Skip to content
KnownTail
Aircraft record

N3796B1985 Lockheed 382G-44K-30

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 17, 2024.

Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply10 service difficulty reports

Registration
Deregistered
Last based in
Wilmington, DE
owner city / state
Engine
501-D22A · 4680 hp
Allison
Owners
1
since 2007
NTSB events
None
since 1982
ADs may apply
8
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Northcap LLC
Owner type
LLC
City, state
Wilmington, DE
Certificate issued
Mar 6, 2007
Canceled
Oct 17, 2024
Airworthiness
Standard · Transport
Airworthiness date
Oct 31, 2005

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Lockheed
Model
382G-44K-30
Year
1985
Serial number
5027
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
3
Engines
4
Max takeoff weight
20,000 and over lb
Mode S code
A45866

Engine

Make and model
Allison 501-D22a
Type
Turbo-prop
Power
4680 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2007 – 2024Northcap LLCWilmington, DE
  2. 1961 – 1970Individual ownerOklahoma City, OK · different airframe: Beechcraft C-50 S/N Ch-306

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (8)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2009-11-03Lockheed Model 382, 382B, 382E, 382F, and 382G Series AirplanesJun 4, 2009Airframe (382G-44K-30)
2008-20-01Lockheed Model 382, 382B, 382E, 382F, and 382G Series AirplanesNov 3, 2008Airframe (382G-44K-30)
2008-14-10Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J Series AirplanesJul 22, 2008Airframe (382G-44K-30)
2006-25-12Rolls-Royce Corporation 501-D Series Turboprop EnginesJan 23, 2007Engine (501-D22A)
2005-22-03Rolls-Royce Corporation (Formerly Allison Engine Company) 501-D22A, 501-D22C, and…Nov 29, 2005Engine (501-D22A)Serial numbers per Table 1 of this AD (turbine wheel serial numbers). Only with: Engines with turbine wheels installed: P/N 6875431 1st stage S/N KK50152-KK50199; P/N 6845592 2nd stage S/N KK40998-KK41057; P/N 6845593 3rd stage S/N KK36452-KK36461 and KK36492-KK36532; P/N 6870434 4th stage S/N KK40320-KK40393 and KK40485-KK40535.
Show all 8 ADs
ADSubjectEffectiveApplies to
2003-14-16Lockheed Model 382G Series AirplanesAug 25, 2003Airframe (382G-44K-30)Serial numbers per Hercules Service Bulletin 382-52-9, dated July 5, 2000
97-21-13Lockheed Model 382 Series AirplanesNov 24, 1997Airframe (382G-44K-30)
97-05-07Lockheed Model 382 Series AirplanesApr 4, 1997Airframe (382G-44K-30)Only with: Equipped with a servo-type valve housing assembly P/N 714325-3 or 714325-7 installed on any outboard engine.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (10)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Propellers · barrel · crackedOct 26, 2017

    DURING A PROPELLER INSTALLATION PROCEDURE, A CRACK WAS NOTICED ON THE FORWARD SURFACE OF THE PROPELLER REAR BARREL HALF ASSEMBLY, WHERE THE PITCH LOCK REGULATOR EXTERNALLY THREADED RING SCREWS INTO THE REAR BARREL. PRIOR TO THE PLACEMENT OF THE PITCH LOCK RATCHET RING, NOTICED A CRACK 3/4 OF AN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · angle · corrodedJul 3, 2012

    S/O 127043 N/R 24763 DURING SCHEDULED INSPECTION, FOUND CARGO DOOR LEFT SIDE BEAM ANGLE HAS CORROSION AT AFT END SURFACE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · angle · corrodedJul 3, 2012

    DURING SCHEDULED INSPECTION, FOUND VERTICAL STABILIZER RIGHT ATTACH ANGLE HAS CORROSION AT MATING SURFACE FS 1041 APPROX, ALSO AT UPPER SURFACE HSS 991.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Stabilizers · attach angle · corrodedJul 3, 2012

    S/O 127043 N/R 24790 DURING SCHEDULED INSPECTION, FOUND VERTICAL STABILIZER LOWER LEFT SIDE FWD ATTACH ANGLE CORRODED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · attach fitting · gougedJul 3, 2012

    S/O 127043 N/R 24791 DURING SCHEDULED INSPECTION, FOUND AFT FUSELAGE LEFT UPPER HORIZONTAL STAB ATTACH FITTING HAS GOUGES AT I/D SURFACE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · nut plate · brokenJul 3, 2012

    DURING SCHEDULED INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER L/E ATTACH SCREW NUT PLATES BROKEN (9 EACH).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · attach angle · corrodedJul 3, 2012

    DURING SCHEDULED INSPECTION, FOUND RIGHT VERTICAL STABILIZER ATTACH ANGLE AT FS 967 AND 991 CORRODED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · diffuser · crackedJul 3, 2012

    S/O 127043 N/R 24783 DURING SCHEDULED INSPECTION, FOUND LEFT HORIZONTAL STABILIZER L/E ANTI-ICE DIFFUSER HAS SEVERAL CRACKS AT HSS 200, HSS 252, HSS 265.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · attach angle · out of limitsJul 3, 2012

    DURING SCHEDULED INSPECTION, FOUND RT VERTICAL STABILIZER ATTACH ANGLE HAS BLEND OUT OF LIMITS AT FS 1098.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · damagedJul 3, 2012

    S/O 127043 N/R 24762 - DURING SCHEDULED INSPECTION, FOUND RUDDER TIP SKIN HAS A LIGHTNING STRIKE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

Request owner name removalReport an error in this record