# N596HA: 1986 Boeing 767-332, registration cancelled 2014-03-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 11, 2014
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-332](https://openairdocs.org/model/boeing-767-332) (registry code 1385101)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 23276
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 9, 1986
- Certificate issued: April 4, 2006
- Last registry action: November 26, 2013
- Mode S code: A7B461
- Owner when cancelled: [Hawaiian Airlines Inc](https://openairdocs.org/faa-owner/HAWAIIAN%20AIRLINES%20INC)
- Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu)
- Owner type: Corporation
- Owner's area on the map: 21.3477° N, 157.8767° W: Placed by OpenAirDocs at the center of ZIP code 96819, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N596HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=596HA
- Page: https://openairdocs.org/deregistered/N596HA-2014-03-11

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 767-332: https://openairdocs.org/model/boeing-767-332.md

## Service difficulty reports (251, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR HALA201312250181](https://openairdocs.org/sdr/HALA201312250181), Dec 25, 2013: CONNECTOR. FAILED. FUEL QTY INDICATION STATUS MESSAGE CENTER TANK FUEL & TOTALIZER ON OVERHEAD ARE BLANK. R & R FQIS PROCESSOR IAW AMM 28-41-08 CONDITION SAME. FQIS BITE FAULT COD
- [SDR HALA2013111100167](https://openairdocs.org/sdr/HALA2013111100167), Nov 11, 2013: PUMP. FAILED. LEFT HYD PRIMARY OVERHEAT EICAS MESSAGE. IAW MOC INSTRUCTION/TSI T/S FIM 29-11, FT821. R & R ENG DRIVEN HYD PUMP IAW AMM 29-11-05. RAN LT ENGINE. LT EDP PRESSUR
- [SDR HALA2013092600122](https://openairdocs.org/sdr/HALA2013092600122), Sep 26, 2013: CIRCUIT CARD. FAILED. WARN ELEX ADVISORY DISPLAYED IN FLIGHT ALONG WITH AMBER SPLIM ON F/O ADI SPEED TAPE WITH LOSS OF RED SPEED TAPE INDICATOR BAR. REPLACED RT WARNING ELEX STALL WA
- [SDR HALA2013072400094](https://openairdocs.org/sdr/HALA2013072400094), Jul 24, 2013: TRANSFORMER. INOPERATIVE. ACFT DIVERTED TO AN ALTERNATE STATION. T/E FLAP DISAGREE EICAS AND CVE LIGHTS ILLUMINATED WHEN FLAPS SELECTED TO 15 DEGREES. AND STATUS T/E FLAP SHUTDOWN. ACCOM
- [SDR HALA2013071500089](https://openairdocs.org/sdr/HALA2013071500089), Jul 15, 2013: CONNECTOR. DIRTY. ON RIGHT ENG START EGT FLUCTUATING DID NOT INCREASE. CLEANED CONNECTOR ON RT ENG. OPS NORMAL, OK FOR SERVICE.
- [SDR HALA2013071200087](https://openairdocs.org/sdr/HALA2013071200087), Jul 12, 2013: CONNECTOR. DISCONNECTED. AFTER START RT ENGINE EGT FAILED (13DEG) (BTB). INSPECTED RT ENG THERMOCOUPLES, FOUND CONNECTOR DISCONNECTED ON THE FWD SIDE OF J-BOX. CONNECTED CONNECTOR, RAN 
- [SDR HALA2013061400081](https://openairdocs.org/sdr/HALA2013061400081), Jun 14, 2013: SKIN. DENTED. DENT FOUND FWD AND LOWER OF AFT CARGO COMPT. APPROX BS 1329, BETWEEN STRINGERS S36-37. NDT INSPECTION-NO CRACKS NOTED. PERFORMED INTERNAL VISUAL INSPECTION IAW 
- [SDR HALA2013061400080](https://openairdocs.org/sdr/HALA2013061400080), Jun 14, 2013: SKIN. DAMAGED. DENT FOUND FWD AND LOWER OF AFT CARGO COMPT APPROX BS 1280.5. BETWEEN STRINGERS S36-38. DENT 9"L X 12"W X .1875 DEPTH. GOUGE NOTED IN DENT .040 DEPT. NDT INSPEC
