# N584HA: Boeing 767-3G5, registration cancelled 2013-12-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 17, 2013
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-3G5](https://openairdocs.org/model/boeing-767-3g5) (registry code 1385126)
- Serial number: 24258
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: March 21, 2002
- Certificate issued: May 21, 2013
- Last registry action: December 17, 2013
- Mode S code: A78574
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles)
- Owner type: Corporation
- Owner's area on the map: 34.0564° N, 118.4137° W: Placed by OpenAirDocs at the center of ZIP code 90067, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N584HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=584HA
- Page: https://openairdocs.org/deregistered/N584HA-2013-12-17

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 767-3G5: https://openairdocs.org/model/boeing-767-3g5.md

## Service difficulty reports (215, newest 50)

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

- [SDR HALA2013021200018](https://openairdocs.org/sdr/HALA2013021200018), Feb 12, 2013: CONNECTOR. BROKEN. AT DEPARTURE TIME CREW REPORTS MID GALLEY EMERGENCY LIGHTING FLOOR STRIP LT SIDE CONNECTOR BROKE LOOSE. RESECURED MID GALLEY EMERGENCY LIGHT FLOOR STRIP WIRES. 
- [SDR HALA2012091700208](https://openairdocs.org/sdr/HALA2012091700208), Sep 17, 2012: WARNING LIGHT. FALSE ACTIVATION. NR 1 ENGINE AND APU FIRE LOOP SHOWED EICAS MESSAGE NO TEST. PERFORMED ENG AND APU FIRE LOOP TEST IAW FIM 26-15 FIG 803 & 804. OPS CHECKED GOOD, NO FAULTS NOTED.
- [SDR HALA2012071800176](https://openairdocs.org/sdr/HALA2012071800176), Jul 18, 2012: RELIEF VALVE. LEAKING. RIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSU
- [SDR HALA2012071000170](https://openairdocs.org/sdr/HALA2012071000170), Jul 10, 2012: BYPASS VALVE. LEAKING. APU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW A
- [SDR HALA2012070200166](https://openairdocs.org/sdr/HALA2012070200166), Jul 2, 2012: STARTER. SEIZED. NR 2 ENGINE WOULD NOT START, NO N1 OR OIL PRESSURE NOTED. PNEU PRESSURE WAS NORMAL & START VALVE OPENED AND CLOSE NORMAL. FOUND NR 2 ENGINE STARTER SEIZED. R & 
- [SDR HALA2012070200165](https://openairdocs.org/sdr/HALA2012070200165), Jul 2, 2012: COUPLING. SHEARED. RT ENGINE STARTER TO GEARBOX COUPLING SHEARED. R & R STARTER DRIVE COUPLING IAW AMM 72-61-09.
- [SDR HALA2012060500159](https://openairdocs.org/sdr/HALA2012060500159), Jun 5, 2012: WARNING LIGHT. FALSE ACTIVATION. RT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 EN
- [SDR HALA2012042900127](https://openairdocs.org/sdr/HALA2012042900127), Apr 29, 2012: SENSOR. OPEN. CLIMBING THROUGH 9,000' RECEIVED "RT FWD WINDOW" LIGHT AND INOPERATIVE LIGHT ON, FOLLOWED QRH. LIGHT STAYED ON, RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00
- [SDR HALA2012042900126](https://openairdocs.org/sdr/HALA2012042900126), Apr 29, 2012: CONTROL UNIT. MALFUNCTIONED. CLIMBING THROUGH APPROX 25,000' RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. RET
- [SDR HALA2012021800126](https://openairdocs.org/sdr/HALA2012021800126), Apr 29, 2012: CONTROL UNIT. MALFUNCTIONED. CLIMBING THROUGH APPROX 25,000', RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. AC
- [SDR HALA2012031800113](https://openairdocs.org/sdr/HALA2012031800113), Mar 18, 2012: CONNECTOR. UNSECURE. ON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING BETWEEN L1 & R1 DOOR INOPERATIVE. RECONNECTED AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR. OPS CHECKE
