Aircraft Report for n214ha



Registration History for n214ha



N-Number Make Model Serial Location Description Time
N214HA AIRBUS A321-271N 8157 HONOLULU, HI Aircraft registered to HAWAIIAN AIRLINES INC, airworthiness date 2018-07-19, expiration date 2024-07-31, serial number 8157. 2021-03-03
N214HA AIRBUS A321-271N 8157 HONOLULU, HI Aircraft registered to HAWAIIAN AIRLINES INC, airworthiness date 2018-07-19, expiration date 2021-07-31, serial number 8157. 2018-07-19

Service Difficulty Reports for n214ha






























N-Number Make Model Serial Description Time
N214HA AIRBUS A321271N During CLIMB - 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. 2022-11-14
N214HA AIRBUS A321271N During CLIMB - ATB-AFTER T/O SKIN AIR INLET VALVE ECAM. THROUGH 4000' FEET IN CLIMB LOUD EXPLOSION SOUND, VIBRATION, AND PRESSURE FLUCTUATIONS. TROUBLESHOOTING PER TSM ANDBORESCOPE INSPECTION ARE IN-PROGRESS 2022-11-10
N214HA AIRBUS A321271N During CLIMB - 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. 2022-05-11
N214HA AIRBUS A321271N During UNKNOWN - 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. 2022-03-24
N214HA AIRBUS A321271N During NOT REPORTED - 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. 2021-11-30
N214HA AIRBUS A321271N During CLIMB - 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 CHECKGOOD. OK FOR SERVICE. 2020-06-23
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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. 2020-05-19
N214HA AIRBUS A321271N During INSP/MAINT - 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. 2020-03-20
N214HA AIRBUS A321271N During CRUISE - 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. 2020-03-11
N214HA AIRBUS A321271N During NOT REPORTED - 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. 2020-03-11
N214HA AIRBUS A321271N During CLIMB - SUP - ATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAKCHECK GOOD. OK FOR SERVICE. 2020-03-11
N214HA AIRBUS A321271N During APPROACH - 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. 2019-12-10
N214HA AIRBUS A321271N During NOT REPORTED - ETOPS SIGNIFICANT SYSTEM - ECAM AIR ENG 1 BLEED ABNORMAL PR COMPLIED WITH ECAM PACK 1 OFF. PERFORMED BITE TEST IAW AMM36-11-00. TEST OK. 2019-11-14
N214HA AIRBUS A321271N During DESCENT - 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. 2019-10-09
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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. 2019-08-30
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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. 2019-08-05
N214HA AIRBUS A330243 During CRUISE - -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 FORSERVICE. 2019-08-01
N214HA AIRBUS A321271N During CRUISE - 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. 2019-07-24
N214HA AIRBUS A321271N During TAXI/GRND HDL - ETOPS SIGNIFICANT SYSTEM - BTB ENG 1 OIL CHIP DETECTED. DURING ENG START.// PERFORMED TSM 79-35-00-810-806-A FOR RELATEDGROUND 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. 2019-07-17
N214HA AIRBUS A321271N During TAXI/GRND HDL - ETOPS SIGNIFICANT SYSTEM - UPON ENGINE START ENG 1 OIL CHIP DETECTED ECAM DISPLAYED.// INSPECTED ALL CHIP DETECTORS PERAMM 79-00-00-281-802-A. ALL CHECK OK. RAN #1 ENGINE AND NO ECAM MESSAGES, NO LEAKS NOTED. OK FOR SVC. 2019-07-12
N214HA AIRBUS A321271N During INSP/MAINT - 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. 2019-07-10
N214HA AIRBUS A321271N During INSP/MAINT - 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. 2019-07-09
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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 .WITHNO FAULTS NOTED. RAN # 1 ENG AND NO MESSAGES. NO LEAKS NOTED. OK FOR SVC 2019-07-08
N214HA AIRBUS A321271N During INSP/MAINT - 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. 2019-07-02
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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. 2019-06-28
N214HA AIRBUS A321271N During TAXI/GRND HDL - 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 THENR 1 AND 2 ENGINES, NO FAULTS. 2019-06-28
N214HA AIRBUS A321271N During TAXI/GRND HDL - NR 1 ENGINE OIL CHIP DETECTED DURING ENGINE START, SHUTDOWN THE ENGINE. PERFORMED TSM 79-35-00-810-808-A, EXAMINED THEW03 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 OFODM 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 REM 2019-01-03
N214HA AIRBUS A321271N During TAXI/GRND HDL - NR 2 ENGINE OIL CHIP DETECTOR ACTIVATED. FOUND AFT CARBON SEAL BAD. REMOVE AND REPLACED THE NR 2 ENGINE. 2019-01-03
N214HA AIRBUS A321271N During CLIMB - 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. 2018-10-11

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