- [SDR HALA2013042700046](https://openairdocs.org/sdr/HALA2013042700046), Apr 27, 2013: J-BOX. FAILED. RT PRIMARY ENGINE EGT INDICATOR READS ZERO USING LDRR ICAS COMPUTER STANDBY ENGINE INSTRUMENT ALSO READS ZERO. TROUBLESHOT IAW FIM 77-21, FAULT TREE 803 INSPECT
- [SDR HALA2013041700039](https://openairdocs.org/sdr/HALA2013041700039), Apr 17, 2013: ENGINE. MAKING METAL. APU AUTO SHUTDOWN. LOW OIL PRESSURE FAULT ON ECU. DP POPPED ON OIL FILTER. METAL PARTICLES FOUND ON GEARBOX CHIP DETECTOR. REPLACED APU IAW M266, AUXILIARY POWE
- [SDR HALA2012121000233](https://openairdocs.org/sdr/HALA2012121000233), Dec 10, 2012: ENGINE. HUNG START. LEFT ENGINE HUNG START, N1 18.37. EGT 740. N2 56.47 F/F 1,200. REPLACED LT ENGINE MEC & LEAK CHECKED IAW AMM 73-21-01. REPLACED LT ENGINE T2 SENSOR IAW AMM 73-2
- [SDR HALA2012101000226](https://openairdocs.org/sdr/HALA2012101000226), Oct 10, 2012: SKIN. DAMAGED. LIGHTING STRIKE FOUND AT BS 148.2, 6.5" BELOW & -24L. DAMAGED AREA CUT OUT IAW SRM 53-00-01-2R-16, REPAIR 14D6347210, REV. 90. REPAIR PARTS FABRICATED IAW SRM 5
- [SDR HALA2012053000151](https://openairdocs.org/sdr/HALA2012053000151), May 30, 2012: CIRCUIT CARD. FAILED. ACFT ARRIVED SAFELY, NR 1 & 2 FIRE BOTTLES FOR RT ENGINE WERE DISCHARGED BY THE FLT CREW DURING APPROACH. WHILE LINING UP FOR APPROACH RECEIVED "FIRE WARNING" A
- [SDR HALA2012052900149](https://openairdocs.org/sdr/HALA2012052900149), May 29, 2012: WIRE HARNESS. MALFUNCTIONED. RIGHT ENGINE LP2 STATUS MESSAGE WAS INTERMITTENT. R & R WIRE HARNESS ON RESPONDERS IAW AMM 26-11-02/401 AND ACCOMPLISHED LEAK CHECK ON ALL DUCTING IAW AMM 36-11
- [SDR HALA2012052700148](https://openairdocs.org/sdr/HALA2012052700148), May 27, 2012: CHECK VALVE. MALFUNCTIONED. RT ENGINE FIRE LP 2 STATUS MESSAGE INTERMITTENT. FOUND & REPLACED INTERMEDIATE CHECK VALVE & DUCT ASSY. OPS & LEAK CHECKED GOOD IAW AMM 36-11-06. LEAK CK GOOD.
- [SDR HALA2012052700147](https://openairdocs.org/sdr/HALA2012052700147), May 27, 2012: WARNING LIGHT. NO INDICATION. LEFT PACK OFF LIGHT & LT PACK OFF EICAS MESSAGE NEVER ILLUMINATED WHEN PACK SELECTOR IN OFF POSITION. PERFORMED BITE CHECK ON LT PACK CONTROLLER NO FAULTS NOTED
- [SDR HALA2012052100143](https://openairdocs.org/sdr/HALA2012052100143), May 21, 2012: FIRE DETECTOR. FALSE ACTIVATION. RIGHT ENGINE FIRE LP2 EICAS ILLUMINATED. PERFORMED FIM 26-11-00/101, FIG 104, ENGINE FIRE DETECTION SYS BITE PROCEDURE RESECURED COUPLINGS AT HIGH STAGE BLEED M
- [SDR HALA2012051900141](https://openairdocs.org/sdr/HALA2012051900141), May 19, 2012: UNKNOWN. WARNING MESSAGE. RIGHT EEC EICAS ILLUMINATED, DID NOT RESET IAW QRA. TROUBLESHOOTING PERFORMED, ECC MONITOR BITE NO FAULTS NOTED. RESET EEC SWITCH RAN ENGINE FOR 10 MIN. NO FAUL
- [SDR HALA2012051900140](https://openairdocs.org/sdr/HALA2012051900140), May 19, 2012: TRANSCEIVER. NOT SEATED. A/S 192 KTS FLAP 20 DEGREE WHEN SPEEDBRAKES EXTENDED. RECEIVED RED CONFIG WARNING & GEAR NOT DOWN EICAS. RERACKED NR 1 RADIO ALT TRANSCEIVER, GROUND CHECKED OK.
