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Aircraft record

N3812CBeechcraft 76

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply4 service difficulty reports

Registration
Valid
expires Aug 31, 2029
Based in
Wilmington, DE
owner city / state
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Christiansen Aviation LLC
Owner type
LLC
City, state
Wilmington, DE
Certificate issued
Aug 15, 2022
Expires
Aug 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Mar 5, 1985

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
Beechcraft
Model
76
Serial number
ME-390
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A461A2

Engine

Make and model
Lycoming O&Vo-360 Ser
Type
Reciprocating
Power
180 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. 2022 – nowChristiansen Aviation LLCWilmington, DE · current

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 (2)

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
2021-08-06Textron Aviation Inc. AirplanesMay 25, 2021Airframe (76)Certain serial numbers: 76 ME-1–ME-437. Only with: Excludes airplanes with MLG "A" frame assemblies P/N 105-810023-0083 (left) and P/N 105-810023-0084 (right) installed.
99-05-13Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55…Apr 19, 1999Airframe (76)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798

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

Service Difficulty Reports (4)

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.

  • Air conditioning and pressurization · solenoid · leakingMar 30, 1998

    INTERMITTENT HEATER OPERATION FOUND FUEL SOLENOID LEAKING THROUGH SAME HOLE IN SIDE OF SOLENOID THAT THE WIRING COMES OUT OF. FUEL PUDDLED UP IN DRAIN PAN, THEN DRAINED OVERBOARD. FUEL OVERBOARD DRAIN IS LOCATED DIRECTLY IN FRONT OF EXHAUST.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · prop lever · jammedMar 26, 1998

    LEFT PROPELLER WAS FEATHERED IN-FLIGHT FOR TRAINING. UNABLE TO INITIALLY GET PROPELLER LEVER BACK FORWARD. FINALLY, WHEN LEVER BROKE LOOSE, A LOUD SNAP WAS HEARD. PROPELLER CAME OUT OF FEATHER. LANDING WAS UNEVENTFUL. UPON INVESTIGATION, FOUND BOTH PROP LEVERS COULD RIDE UP AND OVER FEATHER DETENT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedApr 22, 1997

    FORWARD SPAR ATTACH BRACKET AT STA 94.0 LEFT AND RIGHT SIDES. DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT. LEFT FRAME WAS CRACKED .3750 INCH LONG, RT FRAME FOUND CRACKED .0625 INCH LONG. CAUSE: APPEARED TO BE STRESS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Fuselage · frame · crackedApr 22, 1997

    FORWARD SPAR ATTACH BRACKET AT STA 94.0 LEFT AND RIGHT SIDES. DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE LOWER PORTION OF THE UPPER RADIUS FOR THE FORWARD SPAR SLOT CUT-OUT. LEFT FRAME WAS CRACKED .3750 INCH LONG, RT FRAME FOUND CRACKED .0625 INCH LONG. CAUSE: APPEARED TO BE STRESS…

    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

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