECK GOOD. NO LEAK NOTED. OK FOR SVC.
ETOPS - APU: AUTO SHUT DOWN ON TAXI IN 3X ATTEMPTS FAILED. REMOVED & REPLACED WIRING FROM APU STARTER MOTOR + TERMINAL LUG TO 7120VC PIN 1. WIRES X011A20, X011B14, X011C14 PER ESPM 20-33-11. REMOVED & REPLACED APU STARTER MOTOR CLUTCH PER AMM 49-42-52. PERFORMED OPS TEST OF APU PER AMM 49-00-00, OPS TEST GOOD. OK FOR SERVICE.
ETOPS - HYD LEAK COMING FROM LH AFT DRAIN MAST. REMOVED AND REPLACED PACKING ON # 1 ENG HYD PUMP PRESSURE SWITCH PER AMM 29-11-17, OPS AND LEAK CHECK OKAY.
ETOPS - SAW A FEW DROPS OF OIL UNDER #1 ENGINE FAN COWL. FOUND LP05 OIL MANIFOLD DRAIN PLUG MISSING SCREW REF PIPC 79-21-49-01 ITEM 320 & 140 & 150. INSTALLED MISSING BOLT P/N: ST2601-06. NO LEAKS NOTED OK FOR SERVICE.
FOUND EMER LT/EPSU (12WL) INOP DURING SERVICE CHECK. REMOVED AND REPLACED EPSU BATTERYPER AMM 33-51-38. BITE TEST GOOD. OK FOR SERVICE
ETOPS - HYDRAULIC OIL LEAKING FROM RH ENGINE. REMOVED AND REPLACED O RING SEAL IN COUPLING HALFT FROM YELLOW HYDRAULIC SYSTEM PER AMM 29-13-39. LEAK CHECK WITH DRY MOTOR OF ENGINE PER AMM 71-00-00-860-817A GOOD. NO FAULTS. OK FOR SERVICE
ETOPS - 1L DOOR HANDSET UNREADABLE ON INTERCOMAND PA. REMOVED AND REPLACED 1L DOOR HANDSET. OPS CHECK GOOD. OK FOR SERVICE PER AMM 23-73-44.
ETOPS - ENG 2 FIRE LOOP A FAULT ON ECAM PAGE. REMOVED AND REPLACED FIRE DETECTOR ELECTRICAL LOOP A PER AMM 26-12-61-000-807-A. OPS CHECK GOOD. OK FOR SERVICE.
SUPPLEMENTAL SUBMISSION TO HALA2023041300086. CORRECTION FROM REGISTRATION # 217HA TO 208HA. ATB - AFTER REACHING CRUISE ALT FL340 ENG 1 START VALVE FAULT ECAM. VERIFIED START VALVE POS CLOSED, MOVED FREELY (REF TSM 80-11-00-810-828-A) REMOVED AND REPLACED #1 STARTER PER AMM 80-AA-01. LEAK CHECK AND OPS CHECK GOOD.
ETOPS - DUIRNG T/C 321-72-HWI-03 LEAK CHECK FOUND PRV MUSCLE TUBE CRACKED AND LEAKING BLEED AIR. REMOVED AND REPLACED PRV MUSCLE TUBE IAW AMM 36-11-52-000-802-A. AND 36-11-52-400-802-A. OPS CK GOOD. LEAK TEST GOOD. OK TO CONTINUE.
SUPPLEMENTAL TO HALA2023032000051. UPDATED WITH RESOLUTION. ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). REMOVED AND INSTALLED VENT EXTRACT FAN PER AMM 21-26-51-00. PERFORMED OPERATIONAL TEST OF VENTILATION SYSTEM PER AMM 21-26-00-710-001-A. OPS CHECK GOOD. PLACARD REMOVED MIC SHEET UPDATED.
ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). AWAITING RESOLUTION.
ETOPS - DMI# 206657 ENG 1 FIRE LOOP B FAULT IN CRUISE ( ENGINE FIRE DETECTION SYSTEMS LOOP B (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE PROVIDED: ASSOCIATED LOOP A IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DEPARTURE) ) TROUBLESHOT PER TSM 26-12-00-810-804-A. FOUND PYLON LP "B" DETECTOR (4WD1) INTERNAL SHORTING TO GROUND. NEED TO REPLACE #1 ENGINE PYLON DETECTOR LP "B". REMOVED AND REPLACED, #1 ENGINE PYLON DETECTOR LOOP "B", PER AMM 26-12-16. OPS CHECK GOOD. MIC SHEET CLEARED, PLACARD REMOVED.
