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Aircraft record

N520MC1975 Beechcraft 200

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply14 service difficulty reports

Registration
Valid
expires Jan 31, 2032
Based in
Anniston, AL
owner city / state
Engine
PT6A-41 · 850 hp
U/A Canada
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
14
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Bedrock LLC
Owner type
LLC
City, state
Anniston, AL
Certificate issued
Jan 19, 2025
Expires
Jan 31, 2032
Airworthiness
Standard · Normal
Airworthiness date
Feb 11, 1975

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
1975
Serial number
BB-43
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
A68A04

Engine

Make and model
U/A Canada Pt6a-41
Type
Turbo-prop
Power
850 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. 2025 – nowBedrock LLCAnniston, AL · 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 (14)

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.

  • Wings · spar cap · corrodedMar 22, 2013

    HEAVY CORROSION FOUND DURING PHASE INSPECTION ON WING MAIN SPAR LOWER CAP AREA WHERE IT PASSES THROUGH THE LT FUSELAGE PRESSURE VESSEL. CAUSE OF CORROSION WAS DUE TO MOISTURE BEING TRAPPED UNDERNEATH DETERIORATING SEALANT THAT SEALS THE PRESSURE VESSEL. A MAJOR REPAIR RESULTED BY REMOVING ALL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · control knob · faultyDec 21, 2011

    DURING RECEIVING INSP OF O/H PRESSURE CONTROLLER AND BEFORE INSTALLATION, FOUND THE "CAB ALT" KNOB BINDING INTERMITTENTLY AND MAKING A RATCHETING NOISE WHEN ADJUSTED. PART WAS NOT INSTALLED ON ACFT. NOTIFIED THE VENDOR THAT THE PART WAS PURCHASED FROM. PLACED AN ORDER FOR A DIFFERENT CONTROLLER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · bracket · bentAug 28, 2007

    DURING CRUISE FLT, CREW HEARD A NOISE & NOTICED THAT THE LT WING LOCKER HAD COME OPEN AND DOOR WAS TRAILING A FEW INCHES OPEN IN FLIGHT. ACFT APPROXIMATELY 25 MILES FORM A SUITABLE AIRPORT & CREW LANDED WITHOUT FURTHER INCIDENT. BAGGAGE FROM WING LOCKERS REMOVED & PLACED IN BAGGAGE COMPARTMENT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · wire · pinchedAug 25, 2007

    SHORTLY AFTER TAKEOFF THE PASSENGER NOTIFIED THE FLIGHT CREW THAT THEY HAD OBSERVED SMOKE FROM THE AREA OF THE NO SMOKING FASTEN SEAT BELT SIGN. THE FLIGHT CREW THAN OBSERVED THAT THE NO SMOKING FASTEN SEAT BELT SIGN CIRCUIT BREAKER HAD IN FACT POPPED. THE FLIGHT CREW RETURNED TO THE AIRPORT AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · pressure panel · crackedJan 24, 2007

    DURING INSPECTION OF THE AIRCRAFT TO EVALUATE A PRESSURIZATION LEAK, THE PANEL BEHIND THE REAR SPAR WAS FOUND TO BE CRACKED IN THE LOWER RADIUS AREA. THERE WAS A CRACK APPROXIMATELY 4 INCHES LONG NEAR THE CENTER LINE OF THE AIRCRAFT. THE AIRCRAFT SKIN WAS NOT FOUND TO BE CRACKED AT THIS TIME. THIS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · crackedJan 31, 2004

    LANDING GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. LANDING GEAR WAS EXTENDED MANUALLY AND LANDING WAS PERFORMED NORMALLY. AC HAD BEEN IN AND OUT OF COLD AND SNOW ON ITS PREVIOUS FLIGHTS. AC WAS JACKED IN HANGAR AND GEAR WORKED NORMAL. GEAR WAS CYCLED SEVERAL TIMES. SWITCH WHICH DISABLES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedAug 8, 1998

    DURING AN INSPECTION OF THE AIRCRAFT, THE HINGE FOR THE ENTRY DOOR WAS LOOSE. THE HINGE WAS REMOVED AND INSPECTION REVEALED FRAME, P/N 50-430043-328, TO BE CRACKED AT 4 OF THE AFT RIVET HOLES. ALSO NOTED 3 RIVETS ATTACHING THE FRAME, P/N 50-430043-324, TO THE 2 CENTER FRAMES, WERE MISSING CAUSING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · fire detector · malfunctionedJul 27, 1998

    AFTER TAKEOFF, CLIMBING THROUGH 15,000 FEET, THE LEFT FIRE WARNING LIGHT CAME ON. THE PILOT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND NO EVIDENCE OF FIRE WAS FOUND. THE FIRE WARNING WAS CHECKED FOR PROPER OPERATION AND CHECKED GOOD. MAINTENANCE WAS UNABLE TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · nutplate · crackedDec 1, 1997

    DURING AN INSPECTION OF THE AIRCRAFT, THE LEFT LEADING EDGE WING ROOT FAIRING WAS REMOVED TO PERFORM MAINTENANCE. A 2.50 INCH CRACK WAS FOUND FROM ONE OF THE RIVETS WHICH HOLD THE NUTPLATE IN PLACE FOR THE WING ROOT FAIRING IN THE PRESSURE VESSEL AREA. CRACK WAS STOP DRILLED AND A DOUBLER WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedDec 1, 1997

    DURING AN EVENT 1 INSPECTION, CRACKS IN THE WING SKIN IN THE AREA OF THE LEFT AND RIGHT LOWER WING BOLT FITTING WERE FOUND. THESE CRACKS TEND TO GO THROUGH THE HOLES WHERE SCREWS ARE USED TO SECURE THE SKIN TO THE WING SPAR CAP, AND EXTEND TO THE HOLE IN THE SKIN FOR THE FUEL DRAIN. SUBMITTER…

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

Showing the 10 most recent of 14 reports.

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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