- [SDR HALA2012022600081](https://openairdocs.org/sdr/HALA2012022600081), Feb 26, 2012: WARNING MESSAGE. FALSE ACTIVATION. LEFT PACK TEMPERATURE EICAS MESSAGE. LT PACK INOP ON OVERHEAD MULTIPLE TIMES AT 5 SECS EACH TIME, SELECTED STANDBY IAW QRH. BITE CHECKED LT PACK CONTROLLER, NO 
- [SDR HALA2012011900045](https://openairdocs.org/sdr/HALA2012011900045), Jan 19, 2012: ENGINE. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FRO
- [SDR HALA2012011700041](https://openairdocs.org/sdr/HALA2012011700041), Jan 17, 2012: GENERATOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - GENERATOR FIELD MANUAL RESET (RT) FIELD OFF LIGHT ON. BITE CHECKED BPCU AND NO FAULTS NOTED. RAN NR 2 ENGINE RESET NR 2 GENERATOR. OPS C
- [SDR HALA2012011600035](https://openairdocs.org/sdr/HALA2012011600035), Jan 16, 2012: DISPLAY. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - F/O RADAR SCREEN FLICKERS IN WX MODE. REPLACED F/O EMSI DISPLAY. OPS CHECKED OK IAW MM 34-22-00. PERFORMED MCDP TEST 30 TEST PASSED.
- [SDR HALA2012011500036](https://openairdocs.org/sdr/HALA2012011500036), Jan 15, 2012: TRANSCEIVER. FAILED. ETOPS SIGNIFICANT SYS - AMBER RADAR ALITMETER WARNING BOX ILLUMINATED ON FO ADI " NO LAND 3" APPEARS IN AUTOLAND STATUS. REPLACED RT RADIO ALTIMETER TRANSCEIVER
- [SDR HALA2012011300024](https://openairdocs.org/sdr/HALA2012011300024), Jan 13, 2012: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYS - ON POST FLIGHT FOUND ENGINE NR 2 GENERATOR FIELD OFF LIGHT ILLUMINATED. ACCOMPLISHED BPCU BITE CHECK IAW AMM 24-22-00-745-071. RERACKED 
- [SDR HALA2012011100018](https://openairdocs.org/sdr/HALA2012011100018), Jan 11, 2012: GCU. FAILED. ETOPS SIGNIFICANT SYS - FOUND RT GENERATOR FIELD LIGHT ILLUMINATED ON P61. SERVICED IDG RESET FIELD LIGHT IAW AMM 24-22-00. PERFORMED IDLE ENGINE RUN. FAULT DID
- [SDR HALA2012010100002](https://openairdocs.org/sdr/HALA2012010100002), Jan 1, 2012: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYS - EICAS MESSAGE TRACK FAIL ILLUMINATED AFTER TAKEOFF. PERFORMED TROUBLESHOOTING, PLACED IECAS COMPUTER SELECTED SWITCH TO ALTERNATE POSITI
- [SDR HALA2011122600618](https://openairdocs.org/sdr/HALA2011122600618), Dec 26, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - AFTER ENGINE SHUTDOWN, NOTE GENERATOR FIELD TRIP ON RT ENG. ACCOMPLISHED FIM 24-20-00. NO FAULTS NOTED. RESET RT GEN FIELD SWITCH. GROUN
- [SDR HALA2011122500611](https://openairdocs.org/sdr/HALA2011122500611), Dec 25, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - AUX PANEL HAS GENERATOR FIELD OFF INDICATOR ON AFTER LANDING. PERFORMED BPCU BITE ON NR 2 BPCE IAW FIM 24-20-00, FIG 101. INSPECTED WIRI
- [SDR HALA2011122200606](https://openairdocs.org/sdr/HALA2011122200606), Dec 22, 2011: SENSOR. OUT OF POSITION. ON TAXI OUT LT FWD ENTRY DOOR, EICAS AND ENTRY DOORS WARNING LIGHT ILLUMINATED. UPON BEING TUGGED IN LIGHT WENT OUT BY ITSELF. FOUND LT FWD ENTRY DOOR OPEN SENS
- [SDR HALA2011120200596](https://openairdocs.org/sdr/HALA2011120200596), Dec 2, 2011: SUPPORT CHANNEL. CORRODED. INTERNAL SUPPORT CHANNEL CORRODED, BS 1425 AT DRAIN MAST FOR WASTE WATER. FITTED NEW SKIN STIFFENER IAW SRM 53-00-03.
- [SDR HALA2011120200581](https://openairdocs.org/sdr/HALA2011120200581), Dec 2, 2011: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED 1 INCH, BETWEEN BS 742 AND 764 AT RBL 40. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, D634T210, REV 87.
