# N598HA: 1986 Boeing 767-332, registration cancelled 2015-02-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 23, 2015
- 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: 23278
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 24, 1986
- Certificate issued: April 6, 2006
- Last registry action: November 26, 2013
- Mode S code: A7BBCF
- 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/N598HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=598HA
- Page: https://openairdocs.org/deregistered/N598HA-2015-02-23

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 (227, newest 50)

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

- [SDR HALA2014111700193](https://openairdocs.org/sdr/HALA2014111700193), Nov 17, 2014: OVERHEAT LOOP. MALFUNCTIONED. ENGINE FIRE OVERHEAT LOOP 2 FAULT. FOUND BAD O/H LOOP. REPLACED LOOP ASSY NR 2 ENGINE NR 2 SYS IAW AMM 26-11-02.
- [SDR HALA2014110600183](https://openairdocs.org/sdr/HALA2014110600183), Nov 6, 2014: ACCESSORY UNIT. MALFUNCTIONED. F/A REPORT THAT THEY HAD EMERGENCY AUDIO CHIMES ON FINAL 3-4 TIMES AND ALSO DUIRNG TAXI IN 2 TIMES, COCKPIT DID NOT INITIATE ANY EMERGENCY CHIMES. RESEATED AUDI
- [SDR HALA2014091100136](https://openairdocs.org/sdr/HALA2014091100136), Sep 11, 2014: WARNING MESSAGE. FALSE ACTIVATION. NO APU DUCT PRESSURE. IAW APU ECU BITE, FAULTING PT2 INLET PRESSURE SENSOR. RESET APU ECB. BITE TEST COMPLETED AND ALL PASSED. OPERATED APU BLEED VALVE SEVEARL 
- [SDR HALA2014081400117](https://openairdocs.org/sdr/HALA2014081400117), Aug 14, 2014: WIRE HARNESS. DAMAGED. LOST ALL FUEL TANK QTY PANEL INDICATIONS. REMOVE AND REPLACE RT TANK WIRING HARNESS IAW AMM 28-41-09.
- [SDR HALA2014081000113](https://openairdocs.org/sdr/HALA2014081000113), Aug 10, 2014: COMPENSATOR. MALFUNCTIONED. FUEL QTY INDICATOR STATUS MESSAGE ILLUMINATED. RT FUEL QTY AND TOTALIZER BLANK -CALC-OK. BITE OF FQ PRECESSOR SHOWED FAULTS A4, B3, C6. CAPACITANCE VALUES IAW 2
- [SDR HALA2014080900112](https://openairdocs.org/sdr/HALA2014080900112), Aug 9, 2014: PROCESSOR. MALFUNCTIONED. ALL FUEL TANK QTY INDICATIONS BLANK. EICAS MESSAGE FOR FUEL QTY CHANNEL DISPLAYED. R & R FUEL QTY PROCESSOR IAW AMM 28-41-08. OPS CHECKED OK.
- [SDR HALA2014060300075](https://openairdocs.org/sdr/HALA2014060300075), Jun 3, 2014: CONTROL UNIT. OUT OF ALIGNMENT. LEFT IRS SYS DISPLAYS 25 KNOTS GROUND SPEED & INCREASING. ALIGNED IRUS AND OPS CHECKED IAW MM34-51-00. ACFT OK FOR SERVICE.
- [SDR HALA2014040500044](https://openairdocs.org/sdr/HALA2014040500044), Apr 5, 2014: LINE. DAMAGED. AIR DIVERSION, RT HYD QTY INDICATOR ILLUMINATED. FOLLOWED QRH. NOTED QTY ON RT TO 0.48. HYD TUBE ASSY ON LT ANTI SKID SHUTTLE VALVE DAMAGED. FLEX LINE INSTALLED
- [SDR HALA2014021100023](https://openairdocs.org/sdr/HALA2014021100023), Feb 11, 2014: RVDT. MALFUNCTIONED. ENROUTE, STATUS MESSAGE OBSERVED FLAP AND SLAT ELEC MOC ADVISED, REQUESTED ACFT RETURN TO PAE. R & R NR 2 RVDT, AND CORRECTED MISWIRING AT TB215. PERFORMED GOOD
- [SDR HALA2014012100009](https://openairdocs.org/sdr/HALA2014012100009), Jan 21, 2014: ADC. UNKNOWN. F/O ALTIMETER IS NEAR RVSM LIMITS. R & R RT ADC IAW AMM 34-12-01-404-006. PERFORMED FUNCTIONAL TEST IAW AMM SUB TASK 34-12-01-744-016, CHECKED OK. LEAK CHECKED 
- [SDR HALA2014011000002](https://openairdocs.org/sdr/HALA2014011000002), Jan 10, 2014: GROMMET. CUT. LEFT ENGINE AFT THROTTLE CABLE CUTTING INTO PHENOLIC GROMMENT FAIRLEAD INBD OF PYLON. R & R AFT THROTTLE CABLE PHONOLIC GROMMET. OK FOR SERVICE.
