Beech B200C

Service difficulty reports · 169

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'B200C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA970319002Actuator · failed(CAN) THE PILOT SELECTED GEAR UP. THE NOSE GEAR UNLOCKED BUT DID NOT GO UP. THE MAINS REMAINED DOWN AND LOCKED. THIS AIRCRAFT HAD THE AVIA DESIGN LANDING GEAR STC SA4378WP ALTHOUGH THE MOTOR IS AN ORIGINAL BEECH PART NUMBER.Mar 7, 1997 · Beech B200C · Landing Gear ActuatorSDR AU970198Flap · damaged(AUS) LH OUTBOARD WING FLAP DAMAGED - SPAR BENT AND SKIN CREASED -INVESTIGATION FOUND A DEAD HARE ON THE RUNWAYFeb 26, 1997 · Beech B200C · Trailing Edge FlapsSDR CA970228007Hp Bleed Valve · faulty(CAN) ON DESCENT THERE WERE TWO LOUD BANGS FROM #1 ENGINE AND A FLASH OF FLAME FROM THE ENGINE EXHAUST DUCT. AFTER FIVE SECONDS THIS EVENT REPEATED ITSELF. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS CARRIED OUT. POST FLIGHT INVESTIGATION FOUND THEFeb 19, 1997 · Beech B200C · Compressor Bleed ValveSDR AU970128Windshield · cracked(AUS) CO-PILOTS WINDSHIELD OUTER LAMINATION CRACKED IN TOP RH CORNER -WINDSHIELD WAS DELAMINATING PRIOR TO CRACKING (THE DELAMINATION WAS WITHIN MANUFACTURERS LIMITS)Feb 5, 1997 · Beech B200C · Flight Compartment WindowsSDR AU970122Brake Disc · failed(AUS) RH OUTBOARD BRAKE DISC BROKEN - BROKEN PIECE OF DISC DAMAGED WHEEL ASSEMBLY AND BRAKE BACKPLATE - WHEEL JAMMEDJan 28, 1997 · Beech B200C · BrakeSDR AU970121Brake Disc · failed(AUS) LH OUTBOARD BRAKE ROTATING DISC BROKEN - ONE SEGMENT CRACKED AND FELL OUT CAUSING MINOR DAMAGE TO WHEELJan 17, 1997 · Beech B200C · BrakeSDR CA970110004Lighting Panel · shorted(CAN) WHILE IN CRUISE FLIGHT SMOKE WAS NOTED COMING FROM THE RIGHT HAND SAT/COMM AUDIO PANEL LOCATED IN THE CABIN. CIRCUIT BREAKERS PULLED AND THE PANEL WAS REPLACED AFTER A SAFE LANDING.Dec 31, 1996 · Beech B200C · Audio Integrating SystemSDR CA961223006Engine · making metal(CAN) DURING FLIGHT #2 ENGINE CHIP DETECTOR ILLUMINATED. ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE WAS REMOVED FOR INVESTIGATION. REPORT TO FOLLOW.Dec 16, 1996 · Beech B200C · Engine (Turbine/Turboprop)SDR CA961218005Switch · failed(CAN) THIS AIRCRAFT'S ELECTRICAL LANDING GEAR SYSTEM HAD BEEN REPLACED WITH A HYDRAULIC SYSTEM. THE NOSE GEAR GREEN LIGHT DID NOT COME ON WHEN THE GEAR WAS DOWN AND LOCKED. THUS, THE PILOT HAD TO DO SEVERAL GEAR CYCLES AND A FLY-BY. HE LANDED OK. THE NOSE Nov 26, 1996 · Beech B200C · Landing Gear Position and WarningSDR AU961168Compressor Blade · fod(AUS) RH ENGINE COMPRESSOR FIRST STAGE BLADES DAMAGED BY FOD - AIRCRAFTHAD PREVIOUSLY OPERATED FROM GRAVEL STRIPSAug 13, 1996 · Beech B200C · Turbine Engine Compressor SectionSDR AU961151Pipe · chafed(AUS) RH MAIN LANDING GEAR TORQUE TUBE PNO 101-810021-3 RUBBING ON INCORRECTLY POSITIONED FUEL LINE BETWEEN THE NACELLE TANK AND THE AUXILIARY TANK WEARING A HOLE IN THE FUEL LINE AND DAMAGING THE TORQUE TUBE - FUEL LEAKING - PERSONNEL/MAINTENANCE ERRORJul 31, 1996 · Beech B200C · Aircraft Fuel Distribution SystemSDR AU960625Switch · failed(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH INTERNAL FAILUREMay 2, 1996 · Beech B200C · Landing Gear Position and WarningSDR AU960312Circuit Board · faulty(AUS) BATTERY CHARGE SYSTEM PRINTED WIRING BOARD FAULTYMar 10, 1996 · Beech B200C · Battery/Charger SystemSDR AU960271Pipe · worn(AUS) MAIN FUEL PIPE CHAFING ON STRUCTURE IN AREA BETWEEN MAIN LANDING GEAR BAY AND WING FUEL TANK - FUEL PIPE ON VH-AMM IN SIMILAR CONDITIONMar 5, 1996 · Beech B200C · Aircraft Fuel Distribution SystemSDR 97ZZZX1014Control Rod · hung upLEFT ENGINE CRUISE POWER REMAINED STEADY AFTER PILOT PULLED BACK POWER LEVER TO BEGIN DESCENT. ENGINE REACHED HIGH TORQUE LIMIT AND HAD TO BE SHUT DOWN IN-FLIGHT. MAINTENANCE INSPECTED ENGINE AND FOUND THE COTTER PIN ON THE CASTELLATED NUT RETAINING THE FCU Feb 29, 1996 · N107Z · Beech B200C · Fuel Control/Reciprocating EnginesSDR AU960144Diode · faulty(AUS) NO1 ELECTRICAL BUS FEEDER DIODE FAULTYFeb 7, 1996 · Beech B200C · DC Power Distribution SystemSDR CA960123011Connector · crimp failed(CAN)DURING TROUBLESHOOTING OF THE PROPELLER SYNCHROPHASER SYSTEM, WIRES WERE FOUND PULLED OUT OF THE SYNCHROPHASER BOX CONNECTOR. WHEN THE SOCKETS WERE EXTRACTED FROM THE BOX THEY COULD BE SEEN TO BE IMPROPERLY CRIMPED. THERE WAS ALSO NO STRAIN RELIEF BACKSHEJan 5, 1996 · Beech B200C · Propeller Synchronizer SectionSDR CA951221029Fuel Strainer · corroded(CAN)DURING MAINTENANCE A LEAKING FUEL STRAINER WAS INSPECTED AND FOUND TO BE CORRODED ABOUT 3/4 OF THE WAY THROUGH THE FLANGE WHICH IN TURN CAUSED THE LEAK. THE FUEL STRAINER WAS REPLACED.Dec 14, 1995 · Beech B200C · Aircraft Fuel Filter/StrainerSDR ERA00020Airstair Door · out of adjustMRI - AIRSTAIR DOOR OPENED AT ROTATION. RETURNED TO MRI AND MADE UNEVENTFUL LANDING. INSPECTED AIRSTAIR DOOR RIGGING AND STRUCTURE, NO DEFECTS NOTED. TESTED DOOR WARNING SYSTEM FOR PROPER OPERATION IAW MM 52-71-00. ADJUSTED AIRSTAIR DOOR HANDLE SWITCH SLIGNov 26, 1995 · N143LG · Beech B200C · Passenger/Crew Doors
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