# N597HA: 1986 Boeing 767-332, registration cancelled 2014-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 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: 23277
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 4, 1986
- Certificate issued: April 6, 2006
- Last registry action: November 26, 2013
- Mode S code: A7B818
- 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/N597HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=597HA
- Page: https://openairdocs.org/deregistered/N597HA-2014-07-30

From the FAA registry file of November 3, 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 (233, newest 50)

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

- [SDR HALA2014061200082](https://openairdocs.org/sdr/HALA2014061200082), Jun 12, 2014: WARNING LIGHT. FALSE ACTIVATION. C HYD DEM PUMP LIGHT CAME ON DURING DECENT, OVERHEAD LIGHT A EICAS LIGHT. PERFORMED CHECKLIST NO CHANGED SWITCH OFF. PERFORMED OPS TEST OF CTR HYD SYS IAW AMM 2
- [SDR HALA2014060500078](https://openairdocs.org/sdr/HALA2014060500078), Jun 5, 2014: OVERHEAT SENSOR. MALFUNCTIONED. STATUS MESSAGE DISPLAYED: LEFT ENGINE OVERHEAT LP2. REPLACED LT ENGINE OVERHEAT LP2 DETECTION. GROUND OPS CHECKED OK IAW CMM 26-11-02.
- [SDR HALA2014050900063](https://openairdocs.org/sdr/HALA2014050900063), May 9, 2014: OIL SYSTEM. LEAKING. DUE TO DECREASING OIL QTY ON NR 1 ENGINE. REPLACED NR 1 ENGINE.
- [SDR HALA2014043000057](https://openairdocs.org/sdr/HALA2014043000057), Apr 30, 2014: WARNING MESSAGE. FALSE ACTIVATION. APU ISOLATION VALVE STATUS MESSAGE DISPLAYED. RESET MESSAGE & CLEARED GROUND, OPS CHECK NORMAL. OK FOR SERVICE, FIM 28-25, FIG 104.
- [SDR HALA2014042200053](https://openairdocs.org/sdr/HALA2014042200053), Apr 22, 2014: AUTOPILOT SYS. MALFUNCTIONED. LOSS OF LEFT FLT DIRECTOR AUTO PILOT DISCONNECT, SELECTED "R", OPS NORMAL. ACCOMPLISHED MCDP GROUND TEST 40 IAW FIM 22-02-00. NO FAULT NOTED ON TEST. CAPTAIN'S 
- [SDR HALA2014041800047](https://openairdocs.org/sdr/HALA2014041800047), Apr 18, 2014: DUCT. CRACKED. RT BLEED DUCT LEAK EICAS MESSAGE SURING CLIMB, CRUISE, AND TOUCHDOWN WAS AVERAGE. AIR TURN BACK, LANDED AT 287,000 LBS. REMOVED CRACKED DUCT BODY CROSSOVER RT S
- [SDR HALA2014041700048](https://openairdocs.org/sdr/HALA2014041700048), Apr 17, 2014: WARNING MESSAGE. FALSE ACTIVATION. RT BLEED DUCT LEAK EICAS MESSAGE AND DUCT LEAK RT SIDE ON OVERHEAD PANEL ILLUMINATED. FOLLOWED QRH THEN MAINTENANCE ADVISED TO TURN ON RT ENG BLEED AIR DUCT LEA
- [SDR HALA2013110100162](https://openairdocs.org/sdr/HALA2013110100162), Nov 1, 2013: ENGINE. BIRD INGESTION. NR 2 ENGINE BIRD INGESTION PLUS RT WING MAIN FLAP, INBD T/E FLAP, BIRD STRIKE DAMAGE. INSTALLED NR 2 ENG IAW M1139-767. OPS AND LEAK CHECK GOOD.
- [SDR HALA2014012200014](https://openairdocs.org/sdr/HALA2014012200014), Dec 19, 2012: LAMP. INOPERATIVE. FWD ENTRY DOOR LIGHT IS OUT. REPLACED LAMP , OPS CHECKED NORMAL.
