Beech B200

Service difficulty reports · 830

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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 = 'B200'
  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 2005FA0001409Torque Tube · failedFOUND LT ELEVATOR TORQUE TUBE MOUNTING FLANGE FROM TUBE ASSY TO ELEVATOR RIVETS WORKING LOOSE, ALLOWING THE LT ELEVATOR TO HAVE 1.5 INCHES OF PLAY. THIS WAS FOUND DURING A 400 HOUR LUBRICATION AND INSPECTION. RECOMMENDATION TO PREVENT RECURRENCE, USE SOLID ROct 5, 2005 · N6182A · Beech B200 · Elevator StructureSDR CA051003007Motor · failed(CAN) UPON SELECTION OF GEAR DOWN, PILOT NOTICED THAT GEAR WOULD NOT EXTEND AND THAT THE CIRCUIT BREAKER HAD POPPED. HE RESET IT AND SELECTED GEAR DOWN AGAIN WITHOUT ANY SUCCESS. PILOT USED EMERGENCY EXTENSION AND LANDED WITHOUT INCIDENT. UPON INSPECTION OF LASep 13, 2005 · Beech B200 · Landing Gear Retraction/Extension SystemSDR CA050912006Pressure Valve · worn(CAN) REMOVED LT PNEUMATIC CHECK VALVE TO INSPECT INTERNAL HINGE OPERATIONS. FOUND HINGE PIN DISLODGED (WORKED) TO ONE SIDE, RESULTING IN OFFSET FLAPPER DOOR MOVEMENT, WEAR AND POOR OPERATION. A LONGER HINGE PIN OR STAKING THE ORIGINAL PIN MAY PREVENT THIS TYPSep 8, 2005 · Beech B200 · Pressure Regulator/Outflow ValveSDR CA060317005Circuit Board · cracked(CAN) STATIC INVERTER BOARD CRACKED AND MOISTURE SHORTED BOARD. (TC NR 20060317005)Sep 7, 2005 · Beech B200 · AC InverterSDR AKG2005F00000Bearing · failedBEARING ON WHEEL FAILED. THE BEARING WAS LOCATED ON THE LT MAIN LANDING GEAR ON THE IB WHEEL. THIS BEARING FAILURE SUBSEQUENTLY CAUSED THE WHEEL TO DEPART THE AIRFRAME. IT IS SUSPECTED THAT THE EVENT OCCURED ON LANDING. (K)Sep 6, 2005 · N89WA · Beech B200 · Wheel/Ski/FloatSDR CA050810002Heater · failed(CAN) PILOT REPORTED RT ENGINE HAD NO ACCELERATION RATE AS COMPARED TO LT ENGINE. THE RT ENGINE DID EVENTUALLY ACCELERATE, BUT NOT EQUAL WITH THE LT. TROUBLESHOT AND FOUND RT OIL-TO-FUEL HEATER THERMOSTAT GONE TO (FULL HOT) AND FUEL TEMP WAS SAME AS OIL TEMPAug 8, 2005 · Beech B200 · Fuel HeaterSDR CIEA200500013Downlock Switch · failedDURING APPROACH, RT MAIN GEAR DID NOT INDICATE IT WAS DOWN AND LOCKED. DUE TO SERV AT DESTINATION AIRPORT, A/C RETURNED TO ORIG AIRPORT. PILOT CYCLED GEAR SEVERAL TIMES, UNABLE TO GET A DOWN AND LOCK IND ON RT MAIN GEAR. PILOT DID A MANUAL EXTENSION OF GEARAug 3, 2005 · N203LG · Beech B200 · Landing Gear Position and WarningSDR CIEA200500008Hinge · crackedAFT LANDING ATTEMPTED TO CLOSE MAIN CABIN ENTRY DOOR & HAD DIFFICULTY. A 5 INCH CRACK NEAR AFT, BOTTOM END OF DOOR, WHERE HINGE IS ATTACHED. DAMAGED - ENTRY DOOR HINGE HALF FOUND 8 INCH