# N906SJ: Lockheed 382G, registration cancelled 1999-10-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 8, 1999
- Exported to: São Tomé and Príncipe
- Status when cancelled: Valid registration
- Airframe: [Lockheed 382G](https://openairdocs.org/model/lockheed-382g) (registry code 526414U)
- Data sheets: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) (OpenAirDocs)
- Serial number: 4477
- Type of aircraft: Fixed wing multi engine
- Certificate issued: September 28, 1999
- Last registry action: September 28, 1999
- Mode S code: AC870F
- Owner when cancelled: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N906SJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=906SJ
- Page: https://openairdocs.org/deregistered/N906SJ-1999-10-08

From the FAA registry file of November 5, 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 Lockheed 382G: https://openairdocs.org/model/lockheed-382g.md

## Service difficulty reports (16)

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

- [SDR SRAA971206](https://openairdocs.org/sdr/SRAA971206), Dec 5, 1997: LATCH. UNLOCKED. DURING CLIMBOUT, MASTER DOOR WARNING LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE, ACCOMPLISHED AIR TURNBACK. INSPECTED CARGO DOOR LATCH SYSTEM AND FOUND
- [SDR SRAA971013](https://openairdocs.org/sdr/SRAA971013), Oct 28, 1997: CONTROL ROD. STRIPPED. DURING LANDING, NR 1 PROP WOULD NOT GO INTO THE BETA RANGE. ON INSPECTION FOUND THREADS ON THE CONTROL ROD AND ROD ENDS STRIPPED. REPLACED CONTROL ROD ON PROP C
- [SDR SRAA971006](https://openairdocs.org/sdr/SRAA971006), Oct 11, 1997: HYD FITTING. CRACKED. AFTER TAKEOFF, NR 1 ENGINE LOST ALL HYDRAULIC PRESSURE, DUMPED FUEL AND ACCOMPLISHED AIR TURNBACK TO STN. FOUND NR 1 HYD PUMP PRESURE FITTING CRACKED. REPLACED 
- [SDR SRAA970717](https://openairdocs.org/sdr/SRAA970717), Jul 23, 1997: DUCT. FAILED. ON ENGINE START, FLIGHT 514 OUT OF LTBA, NR 1 ENGINE NACELLE OVERHEAT LIGHT CAME ON. ENGINE START TERMINATED AS QRH. REMOVED AND REPLACED AIR DUCT BETWEEN START
- [SDR SRAA970716](https://openairdocs.org/sdr/SRAA970716), Jul 23, 1997: FIRE LOOP. BROKEN. ON PREFLIGHT OUT OF AAB, FLIGHT 513, NR 3 ENGINE FIRE WARNING WOULD NOT TEST. REPLACE FIRE WARNING ELEMENT IAW MM CH 26, OPS CK GOOD.
- [SDR SRAA970616](https://openairdocs.org/sdr/SRAA970616), Jun 27, 1997: INDICATOR SOCKET. DEFECTIVE. NR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING CRUISE, OIL PRESSURE GAUGE READ 240 PSI, FOR GEARBOX, 50 PSI FOR ENGINE, QUANTITY AT 10.5 GAL AND OIL TEMP AT 
- [SDR SRAA970612](https://openairdocs.org/sdr/SRAA970612), Jun 22, 1997: WINDOW. SHORT CIRCUIT. DURING FLIGHT, CO-PILOT'S CENTER SIDE WINDOW NESA SMOKED AND SPARKED. PULLED CIRCUIT BRAKER, SPARKING CONDITION CEASED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPEC
- [SDR SRAA970519](https://openairdocs.org/sdr/SRAA970519), May 28, 1997: BATTERY. DISCHARGED. DURING DEBRIEF AT MHZ, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT WEAK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, SYSTEM OPS CHECKED GOOD PER MM CH 33.
- [SDR SRAA970516](https://openairdocs.org/sdr/SRAA970516), May 24, 1997: VALVE HOUSING. DEFECTIVE. DURING FLIGHT 527 FROM LERT TO LEMO, NR 4 PROPELLER RPM DECAYED TO 975, SHUT DOWN ENGINE AS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. FOUND NR 4 PROPELLER VALV
- [SDR SRAA970511](https://openairdocs.org/sdr/SRAA970511), May 12, 1997: ENGINE. FAILED. FLIGHT 527 REPORTED NR 1 ENGINE CAUSES FUMES FROM BOTH AIR CONDITIONING SYSTEMS WHEN BLEED IS OPEN. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER J/C 7101 AND 7
- [SDR SRAA970307](https://openairdocs.org/sdr/SRAA970307), Mar 24, 1997: LIGHT. DIM. DURING PREFLIGHT INSPECTION, FOUND FLIGHT DECK ESCAPE HATCH EMERGENCY LIGHT DIM. REMOVED AND REPLACED FLIGHT DECK EMERGENCY LIGHT ASSEMBLY, SYSTEM OPS CHECKED G
- [SDR SRAA970301](https://openairdocs.org/sdr/SRAA970301), Mar 2, 1997: ENGINE. DEFECTIVE. DURING TAXI IN FROM FLIGHT 507 AT MHZ, NOTICED OIL FUMES COMING FROM AIR CONDITIONING SYSTEM, SHUT DOWN AIR CONDITIONING SYSTEM. REPLACED NR 3 ENGINE, PERFORMED
- [SDR SRAA970207](https://openairdocs.org/sdr/SRAA970207), Feb 27, 1997: FITTING. LOOSE. ON ENGINE START AT RMS FOR FLIGHT 507, FOUND SMOKE IN COCKPIT WHILE NR 3 ENGINE WAS RUNNING, ABORTED ENGINE START. MOTORED NR 3 ENGINE, FOUND ENGINE OIL LEAK AT
- [SDR SRAA970205](https://openairdocs.org/sdr/SRAA970205), Feb 19, 1997: CONTROL BOX. MALFUNCTIONED. DURING TAXI OUT, BRAKES WENT INOP WITH ANTI-SKID ON. AIRCRAFT RETURNED TO BLOCK. FOUND ANTI-SKID CONTROL BOX MALFUNCTIONED. REPLACED ANTI-SKID CONTROL BOX, SYST
- [SDR SRAA961202](https://openairdocs.org/sdr/SRAA961202), Dec 3, 1996: BATTERIES. DISCHARGED. DURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW MM CH 33, OPS CHECKED GOOD.
- [SDR SRAA109507](https://openairdocs.org/sdr/SRAA109507), Oct 9, 1995: FUEL HEATER. DEFECTIVE. ON CLIMB-OUT FOR FLIGHT ADN5 OUT OF MIA, NOTICED OIL QUANTITY STARTED TO DROP AFTER LEVELING OFF, OIL COULD BE SEEN COMING OUT OF DRAIN MAST. SHUT DOWN NR 3 ENG

## 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 ANC95LA084](https://openairdocs.org/ntsb/ANC95LA084), Jun 5, 1995: Lockheed L-382E (N906SJ), Mcgrath, AK, substantial damage. Probable cause: FAILURE OF THE PILOT-IN-COMMAND TO ASSURE THE AIRPLANE WAS ADEQUATELY FLARED FOR LANDING.

## 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 19950605018059A](https://openairdocs.org/incident/19950605018059A), Jun 5, 1995: Lkheed 382G (N906SJ), Mcgrath, AK, Substantial damage. Landing approach path is over a hill. Runway short 3800 ft. rotated to arrest sink. Dragged the extended tail.

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