N216HA
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 | 2023-10-27 – 2023-10-27 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WHILE PER TASK CARD I321-7DAY-CHECK. FOUND 11WL & 13WL EPSU BATTERY FAULT. GROUNDED - YES. REMOVED AND REPLACED 11WL AND 13WL EPSU BATTERY IAW AMM 33-51-38. OPS GOOD. OK FOR SERVICE.
ETOPS - Y ENG 2 PUMP INOP. REMOVED AND REPLACED NR 2 ENG. DRIVEN HYD. PUMP CONDITION SAME. ACCOMP. TEST OF PTU W/ENG. PUMPS PER AMM 29-23-00-710-004-A. ALL ENG.DRIVEN HYD PUMPS,ELECT HYD. PUMPS & PTU OPS NORMAL OK FOR SERVICE. SECURED NR 2 ENG.COWLINGS. P/N OFF/ON:3031863-002 S/N OFF:MX805985 S/N ON:MX831662
ETOPS - IN FLIGHT, ENG 1 FIRE LOOP B FAULT. REMOVED AND REPLACED #1 ENG PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16. OPS CHECK GOOD. OK FOR SERVICE.
ETOPS - ENG2 OIL SENSOR FAULT MESSAGE FLASHED SPORADICALLY DURING CRUISE. REPLACED PHMU PER AMM 77-31-01 ON RH ENGINE. PERFORMED IDLE AND OPS CHECK. OPS CHECK GOOD. OK TO CONTINUE.
ETOPS - DURING ENGINE HARNESS REPLACEMENT FOUND HPC BLEED VALVE SOLENOID LINE DAMAGED. REMOVED 7 REPLACED HPC BVS LINE PER AMM 75-32-02-400-801A. LEAK CK GOOD. OK FOR SVC.
ETOPS - DURING FOM FOUND WIRE DAMAGE ON #2 ENG N2 SENSOR O/B 4065KS-J64. FOUND WIRE BUNDLE DAMAGE ON #2 ENG BY TACC (FLAGGED) 4055KS-J31. REMOVED & REPLACED WIRE HARNESS W03 ON ENG #2 PER AMM 73-21-63. EEC OPS CK GOOD. OK FOR SVC
EMERGENCY DECLARED. LOW OIL ENG #1 0.0 DECREASING FROM 18.0. AT SHUTDOWN ENG 1 QT 3.5. PILOT NOTED DURING EVENT OIL PSI 152 AND NO INFLIGHT SHUT DOWN PERFORMED. FOUND ENG STARTER LEAKING. REMOVED AND REPLACED PER AMM 80-11-01. LEAK AND OPS CHECK GOOD. ENGINE OIL SERVICED. OK FOR SVC
ATB - AIR ENG BLEED 2 FAULT ECAM DURING CLIMBOUT @ MCT POWER PER WONT CLIMB PROC. UNABLE TTO RESET W/ ECAM OVERHEAT NOTED. T/S REMOVED & REPLACED #2 ENGINE FAN AIR VALVE IAW AMM 36-11-54-400-803-A.
ETOPS-CAPTAIN'S MCDU 3L BUTTON WORKS ONLY INTERMITTENTLY. REMOVED AND REPLACED CAPT'S MCDU PER AMM 22-82-12. OPS CHECK GOOD, OK TO CONT. SERVICE.
ETOPS - INFO TO MX ON DEPARTURE CLIMB ENG 2 AMBER CLOG ANNUNCIATOR ILLUMINATED ON ENG SD PAGE. MESSAGE CLEARED AFTER A FEW MINS. PERFORMED TSM 73-11-00-810-822-A. REMOVED AND REPLAACED FUEL FILTER. FADEC SYSTEM IDLE TEST OK. NO LEAKS NOTED. OK FOR SVC.
LAV SMOKE ECAM IN FLIGHT. ECAM CLEARED ITSELF AFTER 3 SECONDS, FA'S INVESTIGATED AND FOUND NO SOURCE OF FIRE. SUSPECT PAX VAPING. PERFORMED TSM 36-17-00-810-804-A NO DETECTORS FAULTING. NO FAULTS ON POST FLIGHT REPORT CLEANED DUST FROM ALL 4 LAVS. OK FOR SERVICE.