- [SDR HALA2011120100584](https://openairdocs.org/sdr/HALA2011120100584), Dec 1, 2011: FLOORBEAM. CORRODED. AFT CARGO HOLD, FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE A FRAME STA 1197+66, HAS CORROSION OUTSIDE SRM LIMITS AND NUMEROUS CORRODED ANCHOR NUTS. INNER CHORD PN
- [SDR HALA2011113000583](https://openairdocs.org/sdr/HALA2011113000583), Nov 30, 2011: FLOORBEAM. CORRODED. NET CARGO FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE AT BS 1175, HAS CORROSION AS MARKED. REPLACED IAW SRM 51-40-02, REV 87.
- [SDR ANZY20111120102](https://openairdocs.org/sdr/ANZY20111120102), Nov 30, 2011: STRINGER. CORRODED. ON C CHECK, CORROSION OF STRINGER AT S34R HAD CAUSED MULTIPLE HOLES IN EXTRUSION TO THE POINT THAT NO STRUTURAL MATERIAL WAS LEFT. REPAIR UNDER WAY AT THIS TIME
- [SDR HALA2011112900597](https://openairdocs.org/sdr/HALA2011112900597), Nov 29, 2011: MECHANISM. CORRODED. NLG FWD DOOR OPERATING MECHANISM FOUND CORRODED BS 180.5. REPLACED NLG FWD DOOR OPERATING MECHANISM ON LT SIDE IAW AMM 32-22-04, REV 77.
- [SDR HALA2011112900580](https://openairdocs.org/sdr/HALA2011112900580), Nov 29, 2011: STRINGER CLIP. CRACKED. CRACK IN STRINGER CLIP AT STA. 1678, S3R, 1". REPLACED STRINGER CLIP IAW SRM 51-40-02.
- [SDR HALA2011112800602](https://openairdocs.org/sdr/HALA2011112800602), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 605. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800600](https://openairdocs.org/sdr/HALA2011112800600), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800601](https://openairdocs.org/sdr/HALA2011112800601), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011128000600](https://openairdocs.org/sdr/HALA2011128000600), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 575. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800599](https://openairdocs.org/sdr/HALA2011112800599), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5, AT STA. 565. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800598](https://openairdocs.org/sdr/HALA2011112800598), Nov 28, 2011: SEAT TRACK. CORRODED. SEAT TRACK FOUND CORRODED AT RBL 88.5 AT BS 544. REPLACED SEAT TRACK IAW 53-00-52-REV 87.
- [SDR HALA2011112800592](https://openairdocs.org/sdr/HALA2011112800592), Nov 28, 2011: WEDGE. DEBONDED. NR 8 SLAT OTBD END HAS A T/E WEDGE AREA OF DISBOND. REPAIRED IAW SRM 57-43-02-2R-1, REV 87 AND 51-70-10, REV 87.
- [SDR HALA2011112800591](https://openairdocs.org/sdr/HALA2011112800591), Nov 28, 2011: SKIN. DAMAGED. LIGHTING STRIKE NEAR RIVET HEAD AT BS 395, 1 INCH BELOW S33L. DAMAGE REMOVED IAW SRM 53-00-01-2R-8 REV 88. FASTENER REPLACED IAW SRM 51-40-02, REV 88.
- [SDR HALA2011112800582](https://openairdocs.org/sdr/HALA2011112800582), Nov 28, 2011: TEE FITTING. CORRODED. CORROSION ON TEE FITTING BETWEEN STA 808 & 933, BETWEEN RBL 10 & LBL 10. REPLACED TEE FITTING IAW SRM 51-40-02.
- [SDR HALA2011113000512](https://openairdocs.org/sdr/HALA2011113000512), Nov 13, 2011: ENGINE. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - LEFT ENGINE HESITATED AT 50 PERCENT N2 DURING ENGINE START AFTER START VALVE CLOSED AND STARTER CUTOUT WITH SELECTOR BACK IN AUTO. OTHER
- [SDR HALA2011110100500](https://openairdocs.org/sdr/HALA2011110100500), Nov 1, 2011: UNKNOWN. UNKNOWN. ETOPS SIGNIFICANT SYS - HF DATALINK INOPERATIVE BOTH RADIOS, VOICE OK. PERFORMED A BITE TEST ON BOTH HF TRANSCEIVERS, NO FAULTS NOTED. PERFORMED A SYS TEST IAW 