CRACK RESULTING IN CRACK GOING THRU 8 RIVETS AFT OF DOOR FWD. DOOR CHANJul 1, 2005 · N203LG · Beech B200 · Fuselage, Door HingeSDR CIEA200500007Oxygen Mask · mismanufacturedDURING THE CLIMB THE CABIN LOST PRESSURIZATION. (NOTE: SEE SEPARATE SDR ON THE PRESSURIZATION ISSUE). AS A RESULT OF THE PRESSURIZATION LOSS THE OXYGEN MASKS DROPPED. ONE OF THE PASSENGERS HAD AN ALLERGIC REACTION SIMILAR TO A LATEX ALLERGIC REACTION. IF THJun 28, 2005 · N203LG · Beech B200 · Passenger Oxygen SystemSDR CIEA200500006Door Seal · inoperativeDURING CLIMB, PAX HEARD WIND NOISE FROM AFT CABIN. BROUGHT TO ATTENTION OF PILOT, NOTICED CABIN PRESSURIZATION WAS DROPPING, RESULTING IN CABIN ALTITUDE CLIMBING. PILOT ATTEMPTED TO ADJUST PRESSURIZATION CONTROLLER, CABIN LOST PRESSURIZATION. OXYGEN MASKS DJun 28, 2005 · N203LG · Beech B200 · Passenger/Crew DoorsSDR CIEA200500005Strut · corrodedDURING SCHEDULED LG INSP, NLG UPPER STRUT HSG WAS FOUND TO BE CORRODED. CORROSION WAS IN 2 AREAS OF STRUT, NEAR TOP CROSS BRACE. CORROSION IN EXCESS OF 70 PERCENT AROUND STRUT. IT WAS IN SHAPE OF VALLEY, MORE THAN 50 PERCENT OF CORROSION WAS MORE THAN 50 PEJun 21, 2005 · N203LG · Beech B200 · Nose/Tail Landing Gear Strut/AxleSDR CA050621019Windshield · delaminatedDELAMINATION AT WINDSHIELD.Jun 15, 2005 · Beech B200 · Flight Compartment WindowsSDR CIEA200500002Connector · bentSHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BMay 12, 2005 · N5ST · Beech B200 · Light System WiringSDR CIEA200500001Connector · bentSHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BMay 12, 2005 · N5ST · Beech B200 · Light System WiringSDR 2005FA0000789Rivet · missingDURING VISUAL INSPECTION OF AFT FUSELAGE STRINGERS AT AFT PRESSURE BULKHEAD FOR COMPLIANCE WITH AD, NOTED (1) RIVET MISSING FROM NR7L STINGER CLIP AT ZEE SECTION ATTACHMENT. RIVET MISSING WAS AT FARTHEST FORWARD POSITION, REQUIRED REMOVING INSULATION AND SEALMay 5, 2005 · N200ZT · Beech B200 · FastenersSDR 2005FA0000671Fork · crackedFOUND CRACKED NOSE FORK TUBE AT LOWER WELD AREAS WHILE PERFORMING AD 2004-23-02, DURING ROUTINE PHASE INSPECTION. FORK WAS REPLACED WITH MFG KIT NR 101-8030-1, SN 2463.May 2, 2005 · N678SS · Beech B200 · Nose/Tail Landing GearSDR DJFA2005073Windshield · failedCREW REPORTED THAT THE RIGHT WINDSHIELD SHATTERED IN FLIGHT WHILE AIRCRAFT WAS CLIMBING THROUGH FL 210 TO 230. WINDSHIELD HEAT WAS ON AND OAT WAS 10 DEGREES CELSIUS.Mar 28, 2005 · N615TA · Beech B200 · Flight Compartment WindowsSDR CA050309004Booster · failed(CAN) SHOP TOOL FOR FILLING O2 SYSTEMS. THE OXYGEN BOOSTER DESCRIBED ABOVE WAS BEING USED TO FILL MEDICAL OXYGEN IN TO THE AIRCRAFT LIFEPORT MEDICAL