ETOPS - BTB. HYD G ENG 1 PUMP LO PR INDICATION 8X ON TAXI OUT. HYD PAGE PUMP LOW PRESSURE PTU OPERATING SHOWING AMBER AND GREEN INDICATIONS ENG 1 PUMP FAULT LIGHT ON OFF THROUGH INDICATIONS. REMOVED AND REPLACED PRESSURE SWITCH PART #450-1-3100-00 AND ELECTRICAL CONNECTOR P/N EN299E61203BN ON ENG#1 GREEN HYD SYS IAW AMM 29-11-17-400-802. PERFORMED ENGINE RUN ON #1 ENGINE, IDLE TO 25-30% NO FAULTS NOTED G HYDRAULIC PUMP INDICATES PRESSURE NORMAL RAN ENGINE FOR 20 MINS OPS CHECK GOOD.
4R DOOR DISARMED DURING FLIGHT. WOULD NOT REARM. PERFORMED PRESSURIZATION CHECK WITH 4R DOOR ARMED. FOUND ARM/DISARM LEVER NOT FLUSH. FOUND SLIDE LOCK/LATCH BLOCKED WITH DEBRIS. RMEOVED DEBRIS. OPS CHECK OK. OK FOR SVC.
ETOPS-ECAM HYD G ENG 1 PUMP LO PR TURNED OFF ENG 1 PUMP AS INSTRUCTED BY ECAM. PERFORMED TSM 29-11-00-810-804-A, FOUND PRESSURE SWITCH LOOSE. REMOVED AND REPLACED ENG 1 PUMP PRESSURE SWITCH (1047GK) PER AMM 29-11-17. OPS CHECK AND LEAK CHECK GOOD, NO FAULT NOTED. OK FOR SVC.
ETOPS - DURING WALK AROUND, FOUND OIL SEEPING FROM EN1 S/N: P770687 INLET CONE. UPON INSPECTION, FOUND OIL INSIDE INLET CONE. REMOVED & REPLACED FAN SHAFT COVER SEAL PER AMM 72-15-00-960-801-A. NO LEAKS NOTED POST IDLE RUN. OK FOR SERVICE.
ETOPS-FORWARD TRIM AIR VALVE NOT RESPONDING APPROPIATELY TO SWITCH POSITION. TEMP IN CABIN HOT WITH FULL COLD SET. PREVIOUSLY WRITTEN UP, NO CHANGE. REMOVED AND REPLACED TEMPERATURE SELECTOR PER AMM 21-63-11-000-001-A (21315 3/8/24. PENDING OPS CHECK. PERFORMED OPS CHECK OF CAB TEMP CONTROL PER AMM 21-63-00-710-004-A, TEST OK. OK FOR SVC
AFT EXIT SIGN BURNT OUT AIRCRAFT LEFT SIDE. CLEANED AFT EXIT SIGN CONNECTORS. OPS CHECKED PER AMM 33-51-00 CHECK GOOD OK FOR SERVICE.
ETOPS - ENG #2 HYDRAULIC DRIPPING, 1 DRIP PER SECOND. REMOVED AND REPLACED ENG#2 HYD PUMP IAW AMM 29-13-51-000-806-A. ACCOMPLISHED ENG #2 IDLE RUN, NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.
ETOPS - INFO TO MTX: ON CLIMB OUT MOMENTARY ECAM OF: ENG 1 FIRE LOOP A FAULT. CLEARED ITSELF UP AS WE BEGAN ECAM ACTIONS. INSTALLED NEW #1 ENG FIRE ELEC HARNESS ASSY. PER AMM TASK 26-12-61, OPS TEST OK.
INFO TO MX: DURING CRUISE BRIEF ECAM (2X) ENG.1 FIRE LOOP A FAULT. ECAMS CLEARED AFTER APPROX 3 SECS. NOTED BY MAINTENANCE. PERFORMED OPERATIONAL TEST OF THE ENG. FIRE AND OVERHEAT DETECTION TEST I.A.W. AMM 26-12-00-710-002-B. TEST O.K.
