- Registered owner
- Bedrock LLC
- Location
- Anniston, AL
- Owner type
- LLC
- Serial number
- BB-43
- Year built
- 1975
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- February 11, 1975
- Certificate issued
- January 19, 2025
- Expires
- January 31, 2032
- Mode S code
- A68A04
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 59
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 3 |
| 1979 | 1 |
| 1980 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 4 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 3 |
| 2012 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 61 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N520MCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N520MCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech 200 aircraft
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CIEA201303260004Spar Cap · corrodedHEAVY 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 MASDR 2012FA0000333Downlock Switch · inoperativeFLIGHT DISCREPANCY: RT MLG LIGHT DOES NOT ILLUMINATE WHEN GEAR IS DOWN. LIGHT NOT BURNED OUT. MANUALLY EXTENDED GEAR. EMERGENCY WAS DECLARED TO TOWER. PILOT LANDED AIRPLANE SAFELY WITH NO DAMAGE OR INJURIES. A DEFECTIVE DOWNLOCK SWITCH WAS FOUND AFTER TROUSDR CIEA2011122100001Control Knob · faultyDURING 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. PLACSDR CIEA200700007Bracket · bentDURING 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 REMSDR CIEA200700006Wire · pinchedSHORTLY 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 FSDR CIEA200700001Pressure Panel · crackedDURING 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 NOSDR 0022Switch · crackedLANDING 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 SSDR 99ZZZX126Frame · crackedDURING 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 THSDR 99ZZZX130Fire Detector · malfunctionedAFTER 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 CHESDR 98ZZZX613Rib · crackedDURING AN EVENT 1 INSPECTION, 3 RIBS ON THE LEFT INBOARD WING AT STA 56.00, STA 65.50, AND STA 75.50 AND ONE ON THE RIGHT AT STA 65.50 WERE FOUND CRACKED ON THE FORWARD RIVET WHERE THE STRINGER IS ATTACHED. THE CRACK WENT FROM THE RIVET HOLE FORWARD TO THE EDSDR 98ZZZX612Skin · crackedDURING AN EVENT 1 INSPECTION, A .50 INCH CRACK WAS FOUND IN THE SKIN AFT OF THE RIGHT FUEL FILLER CAP. THE CRACK APPEARS TO BE DUE TO IMPROPER USE OF THE FUEL NOZZLE DURING FUELING. INSTALLATION OF AN INTERNAL DOUBLER WAS REQUIRED.SDR 98ZZZX611Skin · crackedDURING 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 SDR 98ZZZX610Nutplate · crackedDURING 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. CRACKSDR 97ZZZX5116Elevator · damagedAFTER A HANGAR RASH INCIDENT, THE RIGHT ELEVATOR WAS BEING REPAIRED FOR DAMAGE TO THE FIBERGLASS TIP. AFTER REMOVAL OF THE TIP, THREE HOLES IN THE OUTBOARD TRAILING EDGE AREA OF THE SKIN WERE FOUND FILLED WITH BODY FILLER. THE FILLER WAS REMOVED AND AN ALUMISDR 97ZZZX4477Skin · crackedDURING ROUTINE MAINTENANCE, A MECHANIC FOUND TWO SMALL CRACKS PROTRUDING FROM RIVET ON LEFT HAND WING LEADING EDGE SKIN OUTBOARD OF ENGINE NACELLE. INSPECTION OF INNER LEADING EDGE REVEALED CRACKED RIB. AFTER REMOVAL OF LEADING EDGE SKIN, FOUND SMALL ENGINE
STCs that may be installed · 422
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.