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Aircraft record

N636B1978 Beechcraft A200

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply15 service difficulty reports

Registration
Valid
expires Jul 31, 2031
Based in
Brandon, MS
owner city / state
Owners
1
since 2024
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
15
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
David Aviation INC DBA
Owner type
Corporation
City, state
Brandon, MS
Certificate issued
Jul 17, 2024
Expires
Jul 31, 2031
Airworthiness
Standard · Normal
Airworthiness date
May 8, 2000

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
A200
Year
1978
Serial number
BC-61
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
15
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A8541F

Engine

Make and model
P&W Pt6a Ser
Type
Turbo-prop
Power
750 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. 2024 – nowDavid Aviation INC DBABrandon, MS · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (A200)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 (A200)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (A200)
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (A200)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 (15)

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.

  • Navigation · indicator · failedOct 1, 2014

    DURING CLIMB THROUGH 4000 FT, THE CAPTAIN SIDE ATTITUDE INDICATOR FLAGGED "GYRO", THEN STARTED INDICATING A BANK TO THE LEFT. CAPTAIN CALLED THE FAILURE AND POSITIVE EXCHANGE OF CONTROLS OCCURRED BETWEEN PILOT AND CO PILOT. CO PILOTFLEW THE RETURN , INTERCEPTED THE ILS 2 AND SAFELY LANDED THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · flap track · tornDec 12, 2013

    AIRCRAFT WAS CLEARED TO LAND AND ON A CLOSE LT DOWNWIND, CIRCLING AT 140 KNOTS FROM A GPS13 APPROACH, CONFIGURED WITH FLAPS SET AT APPROACH AND GEAR SELECTED DOWN. CAPTAIN`S COMMANDED FULL FLAPS. WHEN THEY WERE SELECTED THE FLAPS EXTENDED ONLY TO APPROXIMATELY 80 PERCENT, THEN STOPPED. NO CIRCUIT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · fire detector · failedJul 13, 2012

    ON SHORT FINAL APPROACH, THE LT ENGINE FIRE DETECTOR T HANDLE LIGHT ILLUMINATED. PILOT MADE NORMAL LANDING AND NO SMOKE WAS NOTICED, PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE WAS NOTICED, PERFORMED OPS CHECK WITH COCKPIT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fire protection · fire detector · failedJul 13, 2012

    ON SHORT FINAL APPROACH THE LEFT ENGINE FIRE DETECTOR T-HANDLE LIGHT ILLUMINATED. PILOT MADE A NORMAL LANDING AND NO SMOKE WAS NOTICED. PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE WAS NOTICED, PERFORMED OPS CHECK WITH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · flow valve · failedApr 3, 2009

    DURING CLIMB TO ALTITUDE CABIN FAILED TO MAKE MAXIMUM DIFFERENTIAL PRESSURE AND HAD A HIGHER THAN NORMAL CABIN. FOUND A P3 AIR TUBE DISSCONNECTED AT RT HEAT EXCHANGER IN RT WING. ON MX FLIGHT FOUND LT FLOW CONTROL VALVE WEAK. REPLACED DUCT AND FLOW CONTROL VALVE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · bellcrank · twistedMay 5, 2008

    DRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEGREES FROM WHAT A NEW ONE IS.. ALSO THE BOLT PN NAS110321D THAT THE UPLOCK BRACKET PIVOTS ON WAS DEFORMED SLIGHTLY. THIS WAS PROBABLY CAUSED BY THE UPLOCK HOOK BEING MISRIGGED.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · actuator · inoperativeNov 25, 2007

    DESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL EXTENSION HANDLE. REPLACED RT ICE VANE ACTUATOR MOTOR. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · failedNov 25, 2007

    AWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WAS DETERMINED THAT THE POWER SUPPLY (BALLAST) HAD FAILED AND CAUSED THE SMOKE. POWER SUPPLY WAS RELACED AND LIGHTS OPERATED NORMAL. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · sensor · faultyAug 7, 2007

    AT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED. ALL ENGINE GAUGES INDICATED NORMALLY. ALREADY IN DESCENT, THROUGH 4,500 FT, AND CONTINUED TO A SAFE LANDING. MAINTENANCE DISCOVERED FAULTY LOWER AFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · windshield · failedMar 6, 2007

    WHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDING WERE MADE AT KLEB. THERE WAS NO LOSS OF CABIN PRESSURE. LAST INSPECTION WAS 3 MONTH AND 100 HOURS PRIOR TO THE INCIDENT. (K)

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

Showing the 10 most recent of 15 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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