- [SDR HALA2012051400139](https://openairdocs.org/sdr/HALA2012051400139), May 14, 2012: FIRE DETECTOR. MALFUNCTIONED. AFTER PARKING, STATUS MESSAGE DISPLAYED RT ENGINE FIRE LOOP. AFTER A FEW MINUTES THE STAUS MESSAGE EXTINGUISHED. INSPECTED RT ENGINE FIRE LOOP WIRE HARNESS IAW 
- [SDR HALA2012051400138](https://openairdocs.org/sdr/HALA2012051400138), May 14, 2012: WARNING MESSAGE. FALSE ACTIVATION. RECEIVED A STATUS MESSAGE "RT ENGINE FIRE LP 2". PERFORMED FIM 26-11-00/101 FIG 104. CHECKED RT ENG LP2 AND LP1 CONNECTIONS AND CLEANED. SECURITY/ATTACHMENT VER
- [SDR HALA2012051300137](https://openairdocs.org/sdr/HALA2012051300137), May 13, 2012: CIRCUIT CARD. MALFUNCTIONED. RIGHT ENGINE FIRE LOOP, STATUS MESSAGE ILLUMINATED ON DECENT. EXTINGUISHED AFTER LANDING. CHECKED RESISTANCE AT M684, PINS 19 & 20 - 1.5 K OHMS. CHECKED INSULAT
- [SDR HALA2012051000132](https://openairdocs.org/sdr/HALA2012051000132), May 10, 2012: ECU. FAULTED. PRIOR TO ENGINE START, APU FAULTED AND AUTO SHUTDOWN. BITE CHECKED APU ECU FOUND REVERSE FLOW FAULT. PERFORMED FIM 49-11-00-1 FIG 108. GROUND OPS CHECKED OK.
- [SDR HALA2012031800112](https://openairdocs.org/sdr/HALA2012031800112), Mar 18, 2012: COMPRESSOR. STALLED. NR 2 ENGINE COMPRESSOR STALL AT TOP OF CLIMB. FLT CREW DECLARED EMERGENCY AND DIVERTED BACK, WHERE AN UNEVENTFUL LANDING WAS MADE. OPEN.
- [SDR HALA2012030700107](https://openairdocs.org/sdr/HALA2012030700107), Mar 7, 2012: FIRE DETECTOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - ON COCKPIT PREFLIGHT FOUND NO AURAL WARNING WHEN WHEEL WELL AND ENG/APU/CARGO FIRE SYS TESTED. RE-SET MASTER WARNING CAUTION SWITCH, 
- [SDR HALA2012030500105](https://openairdocs.org/sdr/HALA2012030500105), Mar 5, 2012: CONNECTOR. LOOSE. ETOPS SIGNIFICANT SYS - F/O RADIO ALTIMETER IS INMT ON ADI. CONDITION NORM WITH ALTERNATE EFI SELECTED. PERFORMED BITE OF RT RADIO ALTIMETER. NO FAULTS INDICATE
- [SDR HALA2012022900093](https://openairdocs.org/sdr/HALA2012022900093), Feb 29, 2012: ENGINE. HUNG START. LEFT ENGINE HUNG START, FUEL FLOW AND DUCT PRESSURE WERE NORMAL. HUNG AT 56 PERCENT N2 AND EGT 710 DEGREES WHEN START ABORTED. SECOND START NORMAL. GROUND START
- [SDR HALA2012022700085](https://openairdocs.org/sdr/HALA2012022700085), Feb 27, 2012: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYS - ON INITIAL CLIMB EICAS MESSAGE, RT ENG HIGH STAGE, DISPLAYED RT HI STAGE LIGHT ILLUMINATED, QRH PROCEDURES C/W, LIGHT EXTINGUISHED. COND
- [SDR HALA2012022400073](https://openairdocs.org/sdr/HALA2012022400073), Feb 24, 2012: CONTROL SYSTEM. MALFUNCTIONED. FLAP /SLAT, ELEVATOR EICAS MESSAGE, UNABLE TO LOWER FLAPS. PERFORMED FSEU, FSPM BITE, NO FAULTS NOTED. CYCLED POWER FROM ENGINE TO APU, FLAP/SLAT ELEVATOR EICAS