- [SDR HALA2014010700001](https://openairdocs.org/sdr/HALA2014010700001), Jan 7, 2014: ALTIMETER. FAILED. F/O ALTIMETER FAILED DURING DESCENT. REPLACED ALTIMETER IAW AMM 34-13-01. OPS CHECKED IAW 34-12-00 GOOD.
- [SDR HALA2013101800158](https://openairdocs.org/sdr/HALA2013101800158), Oct 18, 2013: POWER SUPPLY. INOPERATIVE. BOTH FWD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED M1209 EMERGENCY LIGHT PWR SUPPLY IAW AMM 33-51-07.
- [SDR HALA2013101700157](https://openairdocs.org/sdr/HALA2013101700157), Oct 17, 2013: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE, BS 1562 BETWEEN STR 39R & 39L. REPLACED SHEAR TIE SRM 51-40-05-0G-0.
- [SDR HALA2013101700156](https://openairdocs.org/sdr/HALA2013101700156), Oct 17, 2013: SKIN. CORRODED. CORROSION ON INTERIOR SURFACE OF SKIN BS 1544 STR. 39L. REPAIRED SKIN ON ARA 598184.
- [SDR HALA2013101700155](https://openairdocs.org/sdr/HALA2013101700155), Oct 17, 2013: STRINGER. CORRODED. CORROSION ON BULK CARGO AFT BULKHEAD BS 1544 STRINGER 39R. REPAIRED STRINGER FROM BS 1550-1530 IAW SRM 53-00-03-2R-2.
- [SDR HALA2013101700154](https://openairdocs.org/sdr/HALA2013101700154), Oct 17, 2013: STRINGER. CORRODED. CORROSION AFT BULKHEAD BS 1544, STR 39L. REPAIRED STRINGER FROM BS 1555-1530 IAW SRM 53-00-03-2R-2.
- [SDR HALA2013101700153](https://openairdocs.org/sdr/HALA2013101700153), Oct 17, 2013: ROLLER TRAY. CRACKED. ROLLER TRAY AT BS 654+5 HAS TWO CRACKS. REPLACED ROLLER TRAY IAW DWG 451T1005, SRM 51-40-05-0G-0, AMM 51-21-10-307-020 AND 25-53-02-404-004.
- [SDR HALA2013101500152](https://openairdocs.org/sdr/HALA2013101500152), Oct 15, 2013: DOUBLER. CORRODED. CORROSION FOUND ON INTERIOR SURFACE OF E/E COOLING CUT OUT DOUBLER AT BS 478-479, S39R. REPAIRED DOUBLER IAW ARA 598180.
- [SDR HALA2013101500151](https://openairdocs.org/sdr/HALA2013101500151), Oct 15, 2013: STRINGER CLIP. CORRODED. CORROSION ON STRINGER CLIP AT 18R BS 1197+110. REPAIRED STRINGER CLIP IAW SRM 53-00-03-2R-1.
- [SDR HALA2013101500150](https://openairdocs.org/sdr/HALA2013101500150), Oct 15, 2013: SKIN. CORRODED. CORROSION FOUND ON INTERIOR SKIN AT BS 479-481, STR 39R. REPAIRED SKIN IAW ARA 598180.
- [SDR HALA2013101500149](https://openairdocs.org/sdr/HALA2013101500149), Oct 15, 2013: STRINGER. CORRODED. CORROSION ON STRINGER 36L, BS 452. REPAIRED STRINGER FROM BS 437-465 IAW SRM 53-00-03-2R.
- [SDR HALA2013101100148](https://openairdocs.org/sdr/HALA2013101100148), Oct 11, 2013: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BS 360, LBL 54.75, WL 200. REPAIRED SEAT TRACK IAW 53-00-52-2R-2.