ATB - RIGHT WING FUEL AND TEMP INDICATIONS AMBER XX'S, FOB AMBER XX'S. ATTEMPTED QRH RESET WITH MX VIA SATCOM - UNSUCCESSFUL. REMOVED & REPLACED R WING TANK FUEL PROBES 30QT2 & 59QT2 PER AMM 28-42-15 R TANK INDICATION & FOB INDICATION & TEMP INDICATION SHOW NORMALLY.
ETOPS-ENG B FIRE LOOP ON ECAM. CHECKED RESISTANCE BETWEEN PINS J-K AT FDU 2 LOOP B. FOUND RESISTANCE FLUCTUATING FRANTICALLY OUT OF LIMITS WHILE TAPPING HARNESS 4166KS. REMOVED & REPLACED HARNESS 4166KS PER AMM 26-12-62. RESISTANCE STAYED SOLID AT 1.5K OHMS. ECAM MSG CLEARED OK FOR SERVICE.
ETOPS - ALL LAVATORIES NOT WORKING IN FLIGHT, HEADING BACK TO LAX. PERFORMED CIDS POWER UPTEST AND FAULTED 300RH8. REMOVED AND REPLACED DEU-B 300RH8 IAW AMM 23-73-47 PB 401, OPS CHECK OF ALL LAV AS OKAY. AC OK TO CONTINUE. ORIG SUB DATE: 1/3/2023
ETOPS-DURING PDC FOUND #2 ENG LEAKING FUEL AT HPC PRIMARY STATOR VANE ACTUATOR. REMOVED AND REPLACED #2 ENG HPC PRIMARY STATOR VANE PER AMM 75-31-02-400-801-A. MECH 16488 / 21800. PENDING IDLE RUN / LEAK CHECK. COMPLETED IDLE RUN & LEAK CHECK PER AMM 71-00-00-720-811. NO LEAKS NOTED. A/C OK FOR SVC.
ETOPS - APU AUTOSHUTDOWN - TRIED A SECOND TIME WITH ANOTHER AUTOSHUTDOWN. REMOVED AND REPLACED IGNITER AS PER AMM 49-41-41-400-0041-A, ALSO REMOVED AND REPLACED EXITER BOX AS PER AMM 49-41-38-400-003-A, PERFORMED OPS CHECK NORMAL. APU VERIFICATION FLIGHT FOR N216HA (FLT#79) COMPLETED "SATISFACTORILY." INFLIGHT START ON 1ST ATTEMPT @ FL340 (-46)
AIR ENG 1 HP VALVE FAULT. REPLACED PACK INLET PRESS SENSOR (LH) FIN (23HB1) PER AMM 21-51-13. LEAK CHECK OK. OPS PENDING 10-19-22 16801... REMOVED AND REPLACED #1 ENG HPV PER AMM 36-11-51. OPS AND LEAK CHECK PENDING 7880 10/18/22.. CONT ON LOG #895086 ITEM 1. HP VALVE OPS AND LEAK CHECK OK PER AMM 36-11-51. LH PACK INLET PRESS SENSOR OPS AND LEAK CHECK OK PER AMM 21-51-13. PERFORMED HIGH POWER RUN ON BOTH ENGINES, ALL PARAMETERS NORMAL. NO FAULTS NOTED. A/C OK FOR SVC.
ETOPS - ENG 2 FIRE LOOP B FAULT DURING CLIMB @ 16000' PRIOR TO ETOPS ENTRY // REMOVED & REPLACED ENG 2 FIRE LOOP B AGB PER AMM 26-12-17. OPS TEST OF ENG FIRE & OVERHEAT DETECTION GOOD PER AMM 26-12-00. OK FOR SERVICE.
