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Aircraft record

N430MC1981 Beechcraft 200

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply4 service difficulty reports

Registration
Valid
expires Oct 31, 2027
Based in
Fullerton, CA
owner city / state
Engine
PT6A SERIES · 715 hp
U/A Canada
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Fullerton, CA
Certificate issued
Oct 5, 2020
Expires
Oct 31, 2027
Airworthiness
Standard · Normal
Airworthiness date
Jul 23, 1981

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
200
Year
1981
Serial number
BB-904
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
11
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A52434

Engine

Make and model
U/A Canada Pt6a Series
Type
Turbo-prop
Power
715 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. 2020 – nowIndividual ownerFullerton, CA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (4)

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
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (200)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; …
98-20-38Raytheon Aircraft Company 200 Series AirplanesSep 29, 1998Airframe (200)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (200)
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (200)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; …

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.

  • Engine fuel and control · bearing · damagedOct 12, 2009

    PILOT REPORTED THAT THE LT ENGINE WOULD SURGE MODERATELY WHEN CLIMBING OR DESCENDING THROUGH 4000-8000 FT. NO SURGING WAS REPORTED ABOVE OR BELOW THAT ALTITUDE RANGE. WHEN SURGING OCCURRED, OSCILLATION WAS NOTED ON THE FUEL FLOW GAUGE AND ON THE PROP TORQUE GAUGE. FUEL FLOW WOULD OSCILLATE +/-25…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · p3 air line · failedDec 13, 1999

    DURING GROUND RUN-UP, THE LEFT ENGINE WOULD ONLY DEVELOP 89 PERCENT N1 (COMPRESSOR RPM). INSPECTION OF THE FUEL CONTROL P3 AIR LINES REVEALED A LOOSE B-NUT AT THE PROP GOVERNOR. LEAKAGE IN THIS LINE LIMITS THE FUEL CONTROL TO 80 PERCENT (MAXIMUM REVERSE N1). THE SAFETY WIRE FOR THE B-NUT HAD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · exciter box · failedNov 24, 1999

    DURING ROUTINE START-UP, THE LEFT ENGINE FAILED TO LIGHT OFF. THE IGNITION SYSTEM WAS IMMEDIATELY SUSPECT DUE TO LACK OF 'POPPING' THAT ACCOMPANIES THE FIRING OF THE IGNITERS. THE EXCITER BOX WAS REPLACED AND THE ENGINE STARTED NORMALLY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Engine fuel and control · fuel pump · failedApr 28, 1998

    DURING CRUISE FLIGHT, THE RT ENGINE FLAMED OUT AND WOULD NOT RESTART IN-FLIGHT. AFTER A SAFE LANDING, THE ENGINE STARTED NORMALLY. HOWEVER, WHEN POWERED UP TO 100 PERCENT, THE ENGINE WOULD IMMEDIATELY FLAME OUT. INSPECTION REVEALED THE HIGH PRESSURE, ENGINE-DRIVEN FUEL PUMP WAS AT FAULT. THE…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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