Beechcraft B200C

Service difficulty reports · 169

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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 AUS20040176Check Valve · faulty(AUS) FUEL SYSTEM CHECK VALVE SUSPECT FAULTY.Mar 7, 2004 · Beech B200C · Aircraft Fuel Distribution SystemSDR AUS20040151Engine · fluctuates(AUS) LT ENGINE FUEL FLOW AND ENGINE TORQUE FLUCTUATING BEFORE ENGINE STARTED TO ROLLBACK. INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. THE ENGINE WAS GROUND RUN AND THEN TEST FLOWN WITH NO FURTHER REOCCURRENCE.Mar 1, 2004 · Beech B200C · Engine (Turbine/Turboprop)SDR AUS20040115Frame · cracked(AUS) FUSELAGE FRAMES (3OFF) LOCATED AT STN 285.188, STN 278.5 AND STN291.875 CRACKED. FRAME PART NUMBERS PN 101-440091-33, PN 101-440090-27 AND PN 101-440092-31. FOUND DURING INSPECTION IAW AD.Feb 18, 2004 · Beech B200C · Fuselage Main, FrameSDR CA040203006Windshield · broken(CAN) IN CRUISE RT WINDSHIELD HEAT ON, WINDOW SHATTERED, DESCENDED TO 12,000 FT, REDUCED AIR SPEED AND CABIN PRESSURE AND RETURNED TO BASE.Jan 8, 2004 · Beech B200C · Flight Compartment WindowsSDR CA031117014Cable · frayed(CAN) DURING INSPECTION OF CABIN DOOR CAM LOCK LATCHES, THE DOOR LATCHING CABLE WAS FOUND TO HAVE HALF TO THREE QUARTERS OF THE CABLE STRANDS BROKEN. IF THIS CABLE WOULD HAVE BROKEN COMPLETELY IT COULD HAVE CAUSED ONE COMPLETE SIDE OF DOOR TO BECOME UNLATCHEDNov 13, 2003 · Beech B200C · Entrance StairsSDR EHA2004F00005Relay · stuckRT WINDSCREN SHATTERED AT FL250. NO LOSS OF CABIN PRESSURE OCCURED. LANDED SAFELY WITHOUT INCIDENT. UPDATE TO PREVIOUS SDR DATED 11/11/03. UPON DISASSEMBLY AND TESTING, IT WAS DETERMINED THAT THE CAUSE OF THE INCIDENT WAS THE WINDSHIELD HEAT RELAY.Nov 12, 2003 · N134WJ · Beech B200C · Windshield/Door Rain/Ice RemovalSDR CA030925005Pad · loose(CAN) DURING LANDING THE AIRCRAFT WAS PULLING TO THE LEFT SIDE OF THE RUNWAY. UPON APPLICATION OF THE BRAKE ON THE LEFT SIDE AIRCRAFT STARED TO VIBRATE. THE BRAKE WAS ALSO NOTED TO BE SOFT AND INEFFECTIVE. MAINTENANCE INSPECTED IT AND FOUND THE LT OUTBOARD Sep 16, 2003 · Beech B200C · Landing Gear Brake SystemSDR AUS20030943Windshield · failed(AUS) RT WINDSHIELD INNER PANE SHATTERED.Aug 30, 2003 · Beech B200C · Flight Compartment WindowsSDR AUS20030732Inverter · burned(AUS) 240 VAC INVERTER BURNED.Jul 17, 2003 · Beech B200C · AC InverterSDR CA030609004Pressure Switch · failed(CAN) AIRCRAFT FLEW UNEVENTFUL. UPON TAKEOFF, THE CREW SELECTED GEAR UP. THE NOSE AND RT MAIN GEAR BEGAN TO RETRACT. THE LT MAIN GEAR REMAINED DOWN AND LOCKED. CREW SELECTED GEAR DOWN AND RETURNED TO 3 GREEN. ONCE AGAIN, CREW SELECTED GEAR UP. GEAR DID NOT MMay 28, 2003 · Beech B200C · Hydraulic System, MainSDR AUS20030460Bolt · sheared(AUS) NOSE LANDING GEAR UPPER DRAG BRACE BENT AND FORK END OF NOSELANDING GEAR ACTUATOR SPREAD. FURTHER INVESTIGATION ALSO FOUND THE ACTUATOR UPPER SUPPORT BEARINGS ROUGH AND UNSERVICEABLE. SUSPECT CAUSED BY SHEARING OF THE CLEVIS BOLT WHICH ALLOWED THE ACTUAApr 