ON APPROACH STRONG SOCK SMELL LEVELING OFF @ 4000 IN COCKPIT AND FWD CABIN. PERSISTING THROUGH ENG SHUTDOWN // PERFORMED #1 & #2 ENG IDLE RUN PER AMM 71-00-00-860-823-A.OPERATIONAL CHECK OF #1 & #2 PACK PER AMM 21-51-00-710-002-A. NO SMELL NOTED. OK FOR SVC.
INFO TO MX ON DESCENT PASSING 5000' FAINT WET SOCK SMELL THROUGH AIR GASPRES. WENT AWAY AFTER A FEW MIN. FOUND ENG 1 OVER SERVICED BY APPROX 3 QTS. REMOVED EXCESS OIL FROM TANK. OPERATED ENG @ IDLE FOR FOR APPROX 5 MIN. NO SMELL. OK FOR SVC.
ETOPS - APU SHUTDOWN PRIOR TO A/C REPOSITIONING // PERFORMED TSM 49-00-81-810-825-A NEED TO REPLACE IGNITION EXCITER PER PARAGRAGH 4A2A REMOVED AND REPLACED IGNITION EXCITER PER AMM 49-41-38. ALL CHECKS GOOD.
IMMEDIATELY AFTER ENGINE START (LIGHT) AND AFTER INITIATING DESCENT (STRONG) DIRTY SOCK SMELL IN COCKPIT. PERFORMED TROUBLESHOOTING OF ENGINES AFTER SMOKE/OIL FUMES IN THE CABIN PER TSM 71-00-00-810-847-A. RAN BOTH ENGINES 1&2 AND OPERATED ALL PAX SYSTEMS. NO ODORS DETECTED. LEAK CHECK GOOD. OK TO CONTINUE
EMER EQ - EPSU BATTERIES 11WL AND 13WL FAULTING // REMOVED AND REPLACED EPSU BATTERIES AT 11WL AND 13WL PER AMM 33-51-38-400-002-A. OK FOR SVC.
ETOPS SIGNIFICANT SYSTEM - ENG 2 IGN B ECAM WENT THRU THE ALT START PROCEDURES. THE ECAM WENT AWAY (STATUS) AFTER ENGINE SHUTDOWN AT DESTINATION. PERFORMED OPS TEST OF THE ENG 2 IGN A+B PER AMM 74-00-00-710-802-A, OPS NORMAL. NO CURRENT FAULT DISPLAYED, OK FOR SVC.
ATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWAP TO ORIGINAL. AMM 27-93-34. FLT CTL PITCH FAULT + FCDC 1 REMAINS (ELAC 1 OR WIRING FROM R ELEV POS MON XDCR). ELAC 1 (2CE1) CONNECTOR AE TO ELEV POS R XDCR UNIT (49CE2) CONNECTOR B WIRING CK OK, 2E-G, 2F-H, 2G-D, 2H-E. ALSO SEC 1 (1CE1) CONNECTOR AD TO ELEV POS R XDCR UNIT (49CE2) CONNECTOR B WIRING CK OK, 14G-G, 14H-H, 14J-D, 14K-E. ALL WIRES CONTINUITY CK GOOD, NO SHORT TO GND PER WDM 27-93-31. DURING CHECKING TRANSDUCER RESISTANCE CK, FOUND PIN D AND E PUSHED BACK ON CONNECTOR B. REMOVED & REPLACED SYS PRESSURE SWITCH(2151GN) PER TSM 27-933-00-810-947A & PRESSURE TRANSDUCER(2065GN) AMM 29-32-11, CONDITION SAME. REMOVED & REPLACED RH ELEVATOR POSITION TRANSDUCER UNIT PER TSM 27-9-00-810-872A & AMM 27-92-13. DUE TO 2 PINS PUSHED IN ON TRANSDUCER OPS CHECK OF TRANSDUCER GOOD. REMOVED AND REPLACED 1837VT TERMINAL BLOCK PER ESPM 20-44-51. PERFORMED OPS TEST OF ELAC 1 + SEC 1 PER AMM 27-93-00-710-001-A + AMM 27-94-00-710-002-A, OK FOR SVC. AIRCRAFT RETURNED TO DEPARTED STATION, WHERE A UNEVENTFUL LANDING WAS MADE.