- [SDR HALA2012121500235](https://openairdocs.org/sdr/HALA2012121500235), Dec 15, 2012: ECU. FAILED. APU INFLIGHT START WAS NOT SUCCESSFUL. MAX EGT RECEIVED WAS 812' AND MAX RPM REACHED WAS 53 PERCENT. RPM ACCELERATION SEEMED VERY SLOW. APU FAULT ANNUNCIATED. R
- [SDR HALA2012112100228](https://openairdocs.org/sdr/HALA2012112100228), Nov 21, 2012: PITOT HEAD. FAILED. AFTER ENGINE START CAPTAIN`S PITOT HEAT EICAS MESSAGE. FOUND CAPTAIN'S PITOT TUBE OPEN, REPLACED PITOT STATIC PROBE IAW 34-11-01 NOW TESTS NORMAL ALL TAPE AND T
- [SDR HALA2012091700209](https://openairdocs.org/sdr/HALA2012091700209), Sep 17, 2012: CIRCUIT CARD. MALFUNCTIONED. ON GROUND TAXI WITH BOTH ENGINES ON LT ENGINE N1 23, RT ENG N1 36.6 ALSO RT ENGINE EGT IS LOWER THAN LT. IAW AMM 73-32-06 FLIGHT GROUND IDLE SOLENOID CHECK NR 2
- [SDR HALA2012070800168](https://openairdocs.org/sdr/HALA2012070800168), Jul 8, 2012: GROUND WIRE. BROKEN. ON CLIMB OUT, RECEIVED STATUS MSG ONLY " AFT EQ EXH FAN 2". TROUBLESHOT IAW FIM 21-26-00, FIG 104, SHEET 1. FOUND WIRES GD1338 AND GD1340 BROKEN AT GROUND TERMI
- [SDR HALA2012052700150](https://openairdocs.org/sdr/HALA2012052700150), May 27, 2012: PCA. MALFUNCTIONED. RUDDER RATIO EICAS MESSAGE SHORTLY AFTER DEPARTURE. MESSAGE STAYED ON ENTIRE FLT. RUDDER RATIO RT FAULTED PCA. RUDDER RATIO LT FAULTED PCA, ALSO RT MODULAR FAUL
- [SDR HALA2012030400096](https://openairdocs.org/sdr/HALA2012030400096), Mar 4, 2012: CONTROL PANEL. MALFUNCTIONED. FLT CREW LEFT EMERGENCY ESCAPE TEST DOES NOT ILLUMINATE IN TEST 1. R & R SQUIB TEST PANEL. OPS CHECKED OK IN TEST 1 AND TEST 2, IAW AMM 26-21-04. OK FOR SERVICE
- [SDR HALA2012022500074](https://openairdocs.org/sdr/HALA2012022500074), Feb 25, 2012: WARNING MESSAGE. FALSE ACTIVATION. MAIN BATTERY CHARGER EICAS MESSAGE. ACCOMPLISHED FIM 24-31-00-101-103, SYS CHECKED OK. NO FAULTS NOTED. OK TO CONTINUE.
- [SDR HALA2012022700086](https://openairdocs.org/sdr/HALA2012022700086), Feb 24, 2012: ATTACH BRACKET. CRACKED. LEFT PYLON INBD SIDE PYLON TO CORE COWL FAIRING ATTACH BRACKETS 3 EA CRACKED. BRACKETS LOCATED BETWEEN 1ST & 3RD CORE COWL HINGES. REMOVED 3 EA CRACKED BRACKETS
- [SDR HALA2012011900048](https://openairdocs.org/sdr/HALA2012011900048), Jan 19, 2012: SENSOR. DIRTY. ETOPS SIGNIFICANT SYS - UNABLE TO REGULATE MID CABIN TEMPERTURE WITH AUTO CONTROL. FLUCTUATED ENTIRELY HOT THEN SMALL ADJUSTMENT CAUSES IT TO SWING EXTREMELY CO
- [SDR HALA2012011600037](https://openairdocs.org/sdr/HALA2012011600037), Jan 16, 2012: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - FWD EQUIPMENT VALVE ON EICAS & OVERHEAD PANEL. TROUBLESHOT PER FIM 21-58-00 FIG 105 NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2012011600028](https://openairdocs.org/sdr/HALA2012011600028), Jan 16, 2012: EEC. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - AFTER ENGINE START, RIGHT EEC INOPERATIVE, LIGHT ILLUMINATED. RESET RT EEC. PERFORMED ENGINE RUN. ALL OPS CHECKED GOOD.