ETOPS - AVNCS SYS FAULT DURING PREFLIGHT. FOUND INLET BYPASS V (16HQ) FAULT. DEFERRED PER MEL 21-26-03. REF TSM 21-26-00-810-806-A, CHSNGED INLET BYPASS VALVE (16HQ), CONDITION SAME. REMOVED & REPLACED AEVC COMPUTER. BITE CHECK GOOD, NO FAULTS NOTED. PLACARD RMVD, MIC SHEET UPDATED.
ETOPS - APU LEAK DETECT FAULT ON ECAM. PERFORMED TSM 36-22-00-810-876-A. FOUND ELEMENT SESOR (15HF) SHORTED TO GRN. REMOVED AND REPLACED OVHT SENS ELEMENT (15HF) PER AMM 36-22-17-400-001 BITE TESET GOOD. OK FOR SVC.
ETOPS - AT 8000' "ENG 2 FADEC SYS FAULT THRUST LEVER 2 NOT ABOVE IDLE" THRUST LEVERS WERE IN CL DETENT // PERFORMED INSPECTION OF ENG #2 EEC AND N2 SPEED TRANSDUCER HARNESS & CONNECTIONS PER TSM 77-11-00. CHECKS OK. REMOVED & REPLACED ENG #2 N2 SPEED TRANSDUCER PER AMM 77-11-23. NO FAULTS NOTED. OK FOR SVC.
ETOPS - STATUS MSG , ENG # 1 FIRE LOOP A FAULT // RESET FDU 1 C/B'S PER AMM 26-12-34, AS PRECAUTIONARY REMOVED AND REPLACED FDU 1 CAS6465, RAN # 1 ENG AT IDLE FOR FIVE MINUTES NO FAULTS NOTED, OPS CHECK GOOD , OK FOR SERVICE
BTB 1 - SPEED LIMIT DISPLAYED ON BOTH PFDâS FD+SPD LIM RED INDICATIONS // RE-SET A/C TO NORMAL CONDITIONS. BOTH PFD FD AND SPD LIM INDICATIONS ARE ABSENT. INDICATIONS READING NORMAL.
BTB 2 - SELECTING FLAPS 1 ECAM F/CTL FLAPS FAULT // PERFORMED BITE OF SFCC PER AMM 27-54-00. FAULTING SFCC2 22CV. REMOVED AND REPLACED SFCC2 PER AMM 27-51-34, OPS CHECK GOOD. OK FOR SVC
DURING PDC FOUND BOTTOM TAIL AREA FUSELAGE SKIN DAMAGE AND AFT GALLEY DRAIN MAST DAMAGE. DAMAGE AREA: FRAME 61-70, STRINGER 42LH - 40 RH. 176" LONG 22" WIDE // REPAIRED DAMAGE TO BOTTOM TAIL AREA AT FRAME 61-70 STRINGER 42LH-40RH AS PER AIRBUS WOTD: M-308924-EMBOD 12/30/21 MECH 2590 INSP 12559
ETOPS - ENG 1 FIRE LOOP A FAULT DURING TOW UP, FAULTING ENG 1 LOOP A CORE AND AGB LOOPS FOUND LOOSE CLAMP AND WIRE ON LOOP A HI TEMP WIRE HARNESS. SECURED CLAMP AND ADJUSTED SLACK ON HARNESS REPLACED ENG 1 LOOP A CORE DETECTOR PER AMM 26-12-17. ALL OPS CHECK GOOD
ETOPS - ENG2 FIRE LOOP A. PERFORMED TSM26-12-00-810-825-A & TSM 26-12-00-810-914-A. REPLACED ENG2 FIRE LOOP A PER AMM26-12-16-400-803-A AND INSTALLED PYLON FIRE DETECTOR IAW AMM 26-12-16-400-802-A. SECURITY CHECKED GOOD. RAMP ASSY.AMM26-12-00-710-001.SECURITY CK,OPS TEST OK. BIE FDU & BMC2 NO FAULTS, OPS CHECKED GOOD. P/N OFF/ON:8891-48. S/N OFF:D0069794,P/N ON 8891-48 S/N ON:D0042882
ETOPS - PASSING FLI 80 "ENG 2 FIRE LOOP B FAULT" MSG. MSG CLEARED AFTER APPROX 5 MINS. REPEAT WRITE UP. FOUND ENG 2 LOOP B INTERMITTENT. PERFORMED CONTINUITY CHECK PER TSM 26-12-00. NO FAULT NOTED. PRECAUTIONARY ACTION, REMOVED AND REPLACED FWD FIRE LOOP ASSY PER AMM 26-12-17, STEPS 1 THRU 4.B. OPERATIONAL CHECK OK PER AMM 26-12-00-710-801-A.