- [SDR HALA2012011800043](https://openairdocs.org/sdr/HALA2012011800043), Jan 18, 2012: IRS. SPLIT. ETOPS SIGNIFICANT SYS- FMC MESSAGE SPLIT IRS OPERATION LT IRS 034/0.5, CENTER IRS. RT IRS 350/0.6. REMOVED POWER FROM ACFT RE-ESTABLISHED POWER AND ALIGNED TRU'
- [SDR HALA2011122100604](https://openairdocs.org/sdr/HALA2011122100604), Dec 21, 2011: CONTROL UNIT. OUT OF RIG. CALLED FOR FLAPS 20 AT APPROX 8-10' OF FLAP GOT FLAP DISAGREE, T/E LIGHT AND T/E FLAP SHUTDOWN. STATUS MESSAGE. FOLLOWED QRH AND EXTENDED FLAPS TO 20' WITH ALTE
- [SDR HALA2011120700577](https://openairdocs.org/sdr/HALA2011120700577), Dec 7, 2011: RELAY. FAILED. EICAS MESSAGE T/E FLAP DISAGREE DISPLAYED, T/E LIGHT ILLUMINATED WHEN ANY T/E FLAP POSITION WAS SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. DECLARED AN
- [SDR HALA2011120400565](https://openairdocs.org/sdr/HALA2011120400565), Dec 4, 2011: WARNING MESSAGE. MULTIPLE FAIL. FLAP ASSY MESSAGE ON GROUND. ON GEAR RETRACTION, RECEIVED A GEAR UN-SAFE LIGHT. OPEN.
- [SDR HALA2011112800544](https://openairdocs.org/sdr/HALA2011112800544), Nov 28, 2011: CONTROL UNIT. MALFUNCTIONED. FLAPS WOULD NOT EXTEND BEYOND 15DEG ACCOMPANIED BY T/E FLAP ASSYMETRY ANNOUNCIATION. USED ALTERNATE FLAPS TO EXTEND TO 30 DEG, NORMAL LANDING. ACFT ARRIVED WITH
- [SDR HALA2011114000518](https://openairdocs.org/sdr/HALA2011114000518), Nov 14, 2011: BULB. MISSING. ON OVERNIGHT CHECK, FOUND SEAT 1H FWD AISLE EMERGENCY LIGHT MISSING LENS & BULBS AND SEAT 2H BOTH AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED LENS AND BULBS. O
- [SDR HALA2011114000517](https://openairdocs.org/sdr/HALA2011114000517), Nov 14, 2011: BLADE. DAMAGED. ETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLA
- [SDR HALA2011111100516](https://openairdocs.org/sdr/HALA2011111100516), Nov 11, 2011: BLADE. DAMAGED. ETOPS SIGNIFICANT SYS - FOUND .2500 X .2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 7
- [SDR HALA2011111000511](https://openairdocs.org/sdr/HALA2011111000511), Nov 10, 2011: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH, SELECTED FLAPS 15 DEGREE, GOT EICAS FLAP DISAGREE MSG HANDLE IN DETENT AND FLAP GAUGE SHOWED APPROX 10 DEGREE. FOLLOWED PROCEDURE AND LANDED WITHOU
- [SDR HALA2011102800497](https://openairdocs.org/sdr/HALA2011102800497), Oct 28, 2011: FMC. UNKNOWN. ETOPS SIGNIFICANT SYS - FMC BOTH WHILE IN ATC MODE ON ATC INDEX PAGE PRINTING IS ILLUMINATED ON ATC LOG PAGE. ALL INFO UPLINK WILL NOT PRINT, L6 INDICATES PRINT
- [SDR HALA2011102400486](https://openairdocs.org/sdr/HALA2011102400486), Oct 24, 2011: OIL SYSTEM. LOW. ETOPS SIGNIFICANT SYS - AT GATE APU AUTO SHUTDOWN. BITE CHECKED ECU FOUND LOW OIL PRESSURE FAULT, SERVICED APU WITH 2.5 QTS, RAN APU NO LEAKS NOTED, OK FOR SVC.