- [SDR HALA2012011500020](https://openairdocs.org/sdr/HALA2012011500020), Jan 15, 2012: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - FWD EQUIPMENT VALVE ON EICAS AND OVERHEAD PANEL. TROUBLESHOT IAW FIM 21-58-00, FIG 105. NO DEFECTS NOTED, OK FOR SERVICE.
- [SDR HALA2012011100019](https://openairdocs.org/sdr/HALA2012011100019), Jan 11, 2012: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - MX LEVEL EICAS MESSAGE FOR ENGINE EEC LATCHED. PERFORMED TROUBLESHOOTING IAW FIM 767-FIM HWI D633T6A8, FIG 104, SHEET 1, STEP 1 THUR 4. 
- [SDR HALA2011122900620](https://openairdocs.org/sdr/HALA2011122900620), Dec 29, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - BTB RT EEC EICAS. RT ENGINE EEC ON STARTUP. INFO NOTED. BITE EEC NO FAULTS NOTED. RAN ENGINES AT GATE, ALL OK IAW FIM 71 EEC MX MONITOR 
- [SDR HALA2011122400617](https://openairdocs.org/sdr/HALA2011122400617), Dec 24, 2011: SLEEVE. CRACKED. ETOPS SIGNIFICANT SYS - NR 1 ENGINE EXHAUST NOZZLE (SLEEVE) HAS NUMEROUS CRACKS A LONG LENGTH OF EXHAUST ABOUT 8 O'CLOCK POS. R & R NR1 ENG EXHAUST NOZZLE SLEEV
- [SDR HALA2011122100607](https://openairdocs.org/sdr/HALA2011122100607), Dec 21, 2011: GPS. INOPERATIVE. ETOPS SIGNIFICANT SYS - RT GPS INOPERATIVE WITH EICAS MESSAGE. PERFORMED ADJUSTMENT AND TEST IAW AMM 34-58-00/501. SYS CHECKED OK.
- [SDR HALA2011120700576](https://openairdocs.org/sdr/HALA2011120700576), Dec 7, 2011: CARTRIDGE. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - LT NACELLE FIRE TEST 1 WILL NOT TEST FOR CARTRIDGE SQUIB ON FIRE EXTINGUISHING SYS. DISCONNECTED ELECTRICAL CONNECTOR AND REMOVED CARTRI
- [SDR HALA2011120300563](https://openairdocs.org/sdr/HALA2011120300563), Dec 3, 2011: CONTROLLER. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - ATB - RT ENG BLEED LIGHT ON AT TOP OF CLIMB. COMPLIED WITH TSI IAW FIM 36-10-00 FIG 111 AND WD 36-11-62, WIRING BETWEEN BLEED CONTROL CA
- [SDR HALA2011112500545](https://openairdocs.org/sdr/HALA2011112500545), Nov 25, 2011: COUNTERBALANCE. BROKEN. L4 DOOR HARD TO CLOSE. FOUND COUNTERBALANCE BROKEN. R & R L4 DOOR COUNTERBALANCE ASSY IAW AMM 52-11-16. OPS CHECKED OK.
- [SDR HALA2011111800538](https://openairdocs.org/sdr/HALA2011111800538), Nov 18, 2011: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYS - ATB - EICAS MESSAGE RT ENGINE BLEED VALVE. T/S IAW FIM 36-11-00 FIG 111, CLEANED CONNECTOR TO HPC, RECONNECTED CONNECTOR AND UNLOCKED VA
- [SDR HALA2011112000515](https://openairdocs.org/sdr/HALA2011112000515), Nov 12, 2011: WARNING MESSAGE. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - APU ISOLATION VALVE STATUS MESSAGE. PERFORMED FIM 28-25-00/101, FIG 104, NO FAULTS NOTED, MESSAGE CLEARED OK FOR SERVICE.