- [SDR HALA2013101000147](https://openairdocs.org/sdr/HALA2013101000147), Oct 10, 2013: STRINGER. CRACKED. STRINGER END IS CRACKED AT OVERWING ILLUMINATION LIGHT BS 654+27, STR 19L. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013101000146](https://openairdocs.org/sdr/HALA2013101000146), Oct 10, 2013: STRINGER. CRACKED. STRINGER END IS CRACKED AT OVERWING ILLUMIATION LIGHT BS 654+39, STR 19L. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013101000145](https://openairdocs.org/sdr/HALA2013101000145), Oct 10, 2013: STRINGER. CRACKED. STRINGER END CRACKED AT OVERWING ILLUMIATION LIGHT BS 654+27, STR 19R. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013100900141](https://openairdocs.org/sdr/HALA2013100900141), Oct 9, 2013: PAN. CORRODED. CORROSION ON FWD CARGO BIN, MOTOR PAN 8R, BS 616, RBL 34. R & R PDU PAN IAW SRM 51-40-02-0G-0, 51-40-05-0G-0 AND AMM 25-53-01-404-010.
- [SDR HALA2013100900139](https://openairdocs.org/sdr/HALA2013100900139), Oct 9, 2013: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, BS 654+82, RBL-38. REPLACED FLOOR SUPPORT IAW DWG 143T5400 AND SRM 51-40-02-0G-0.
- [SDR HALA2013102300138](https://openairdocs.org/sdr/HALA2013102300138), Oct 9, 2013: FLOOR SUPPORT. CRACKED. CRACKED CABIN FLOOR SUPPORT BS 654+82 RBL-38. REPLACED SUPPORT IAW DWG 143T5400 AND SRM 51-40-02-0G-0.
- [SDR HALA2013091200111](https://openairdocs.org/sdr/HALA2013091200111), Sep 12, 2013: FILTER. UNKNOWN. DURING CLIMBOUT, RT FUEL MESSAGE DISPLAYED. DIVERTED TO AN ALTERNATE STATION. ACCOMPLISHED FUEL FILTER BYPASS TEST. NO PR'S NOTED. R & R FUEL FILTER AS A PRECAU
- [SDR HALA2013081200100](https://openairdocs.org/sdr/HALA2013081200100), Aug 12, 2013: IDG. FAILED. AIR DIVERSION - RT GEN DRIVE EICAS DISCONNECTED GEN DRIVE. R & R NR 2 IDG IAW AMM 24-11-01. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2013071600090](https://openairdocs.org/sdr/HALA2013071600090), Jul 16, 2013: PUMP. FAILED. LEFT HYD DEMAND PUMP FAILURE. R & R LT HYD ACMP IAW AMM 29-11-01, OPS AND LEAK CHECK GOOD.
- [SDR HALA2013041100037](https://openairdocs.org/sdr/HALA2013041100037), Apr 11, 2013: ACTUATOR. INOPERATIVE. LT FUEL SPAR VALVE LIGHT REMAINED ILLUMINATED AFTER ENG SHUTDOWN. R & R LT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.
- [SDR HALA2013010300002](https://openairdocs.org/sdr/HALA2013010300002), Jan 3, 2013: PUMP. FAILED. RT HYD PRIM PUMP EICAS. CHECKED RT HYD PUMP DEPRESS PLUG, WIRING CHECKED OK IAW SYS SCH MANUAL 29-00-03. RT ENG HYD PUMP SPLINE INTACT, HEAD PRESSURE LINE FROM 
- [SDR HALA2012123100238](https://openairdocs.org/sdr/HALA2012123100238), Dec 31, 2012: SHAFT. SHEARED. DURING CLIMBOUT RECEIVED " B HYD PRIM PUMP " EICAS MESSAGE ALONG WITH ASSOCIATED "PRESS" LIGHT ON OVERHEAD PANEL. VOLTAGE CHECK AT HYD PUMP DEPRESS VALVE GOOD I
- [SDR HALA2012072700185](https://openairdocs.org/sdr/HALA2012072700185), Jul 27, 2012: TERMINAL. SHORTED. ETOPS SIGNIFICANT SYSTEM, UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUN
- [SDR HALA2012072700184](https://openairdocs.org/sdr/HALA2012072700184), Jul 27, 2012: GROUND STUD. ARCED. ETOPS SIGNIFICANT SYS - UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUND 
- [SDR HALA2012060300156](https://openairdocs.org/sdr/HALA2012060300156), Jun 3, 2012: BLADE. DAMAGED. NR 2 ENGINE BOROSCOPE INDICATES ENGINE DAMAGED. FOUND FIRST STAGE HPT BLADES DAMAGED BEYOND AMM LIMITS. CHANGED NR 2 ENGINE. LEAK CHECK & OPS CHECK GOOD. OK FOR
- [SDR HALA2012052200144](https://openairdocs.org/sdr/HALA2012052200144), May 22, 2012: FUEL FILTER. WARNING LIGHT. DURING CLIMB, AFTER 1000 FT AGL. EICAS DISPLAY RT ENGINE FUEL FILTER. R & R RT ENGINE FUEL FILTER IAW AMM73-11-02 ENG RUN. OPS & LEAK CHECKED GOOD, OK FOR SERVI
- [SDR HALA2012030300102](https://openairdocs.org/sdr/HALA2012030300102), Mar 3, 2012: TEE FITTING. CRACKED. INBD TEE FITTING ON AFT ATTACH BEAM FOR INBD AILERON ACTUATOR ACCESS PANEL CRACKED. REPLACED INBD TEE FITTING ON AFT ATTACH BEAM, SECURITY CHECKED GOOD.