- [SDR HALA2011101400461](https://openairdocs.org/sdr/HALA2011101400461), Oct 14, 2011: ENGINE. HUNG START. ETOPS SIGNIFICANT SYS - LT ENGINE HUNG START AT EGT 739 DEG; N2 53 PERCENT; FUEL FLOW 1500; OAT 14DEG C. ABORTED START, RESTARTED SUCCESSFUL. ACCOMPLISHED LT EN
- [SDR HALA2011091500403](https://openairdocs.org/sdr/HALA2011091500403), Sep 15, 2011: INDICATOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - ATTITUDE INDICATION OF STANDBY ALTITUDE INDICATOR IS ABNORMAL IN PITCH & ROLL. GYRO FLAG RETRACTED. REPLACED STANDBY ATTITUDE INDICATOR 
- [SDR HALA2011081600368](https://openairdocs.org/sdr/HALA2011081600368), Aug 16, 2011: CIRCUIT CARD. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - C DEMAND PUMP EICAS "ON" WITH CTR AIR DEMAND PUMP "PRESS" LIGHT "ON" INTERMITTENTLY FROM INITIAL DESCENT TO LANDING. T/S IAW FIM 29-11-0
- [SDR HALA2011072300335](https://openairdocs.org/sdr/HALA2011072300335), Jul 23, 2011: TOTALIZER. INACCURATE. ETOPS SIGNIFICANT SYS - CALC & TOTALIZER HAS A 2,300 LB DIFF IAW FIM 28-41-00, FIG 107 TOTAL FUEL & FMC CAL FUEL CHECKED OK.
- [SDR HALA2011070600315](https://openairdocs.org/sdr/HALA2011070600315), Jul 6, 2011: PROCESSING UNIT. FAULTED. ETOPS SIGNIFICANT SYS - INTERMITTENT FUEL QTY BITE EICAS MESSAGE. BITE CHECKED FUEL QTY PROCESSOR UNIT. FOUND "D2" FAULT. PERFORMED RESET VERIFY CONFIRMED NO FA
- [SDR HALA2011070200303](https://openairdocs.org/sdr/HALA2011070200303), Jul 2, 2011: OVERHEAT LOOP. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - STATUS EICAS WARNING ON DESCENT. "R ENG OH LP 2". REPLACED DAMAGED RT ENGINE OVERHEAT LOOP DETECTOR AND OPS CHECK OK IAW MM 26-11-02.
- [SDR HALA2011062500291](https://openairdocs.org/sdr/HALA2011062500291), Jun 25, 2011: CIRCUIT CARD. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - EICAS STATUS MSG: RT ENG OH LP2 DISPLAYED. ACCOMPLISHED FIM DAL D633T605 AND WDM 26-11-22. REPLACED RT ENG LP2 OVERHEAT DETECTION CARD (
- [SDR HALA2011061800269](https://openairdocs.org/sdr/HALA2011061800269), Jun 18, 2011: COMPUTER. UNKNOWN. TCAS COMPUTER FAILURE NR 1 & NR 2 TRANSPONDER DATA BUSS FAILURE. 1 & 2 PROCESSER FAILURE RA DISPLAY NR2 RADIO ALT NR1. RECYCLED TCAS C/B. GROUND CHECK OK.
- [SDR HALA2011051700207](https://openairdocs.org/sdr/HALA2011051700207), May 17, 2011: LINE. LOOSE. ETOPS SIGNIFICANT SYS - ON DESCENT WITH POWER IDLE LEFT ENGINE BLEED VALVE LIGHT ON. TROUBLESHOT IAW FIM 36-10-00, FIG 111. FOUND & SECURED LOOSE SENSE LINE AT 
- [SDR HALA2011041900163](https://openairdocs.org/sdr/HALA2011041900163), Apr 19, 2011: A/C PACK. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - RT PACK INOP LIGHT ILLUM, EICAS MESSAGE RT PACK TEMP DISPLAYED NORMAL AFT STBY SELECTED. T/S IAW FIM 21-51-00/101, FIG 103. DID PACK TEM

All 251: https://openairdocs.org/deregistered/N596HA-2014-03-11/reports.md

## Other aircraft with N596HA

- [Cancelled 1988-08-12](https://openairdocs.org/deregistered/N596HA-1988-08-12): Beech B-99, S/N U160. Triennial form not returned

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