- [SDR HALA2011110900508](https://openairdocs.org/sdr/HALA2011110900508), Nov 9, 2011: WARNING MESSAGE. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - RA DISPLAYED ON THE F/O ADI. RESET F/O RADIO ALTIMETER CIRCUIT BREAKER, BITE CHECKED OK, TEST 30 OK. LMP REMAINS IN LAND 3.
- [SDR HALA2011102500492](https://openairdocs.org/sdr/HALA2011102500492), Oct 25, 2011: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYS - RT ENG IDG VALVE CB POOPED IN FLT (M31). INSPECTED RT IDG VALVE WIRING, CLEANED CONNECTOR TO IDG VALVE. T/S IAW FIM 24-20-00. RESET C/B,
- [SDR HALA2011102400488](https://openairdocs.org/sdr/HALA2011102400488), Oct 24, 2011: WARNING MESSAGE. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - PACK HIGH FLOW INHIBIT MESSAGE. TROUBLE SHOT IAW FIM 21-51-00/101, RESET PACK RECIRCULATION FANS AND PACK CONTROLLERS. OP CHECKED NORMAL
- [SDR HALA2011101000451](https://openairdocs.org/sdr/HALA2011101000451), Oct 10, 2011: LINK. BROKEN. ETOPS SIGNIFICANT SYS - DURING NR 2 ENG EXTERNAL INSPECTION, FOUND TURBINE COOLING DUCT SUPPORT LINK AT 2 O'CLOCK POS BROKEN. R & R SUPPORT LINK AND OK FOR SERV
- [SDR HALA2011101000446](https://openairdocs.org/sdr/HALA2011101000446), Oct 10, 2011: LINK. BROKEN. ETOPS SIGNIFICANT SYS - DURING NR 2 ENG. EXTERNAL INSPECTION, FOUND TURBINE COOLING DUCT SUPPORT LINK AT 2 O' CLOCK POS BROKEN. R & R SUPPORT LINK AND OK FOR SE
- [SDR HALA2011081900374](https://openairdocs.org/sdr/HALA2011081900374), Aug 19, 2011: A/C PACK. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - LT PACK TEMP LIGHT CAME ON TWICE ON APPROACH CLOSE TO FINAL THEN WENT OUT. DUCT PRESSURE NORMAL. PERFORMED PACT TEMP CONTROLLER BITE PRO
- [SDR HALA2011070600316](https://openairdocs.org/sdr/HALA2011070600316), Jul 6, 2011: INDICATION SYS. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - DURING CLIMB & CRUISE, NOTED ENGINE INDICATIONS CLIMB - N1-LT 104.3 RT 104.3, EGT-LT 818 RT 844, N2-LT 103.2 RT 106.6, FF-LT 10.0 RT 10.
- [SDR HALA2011070500309](https://openairdocs.org/sdr/HALA2011070500309), Jul 5, 2011: LAMP. INOPERATIVE. ETOPS SIGNIFICANT SYS - LT FWD FUEL PUMP PRESSURE LIGHT DOES NOT ILLUMINATE PUMP OFF, ALSO DOES NOT TEST. RELAMPED L FWD FUEL PUMP SWITCH, OPS CK OK.
- [SDR HALA2011062500289](https://openairdocs.org/sdr/HALA2011062500289), Jun 25, 2011: DUCT. LEAKING. ETOPS SIGNIFICANT SYS - ATB - LT PACK HAS AIR LEAK. R & R OUTLET DUCT ON LT PACK AND TEMP SENSOR BULB IAW AMM 21-52-01 AND AMM 21-51-03. OPS AND LEAK CK PENDING
- [SDR HALA2011062500288](https://openairdocs.org/sdr/HALA2011062500288), Jun 25, 2011: CIRCUIT CARD. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - INTERMITTENT FLICKERING RT DUCT LEAK LIGHT WITH RT DUCT LEAK EICAS MSG DURING CLIMB OUT. NO OTHER ABNORMAL INDICATIONS. ACCOMPLISHED FIM
- [SDR HALA2011061100262](https://openairdocs.org/sdr/HALA2011061100262), Jun 11, 2011: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ILLUMINATED ON EICAS. C/W FIM 27-21-00/101, FIG 104 CLEANED CONNECTORS ON RUDDER RATIO ACTUATOR, OK FOR SERVICE.