ETOPS - ECAM ENG2 FIRE LOOP A FAULT, REMOVED AND REPLACED FIRE DETECTOR ENG 2 LOOP A PYLON IAW AMM 26-12-16 OPS CHECK OK NO FAULTS NOTED.
ETOPS - #2 FIRE LOOP A FAULT // FOUND ENGINE 2 PYLON DETECTOR LOOP A (3WD2) BROKEN. REMOVED PYLON FIRE-DETECTOR RAMP ASSY PER A321 AMM 26-12-16-000-802-A. 21402. 3/29/21.
ETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CHECK. LEAK CHECK GOOD. OK TO CONTINUE.
ETOPS: ECAM - ENG 2 FIRE LOOP A FAULT ON CLIMB. REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECKED OK.
SUP - ECAM: ENG. 2 FIRE LOOP A FAULT ON CLIMB. // REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECK OK. OK FOR SERVICE.
ETOPS SIGNIFICANT SYSTEM - AFTER GO AROUND ECAM "ENG 1 START VALVE FAULT. START VALVE NOT CLOSED" COMPLIED WITH ECAM ACTIONS. // PERF EEC OPS TEST NO.6 PER AMM 73-21-00-710-807-A. NO DEFECTS NOTED.
ETOPS SIGNIFICANT SYSTEM - ENGINE 2 START VALVE FAULT, VALVE NOT CLOSED. REMOVED AND REPLACED STARTER ON ENGINE 2, PER AMM 80-11-01. OPS CHECK GOOD. OK TO CONTINUE.
ATO - BRAKE SYSTEM 2 FAULT CAME ON @ TAKEOFF POWER. ABORTED TAKEOFF RESET A/SKID AND N/W STEG. RESET SUCCESSFUL. NO INBOUND FAULTS. PREFORMED TROUBLESHOOTING IN REF. WITH TSM 32-51-00-810-514-A. NO DEFECTS NOTED. OKAY FOR SERVICE.
LAVATORY SMOKE ECAM IN-FLIGHT, PAX SUSPECTED OF SMOKING IN LAV D. CHECKED LAV D SMOKE DETECTOR & WASTE BIN FIRE EX, NO FAULTS FOUND. PERFORMED CIDS SDF1 LAV SMOKE WARN TEST NO FAULTS. OK FOR SVC. REF AMM 26-17-00
LAV C SMOKE WARNING WENT OFF FOR SEVERAL SECONDS AND FA'S VERIFIED OPS NORMAL WITH NO SMELL. T/S PER TSM 26-16-17-00-810-812-A. OPS CKS GOOD, OK TO CONTINUE.
ATB - VENT SKIN VALVE FAULT. // FOUND MAIN SKIN AIR OUTLET VALVE IN PARTIALLY OPEN POSITION, MANUALLY OPENED VALVE TO FULL OPEN. ACCOMPLISHED AEVC TEST TWICE, BOTH PASSED. VALVE OPS OK.
DURING FLIGHT LAV SMOKE WARNING, FA PANEL INDICATED LAV 1, NO SMOKE FOUND.// NO SMOKE DETECTED, NO SMOKE INDICATED. OK FOR SERVICE PER AMM26-17-01.
ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A INOP. PERFORMED OPERATIONAL CHECK OF #2 ENGINE IGNITER "A" OPS CK NORMAL ON GROUND. OK TO CONTINUE. REF AMM 74-00-00 PB 501.
ETOPS SIGNIFICANT SYSTEM - ATB - DUE TO ENG. 2 LOOP "A" FAULT. // REMOVED AND REPLACED PYLON FIRE - DETECTOR RAMP ASSEMBLY PER AMM 26-12-16. EMPLOYEE# 3752 (11/14/18). OPERATIONAL CHECK PENDING. OPS CHECK GOOD PER AMM 26-12-00-710-002, FAULT WENT AWAY AND NO DEFECTS NOTED.