- [SDR HALA2011123000622](https://openairdocs.org/sdr/HALA2011123000622), Dec 30, 2011: SENSOR. DIRTY. ETOPS SIGNIFICANT SYS - AFT CABIN TEMP INDICATION IS APPROX 20 DEG TOO HIGH, FWD AND MID SHOW APPROX 73 AFT 93, F/A'S REPORT TEMP FEELS NORMAL. FOUND AFT CABIN 
- [SDR HALA2011121500590](https://openairdocs.org/sdr/HALA2011121500590), Dec 15, 2011: IDG. FAILED. ETOPS SIGNIFICANT SYS - LEFT GENERATOR DRIVE LIGHT ILLUMINATED, DISCONNECTED LEFT IDG. REMOVED NR 1 ENGINE IDG REF AMM 24-11-01. INSTALLED IDG IAW MM 24-11-01-4
- [SDR HALA2011121400589](https://openairdocs.org/sdr/HALA2011121400589), Dec 14, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. SERVICED LT ENGINE IDG, BITE CHECK COMPLETED, ON BPCU & NO FAULTS NOTED
- [SDR HALA2011112300540](https://openairdocs.org/sdr/HALA2011112300540), Nov 23, 2011: FAN. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - AFT EQUIPMENT EXHAUST FAN 1 LIGHT ON. RESET AFT EQUIPMENT EXHAUST FAN & OPS CHECKED OK.
- [SDR HALA2011102700496](https://openairdocs.org/sdr/HALA2011102700496), Oct 27, 2011: TRANSCEIVER. FAILED. ETOPS SIGNIFICANT SYS - RETURN NOISY ON HSI WXR DISPLAY AND WXR INDICATOR DISPLAY INTERMITTENT. REPLACED WXR TRANSCEIVER IAW MM 34-43-01, GROUND CHECK OK.
- [SDR HALA2011102500493](https://openairdocs.org/sdr/HALA2011102500493), Oct 25, 2011: FMC. MALFUNCTIONED. ETOPS SIGNIFICANT SYS. - FUEL CONFIGURATION EICAS MESSAGE, TOTALIZER AND CALCULATED FUEL GREATER THAN 3000 LBS DIFFERENCE. ITEM DIS NR 008921 ON M55 T/S TOTAL F
- [SDR HALA2011102300487](https://openairdocs.org/sdr/HALA2011102300487), Oct 23, 2011: INDICATION SYS. UNKNOWN. ETOPS SIGNIFICANT SYS - FUEL TOTALIZER QTY GREATER THAN CALCULATE FUEL QTY BY 2400 LBS. CALCULATED FUEL APPEARS TO BE MORE ACCURATE. PERFORMED FIM 28-41-00, FIG
- [SDR HALA2011102100480](https://openairdocs.org/sdr/HALA2011102100480), Oct 21, 2011: UNKNOWN. UNKNOWN. ETOPS SIGNIFICANT SYS - AT TOP OF DESCENT, FUEL TOTALIZER READ 21.7. CALCULATED READ 18.5, A DIFFERENC OF -3.2. PERFORMED FIM 28-41-00, FIG 107, NO FAULTS NOTED
- [SDR HALA2011101500462](https://openairdocs.org/sdr/HALA2011101500462), Oct 15, 2011: SHUTOFF VALVE. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - LT PACK REMAINS OFF WITH SWITCH IN AUTO OR STBY FOR OVER 1 MIN BEFORE COMING ON. TROUBLESHOT IAW FIM 21-51-22. R & R LT PACK FLOW CONTRO
- [SDR HALA2011100700440](https://openairdocs.org/sdr/HALA2011100700440), Oct 7, 2011: ENGINE. FAILED. ETOPS SIGNIFICANT SYS - ON APPROACH, AT APPROX 2,400, FLAPS 20, STEADY THROTTLE POSITION, BOTH PILOTS HEARD A MUTED THUD OR BANG AND SHORTLY NOTICED THE LT ENGI

All 227: https://openairdocs.org/deregistered/N598HA-2015-02-23/reports.md

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