- [SDR HALA2011052700240](https://openairdocs.org/sdr/HALA2011052700240), May 27, 2011: HELICOIL. MISINSTALLED. NEW AUTO THROTTLE CLUTCH ASSY FOUND TO HAVE HELICOIL INSERTS INSTALLED INCORRECTLY. REPOSITIONED HELICOIL INSERTS.
- [SDR ANZY2011050301](https://openairdocs.org/sdr/ANZY2011050301), May 24, 2011: CLUTCH. MISOVERHAULED. UNABLE TO FIT BOLTS TO REPLACEMENT AUTO THROTTLE CLUTCH PACK. THE REPLACEMENT AUTO THROTTLE CLUTCH PN 253T7204-2 WAS REQUIRED TO ALLOW REMOVAL OF A LOAN ITEM. W
- [SDR HALA2011051700238](https://openairdocs.org/sdr/HALA2011051700238), May 17, 2011: SPAR CAP. CORRODED. RT WING - OTBD T/E FLAP HAS EVIDENCE OF CORROSION ON UPPER AFT SPAR CAP AT INBD END. CORROSION FOUND BEYOND LIMITS SRM 51-10-02-09-0 REV 85. REPAIR CARRIED OUT.
- [SDR HALA2011051600239](https://openairdocs.org/sdr/HALA2011051600239), May 16, 2011: SKIN. CRACKED. CRACKS BETWEEN FASTENERS OF FAIRING SKIN. CONTACT BETWEEN LT MLG DOOR AND SKIN AT FWD EDGE. NO ADJUSTMENT AVAILABLE ON MOG DOOR. (FWD & AFT).
- [SDR HALA2011051000191](https://openairdocs.org/sdr/HALA2011051000191), May 10, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS -RT DUCT LEAK LIGHT ON OVERHEAD PANEL WITH EICAS RT BLEED DUCT LEAK FLICKERED ON/OFF NUMEROUS TIMES DURING FLIGHT. FIM 26-18-00 C/W SYS & 
- [SDR HALA2011041600157](https://openairdocs.org/sdr/HALA2011041600157), Apr 16, 2011: TRANSMITTER. OUT OF ADJUST. ETOPS SIGNIFICANT SYS. ON TAXI CHECK SELECTING FLAP 5, NOTICED A SIGNIFICANT DIFFERENCE IN AILERON DROOP FROM LT TO RT. BITE FSEU & PSEU NO FAULTS NOTED. NO EIC
- [SDR HALA2011022100117](https://openairdocs.org/sdr/HALA2011022100117), Feb 21, 2011: ACTUATOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - AILERON LOCKOUT AT 310KTS LASTED FOR 2 MIN(CLIMB OUT). T/S PER FIM 27-11-00 FIG. 104.LEFT LOCKOUT ACTUATOR FAILED TWICE DURING CHECK.
- [SDR HALA2011022000109](https://openairdocs.org/sdr/HALA2011022000109), Feb 20, 2011: WARNING MESSAGE. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - EICAS MESSAGE AILERON LOCKOUT ILLUMINATED AT HIGH SPEED (270KTS ACCELERATING) FOR 2 MIN THEN EXTINGUISHED. OTBD AILERONS INDICATED NORMA
- [SDR HALA2011022000108](https://openairdocs.org/sdr/HALA2011022000108), Feb 20, 2011: WARNING MESSAGE. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - EICAS MESSAGE AILERON LOCKOUT ILLUMINATED AT HIGH SPEED (270 KTS ACCELERATING) FOR 2 MIN THEN EXITINGUISHED. OTBD AILERONS INDICATED NOR

All 233: https://openairdocs.org/deregistered/N597HA-2014-07-30/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20131031021499I](https://openairdocs.org/incident/20131031021499I), Oct 31, 2013: Boeing 767-332 (N597HA), Sacramento, CA, Minor damage. Hawaiian airline flight 20 on approach to Sacramento intl airport reported a birdstrike at 1800 feet. No emergency declared. An engine shutdown was not…

## Other aircraft with N597HA

- [Registered now](https://openairdocs.org/aircraft/N597HA): Zipline International P2 ZIP, S/N 18736P22801

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