ETOPS SIGNIFICANT SYSTEM - CAPTAIN'S SIDE ND FLICKERS BETWEEN WX + TERRAIN WHEN TERRAIN SELECTED. // DURING T/S FOUND FLICKERING ONLY OCCURS WHILE WXR 2 IS ON. REMOVED AND REPLACED #2 WXR TRANSCEIVER IAW AMM 34-41-33 PB 401 CONF 01 OPS TEST GOOD, FLICKERING BETWEEN WX AND TERR HAS STOPPED.
ETOPS SIGNIFICANT SYSTEM - WX + T + H AND TERR FLASH CONTINUOUSLY WHEN TERR ON ND IS SELECTED ON CA'S SIDE ND.// FOUND DEFECT ASSOCIATED WITH #2 RADAR SYS. RE-RACKED #2 WEATHER RADAR TRANSCEIVER "15Q2" DEFECT CLEARED. OPS CHECK GOOD. OK TO SERVICE
ETOPS SIGNIFICANT SYSTEM - DURING BOROSCOPE INSPECTION OF #1 ENG FOUND AFT #3 BRG DRY FACE CARBON SEAL MISSING.// REPLACED #1 ENGINE PER TASK CARD J321-72-HWI -02. ALL REQUIRED TESTS CHECK OK. OK FOR SERVICE. ENGINE: IAE, PW1133G-JM.
ATB AT 8,000 ECAM, AIR FAULT PACK 2. REMOVED AND REPLACED PACK FLOW CONTROL VALVE PER AMM 21-51-51-400-001-A AND PERFORMED OPS TEST OF FLOW CONTROL AND INDICATING SYSTEM PER AMM 21-51-00-710-002-A. OPS CHECK GOOD OK FOR SERVICE.
ATB - AFT CARGO DOOR OPEN IN FLIGHT. INSPECTED DOOR, VERIFIED AFT CARGO DOOR CLOSED AND LOCKED PER AMM 52-70-00. PRESSURE CHECK OF AFT CARGO DOOR OK PER AMM 05-53-00-780-001-A. PERFORMED OVERWEIGHT LANDING INSPECTION PER AMM 05-51-11-200-004-B. NO DAMAGE NOTED.
ETOPS SIGNIFICANT SYSTEM - ENGINE 1 OIL FILTER DEGRADE. (OIL FILTER DEGRADE CAUTION ON ECAM. REMOVED & REPLACED NR 1 OIL FILTER & NR 1 OIL FILTER DIFFERENTIAL PRESS SENSOR. ENG NR 1 OIL FILTER DEGRADE MESSAGE DID NOT RETURN. A/C IS OK FOR CONTINUE SERVICE.
OPEN - ATB - AFT CARGO OPEN WARNING IN CLIMB OUT 2500FT. ECAM DOOR PAGE INDICATIONS CARGO DOOR, (INDICATIONS MAY BE INOPERATIVE PROVIDED A VISUAL CHECK IS MADE BEFORE EACH DEPARTURE TO CONFIRM THAT DOORS ARE CLOSED AND LOCKED). SUP - ATB - PERFORMED ALTERNATIVE TEST OF PROXIMITY SWITCH PER AMM 52-35-00 TEST GOOD AMM 52-35-00 TEST GOOD PRESSURIZED TO 4.5 PSI DEFERENTIAL NO ECAM WARNING NOTED MIC SHEET CLEARED PLACARD REMOVED.
AIRCRAFT DEPARTED RIC. EN ROUTE, CREW NOTED BURNED ODOR AND THE NAV UNIT EMITTED SMOKE (A WHISP). CREW PULLED THE CIRCUIT BREAKER OF THE AFFECTED UNIT AND RETURNED TO RIC.
NAVIGATION RECEIVER CONVERTER FAILED CAUSING UNIT TO EMIT A BURNED ODOR IN THE AIRCRAFT COCKPIT AND UNIT DID SMOKE AT FAILURE. CREW PULLED THE CIRCUIT BREAKER AND RETURNED. NO PASSENGERS ON BOARD.