27, 2003 · Beech B200C · Landing Gear Retraction/Extension SystemSDR AUS20030431Insulator · failed(AUS) WIRE SEPARATED FROM AIRCRAFT AT FEED THROUGH INSULATOR. LONG WIRE IS USED FOR MILITARY OPERATIONS.Apr 19, 2003 · Beech B200C · Communications System WiringSDR CA030417010Bearing · failed(CAN) DURING DESCENT THE CREW NOTICED AN ELECTRICAL SMOKE ODOR IN THE CABIN WITH NO VISIBLE SIGNS OF SMOKE, THE CREW ACTIONED THE EMERGENCY CHECKLIST AND LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE FORWARD BLOWER ASSEMBLY WAS A LITTLE NOISApr 7, 2003 · Beech B200C · Air Distribution FanSDR AUS20030319Hub · cracked(AUS) PROPELLER HUB CONTAINED A RADIAL CRACK IN THE OUTBOARD END OF THE NR 1 HUB ARM AT THE HUB/PILOT TUBE JOINT. CRACK WAS CONFIRMEDUSING MAGNETIC PARTICLE INSPECTION (MPI). CRACK LENGTH APPROXIMATELY 25.4MM (1IN). FOUND DURING DISASSEMBLY AND INSPECTION FOLLMar 1, 2003 · Beech B200C · Propeller Hub SectionSDR CA030218001Spar Cap · corroded(CAN) CORROSION ON UPPER RIGHT AND LEFT FORWARD WING SPAR CAPS BETWEEN WS 223 & 236 AND WS 122 & 132. CORROSION IS BEYOND LIMITS, WINGS TO BE REMOVED AND SPARS TO BE REPLACED AS DIRECTED BY BEECHCRAFT ENGINEERING.Feb 3, 2003 · Beech B200C · Wing SparSDR CA030107014Actuator · noisy(CAN) AFTER HAVING PROBLEMS WITH A LOW TIME ACTUATORS ON TWO OTHER AIRCRAFT, WE DECIDED TO CHECK ALL ACTUATOR THAT WERE OVERHAULED BY THAT SUPPLIER.DURING SPECIAL INSPECTION OF THIS ACTUATOR, WE FOUND THAT THE LANDING GEAR ACTUATOR WAS SQUEALING DURING GEAR EXDec 20, 2002 · Beech B200C · Landing Gear ActuatorSDR AUS20021272Bolt · separated(AUS) LT MAIN LANDING GEAR OLEO STRUT PISTON SEPARATING FROM AXLE. SHEAR BOLT HAD SHEARED AND THE PISTON HAD MIGRATED OUT BY APPROXIMATELY 25MM (0.98IN).Oct 30, 2002 · Beech B200C · Main Landing Gear Strut/Axle/TruckSDR AUS20021234Torque Tube · faulty(AUS) RUDDER TORQUE TUBE RIVETS LOOSE AND RIVET HOLES WORN BY UP TO APPROXIMATELY 0.254MM (0.010IN) OVERSIZE.Oct 25, 2002 · Beech B200C · Rudder StructureSDR BN001Strap · crackedUPON REMOVAL OF AIRCRAFT INTERIOR TO TROUBLESHOOT WIRING PROBLEMS, TWO STRAP ASSEMBLIES ON THE RT SIDE OF THE FUSELAGE AT F.S. 227.0 AND 246.0, BUTTOCK LINE 119.0 WERE FOUND COMPLETELY CRACKED THROUGH. THE STRAP ASSEMBLY AT F.S. 246.0. THESE AREAS WOULD NOTOct 17, 2002 · N7232R · Beech B200C · Fuselage Main, FrameSDR AUS20021078Engine · seized(AUS) RT ENGINE SUFFERED AN IN FLIGHT FAILURE WITH THE ENGINE SEIZING. INSPECTION FOUND A CRACK IN THE COMPRESSOR SECTION INTAKE HOUSING WITH OIL POOLING IN THE EXHAUST SECTION. CRACK LENGTH 50.8MM TO 63.5MM (2IN TO 2.5IN).Sep 26, 2002 · Beech B200C · Engine (Turbine/Turboprop)SDR CA020821002Isolation Mount · debonded(CAN) DURING A ROUTINE INSPECTION OF THE RT ENGINE. THE UPPER INBOARD VIBRATION ISOLATOR ENGINE MOUNT WAS FOUND TO BE DEBONDED, THE BACK HALF OF THE RUBBER WAS DEBONDED FROM THE METAL FACE PLATE. THE MOUNT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Aug 21, 2002 · Beech B200C · Engine Mount SectionSDR