- [SDR HALA2011102300484](https://openairdocs.org/sdr/HALA2011102300484), Oct 23, 2011: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS - EICAS STATUS MESSAGE LT ENG EEC C1 DISPLAYED ON LOWER EICAS. TROUBLE SHOT IAW FIM 73-21-00. PIMU CHECKED AND HAD RNG FAIL-CLEARED MESSAG
- [SDR HALA2011102300483](https://openairdocs.org/sdr/HALA2011102300483), Oct 23, 2011: FUEL SYS. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - RT FUEL QTY DECREASED 2800 WITH CENTER TANK PUMPS ON. ELAPSED TIME 42MINS. DECREASED AN ADDITIONAL 600 NR DURING THE NEXT 56 MINS. W/C. 
- [SDR HALA2011100900441](https://openairdocs.org/sdr/HALA2011100900441), Oct 9, 2011: OVERHEAT SYS. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - FOUND LEFT ENGINE OVERHEAT LOOP 2 STATUS MESSAGE ON ETOPS CHECK. ACCOMPLISHED FIM 26-11-00, FIG 104. SWAPPED LT ENGINE O/H CARDS, RERACK
- [SDR HALA2011100600434](https://openairdocs.org/sdr/HALA2011100600434), Oct 6, 2011: INDICATOR. INOPERATIVE. ETOPS SIGNIFICANT SYS -CAPTS ALTIMETER OFF FLAG FLICKERS CONTINUOUSLY. REPLACED CAPT ALTIMETER INDICATOR IAW AMM 34-13-01-404-004, TEST GOOD.
- [SDR HALA2011091700405](https://openairdocs.org/sdr/HALA2011091700405), Sep 17, 2011: OIL SYSTEM. LEAKING. ETOPS SIGNIFICANT SYS - OIL FOUND IN LT ENGINE FAN COWL. OIL LEAKAGE BELOW IDLE SPEED IS WITHIN LIMITS IAW AMM 71-00-00-795-003-N00. OK FOR SERVICE.
- [SDR HALA2011082100377](https://openairdocs.org/sdr/HALA2011082100377), Aug 21, 2011: APU. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - AFTER TURNING OFF THE LT PACK AT THE GATE APU AUTO SHUTDOWN NOTE: JUST BEFORE SHUTDOWN APU BLEED DUCT PRESSURE DROPPED TO APPROX 10 PSI.
- [SDR HALA2011081900379](https://openairdocs.org/sdr/HALA2011081900379), Aug 19, 2011: DUCT. DAMAGED. ETOPS SIGNIFICANT SYS - 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVER PRESSURE VENT DUCT HAVE HOLES IN THEM. R & R 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVERPRESSURE V
- [SDR HALA2011081600371](https://openairdocs.org/sdr/HALA2011081600371), Aug 16, 2011: TRANSMITTER. MALFUNCTIONED. ETOPS SIGNIFICANT SYS - ASA NO LAND 3 DISPLAYED CENTER RADIO ALTIMETER. RA FLAG DISPLAYED FROM T/O TO CRUISE ALT, THEN RESUMED NORMAL OPS. R & R RADIO ALTIMETER
- [SDR HALA2011081400365](https://openairdocs.org/sdr/HALA2011081400365), Aug 14, 2011: B-NUT. LOOSE. ETOPS SIGNIFICANT SYS - NR 1 ENG TOOK 6 PINT DURING SERVICING. TIGHTENED OIL INLET TUBE B-NUT IAW 79-21-01, LEAK CHECKED GOOD. (AT OIL COOLER) (ACFT M/M 79-21-0
- [SDR HALA2011080400348](https://openairdocs.org/sdr/HALA2011080400348), Aug 4, 2011: FLEX LINE. LEAKING. C-HYD QTY DECREASED TO 0.58 IN FLIGHT, 0.40 ON GROUND. REPLACED NR 4 BRAKE FLEX LINE ABOVE RT MLG IAW AMM 32-42-02. REF IPC 32-41-62-05, ITEM 172. LEAK AND OPS 

All 215: https://openairdocs.org/deregistered/N584HA-2013-12-17/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR11LA071](https://openairdocs.org/ntsb/WPR11LA071), Dec 3, 2010: Boeing 767 (N584HA), Pago Pago, Antarctica, no damage. Probable cause: The airplane’s encounter with convectively-induced turbulence, which resulted in serious injury to one flight attendant.

## 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.

- [Accident 20101203053579A](https://openairdocs.org/incident/20101203053579A), Dec 3, 2010: Boeing 767-3G5 (N584HA), Honolulu, HI, No damage. Aircraft climbing through flight level 180 encountered clear air turbulence resulting in 2 flight attendant injuries, one minor (facial contusions) and one…

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