AUS20020894Bulb · burned out(AUS) LANDING GEAR INDICATOR GLOBES (4OFF) UNSERVICEABLE.Aug 12, 2002 · Beech B200C · Landing Gear Position and WarningSDR AUS20020699Flow Divider · faulty(AUS) ENGINE FUEL SYSTEM FLOW DIVIDER FAULTY. IGNITION LEAD ALSO FOUNDTO BE UNSERVICEABLE. ENGINE WAS UNDERGOING GROUND RUNS FOLLOWINGENGINE INSTALLATION. PERSONNEL/MAINTENANCE ERROR.Jul 11, 2002 · Beech B200C · Fuel DividerSDR AUS20020670Stud · fractured(AUS) AILERON CONTROL SYSTEM STUD FRACTURED. CLAMP PNO AN737TW56-66 LOOSE AT BOTTOM OF CONTROL COLUMN ALLOWING THE CONTROL COLUMN BOOT PNO 101-54149-37 TO MOVE UNSECURED AROUND THE CONTROLCOLUMN. LH AILERON CONTROL CABLE TURNBUCKLE LOCKWIRE CAUGHT ONBRACKET PNJul 9, 2002 · Beech B200C · Control Column SectionSDR AUS20020861Bulkhead · cracked(AUS) LOWER REAR PRESSURE BULKHEAD CRACKED. CRACK IS LOCATED IN THE AREA ONE ROW OF RIVETS DOWN FROM THE LAP JOINT AND DIRECTLY ABOVE THE OUTFLOW VALVE. CRACKING IS SIMILAR TO THAT DESCRIBED IN AD/B200/67 BUT WAS NOT FOUND DURING THE AD CHECK. THE AIRCRAFT HASJun 24, 2002 · Beech B200C · Fuselage Main, BulkheadSDR AUS20020647Lap Joint · scratched(AUS) BULKHEAD LAP JOINT SCRATCHED.May 21, 2002 · Beech B200C · Fuselage Main, BulkheadSDR AUS20020265Wire · broken(AUS) LANDING GEAR POSITION SYSTEM WIRE BROKEN. WIRE WAS LOCATED IN THE WIRING LOOM IN THE UNDERCARRIAGE BAY.Mar 13, 2002 · Beech B200C · Landing Gear System WiringSDR AUS20020091Stringer · cracked(AUS) STRINGER NR 9 LT LOCATED BEHIND FRONT PRESSURE BULKHEAD CRACKED AT THE END OF THE ATTACHMENT GUSSETT.Feb 3, 2002 · Beech B200C · Fuselage Main, Longeron/StringerSDR AUS20020083Blade · cracked(AUS) LT PROPELLER NR 2 BLADE CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.57IN) RUNNING CHORDWISE ACROSS THE BLADE FROM THE TRAILING EDGE. CRACK IS LOCATED APPROXIMATELY 150MM (5.9IN) FROM THE BLADE TIP.Feb 1, 2002 · Beech B200C · Propeller Blade SectionSDR AUS20020098Ignition Lead · mismanufactured(AUS) ENGINE IGNITER LEADS CAUSING IGNITER PIN EROSION. LEADS ARE A NEW ITEM WITH SHORTER INSULATORS.Jan 22, 2002 · Beech B200C · Ignition Harness (Distribution)SDR AUS20020028Door · separated(AUS) RT MAIN LANDING GEAR DOOR SEPARATED FROM AIRCRAFT DUE TO FAILURE OF THE HINGE PIN.Jan 14, 2002 · Beech B200C · Landing Gear DoorsSDR AUS20011340Diode · failed(AUS) NR 2 BUS SYSTEM FEED DIODES FAILED.Dec 11, 2001 · Beech B200C · AC Power Distribution SystemSDR AUS20011320Ignition Lead · shorted(AUS) IGNITER LEAD INSULATION SHORT.Dec 9, 2001 · Beech B200C · Ignition Harness (Distribution)SDR AUS20011226Engine · malfunctioned(AUS) NEWLY INSTALLED ENGINE FAILED TO CORRECTLY CONTROL PROPELLER.Nov 13, 2001 · Beech B200C · Engine (Turbine/Turboprop)SDR AUS20011112Compressor · fod(AUS) ENGINE FIRST STAGE COMPRESSOR DAMAGE. FOD.Oct 19, 2001 · Beech B200C · Turbine Engine Compressor SectionSDR AUS20010972Gearbox · disconnected(AUS) ENGINE ACCESSORY GEARBOX DECOUPLED PREVENTING ACCESSORIES FROM OPERATING.Aug 29, 2001 · Beech B200C · Turbine Engine Accessory DriveSDR AUS20010944Circuit Breaker · faulty(AUS) LANDING GEAR INDICATION SYSTEM CIRCUIT BREAKER HAD HIGH RESISTANCE.Aug 24, 2001 · Beech B200C · Landing Gear Position and WarningSDR AUS20010955Detector · unserviceable(AUS) FIRE DETECTOR FAULTY.Aug 23, 2001 · Beech B200C · Fire DetectionSDR CA010523014Connector · damaged(CAN) AFTER TAKEOFF FLT CREW REPORTED THEY WERE UNABLE TO GET L/G TO RETRACT FULLY, OR EXTEND TO DOWN POSITION. ALL C/BS WERE CHECKED TO NO AVAIL. THE GEAR WAS EXTENDED BY USING THE EMERGENCY BLOW DOWN PROCEDURE. THREE GREEN INDICATORS WERE ATTAINED AND VISUALApr 28, 2001 · Beech B200C · Landing Gear Retraction/Extension SystemSDR CA010406009Downlock Switch · intermittent(CAN) ON FINAL APPROACH WHEN GEAR WAS SELECTED DOWN, RT GEAR LIGHT WOULD NOT COME ON. GEAR WAS SELECTED SEVERAL TIMES WITH SOME RESULT. GO AROUND WAS UNDERTAKEN. RT GEAR WAS VISUALLY CHECKED IN THE DOWN POSITION AND ON THE NEXT APPROACH AIRCRAFT LANDED WITHOUTMar 21, 2001 · Beech B200C · Landing Gear Position and WarningSDR AU001263Regulator · leaking(AUS) PRESSURE REGULATOR LEAKING P3 AIR INTO CABIN. INTERNAL INSPECTION FOUND ALL SEALS WORN AND THE REGULATOR WORN AND LEAKING.Dec 2, 2000 · Beech B200C · Pressure Regulator/Outflow ValveSDR AU001138Cover · separated(AUS) STARTER COVER CAME OFF AND JAMMED BETWEEN THE COWL AND THE ENGINE FCU CONTROL ROD.Nov 30, 2000 · Beech B200C · Starter-GeneratorSDR AU001132Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/200/67.Nov 25, 2000 · Beech B200C · Fuselage Main, BulkheadSDR 2001F00087Bracket · crackedCRACK WAS DISCOVERED DURING ROUTINE MAINTENANCE. THIS IS THE SECOND BRACKET REPLACED IN THE LAS 400 FLIGHT HOURS, IN BOTH INSTANCES THE CRACK WAS LOCATED AT THE LOWER LEFT CORNER. (M)Oct 30, 2000 · N7232R · Beech B200C · Fuselage Miscellaneous StructureSDR AU001024Switch · stuck(AUS) FLAP WARNING SYSTEM MICROSWITCH STUCK. (X)Oct 25, 2000 · Beech B200C · Trailing Flap Position Indicating SystemSDR AU001036Stringer · cracked(AUS) STRINGER NR 10 RT LOCATED AT FRAME 207 CRACKED. NEW FRAME 207 AND SKIN HAD BEEN FITTED. (X)Oct 24, 2000 · Beech B200C · Fuselage Main, Longeron/StringerSDR AU001058Valve · faulty(AUS) RIGHT FLOW PACK PN 101-380013-19 FAULTY AND LT PNEUMOSTAT PN 101-380013-3 STICKING. (X)Oct 19, 2000 · Beech B200C · Cabin Pressure Control SystemSDR AU001003Valve · faulty(AUS) CABIN PRESSURIZATION SYSTEM FAULTY RESULTING IN AUTO DEPLOYMENT OF THE OXYGEN MASKS. INVESTIGATION FOUND THE RIGHT FLOW PACK PN 101-380013-19 UNSERVICEABLE AND THE LEFT PNEUMOSTAT PN 101-380013-3 STICKING. (X)Oct 19, 2000 · Beech B200C · Cabin Pressure Control SystemSDR AU000895Switch · misinstalled(AUS) CABIN ALTITUDE SENSE SWITCH INCORRECTLY WIRED. CABIN OXYGEN MASKS FAILED TO CORRECTLY DEPLOY. (X)Sep 17, 2000 · Beech B200C · Passenger Oxygen SystemSDR AU000966Pressure Switch · faulty(AUS) HYDRAULIC PRESSURE SWITCH FAULTY. (X)Sep 5, 2000 · Beech B200C · Hydraulic Pressure Sensor
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