SLED ON BOARD THE AIRCRAFT, WHEN THE UNIT EXPLODED WITH NO WARNING SENDING A TORCHING FLAME WITH HOT SHRAPNEL AMar 7, 2005 · Beech B200 · Portable Oxygen SystemSDR 2005FA0000404Exhaust Stack · crackedCRACK IN BARE METAL DUE TO ENGINE VIBRATION. (K)Mar 7, 2005 · Beech B200 · Engine Collector/Tailpipe/NozzleSDR 2005FA0000250Windshield · crackedPILOT REPORTED WINDSHIELD SHATTERED WHILE CRUISING AT FLIGHT LEVEL 24,000 FT. INNER PANE SHATTERED. (K)Feb 24, 2005 · N415RB · Beech B200 · Flight Compartment WindowsSDR CA050301004Gas Generator · cracked(CAN) DURING ENGINE INSPECTION USING A VIDEO BORESCOPE, THE HIGH PRESSURE BLEED VALVE TUBE FROM P3 WAS FOUND CRACKED OFF AND A HORIZONTAL CRACK APPROXIMATELY 3 INCHES LONG BELOW BLEED VALVE ATTACH FLANGE WAS NOTED. SOME STAINING INDICATED CRACK WAS PROBABLY NOFeb 21, 2005 · Beech B200 · Turbine Engine Compressor SectionSDR 2005FA0000257Windshield · brokenPILOT REPORTS THAT AT CRUISE ALTITUDE 24,000 FT, EVERYTHING NORMAL THE PILOTS WINDSHIELD OUTER GLASS SHATTERED. TO PREVENT RECURRENCE, REPLACED WITH KIT-STRESS FREE WINDOW INSTALLATION IAW INSTRUCTIONS PROVIDED. (K)Feb 17, 2005 · N345WK · Beech B200 · Flight Compartment WindowsSDR CA050127007Line · unserviceable(CAN) HYDRAULIC FLUID LEAKING OUT OF THE LT IB L/E. L/E REMOVED AND FOUND RIGID HYDRAULIC BRAKE LINE CHAFFED THROUGH BY ENGINE CONTROL CABLES ABOVE HEAT EXCHANGER. REPLACED LINE. ALL COMPANY AIRCRAFT USING THIS HYDRAULIC LINE VISUALLY INSPECTED AND FOUND DAMAJan 25, 2005 · Beech B200 · Hydraulic System, MainSDR 2006FA0000151Skin · crackedDURING PHASE 1-4 INSPECTION, EMERGENCY EXIT HATCH OUTER SKIN WAS FOUND CRACKED AT THE IB SURFACE, THROUGH THE ENTIRE 90 DEGREES RADIUS OF THE LOWER AFT CORNER OF SKIN ASSY 115430100-661A. CRACK LENGTH APPROX 6 INCHES. (K)Jan 24, 2005 · N1568E · Beech B200 · Emergency ExitsSDR 2005FA0000025Blower · arcedPILOT REPORTED AN ELECTRICAL SMELL DURING FLIGHT AND THEN THE FORWARD VENTILATION BLOWER WENT INOPERATIVE. FOUND THE BRUSHES WORN OUT AND ARCING ON THE ARMATURE. REPLACED WITH OVERHAULED UNIT AND FUNCTIONAL CHECK OK.Jan 10, 2005 · N773TP · Beech B200 · Air Distribution FanSDR PF212LWAAWindshield · crackedIN CRUISE FLIGHT AT FL290 IN VMC ON IFR FLIGHT PLAN WITH OAT OF -45C, INNER PANE OF CO-PILOTS WINDSHIELD SHATTERED WITHOUT WARNING.Dec 23, 2004 · N212LW · Beech B200 · Flight Compartment WindowsSDR 2004FA0000928Stringer · crackedSTRINGER NR 9 ON THE LT SIDE FOUND CRACKED DURING NON-RELATED MAINTENANCE.Dec 21, 2004 · N200EW · Beech B200 · Fuselage Main, Longeron/StringerSDR 2004FA0000941Stringer · crackedSTRINGER NR 9 ON THE RT SIDE WAS FOUND CRACKED DURING NON-RELATED MAINTENANCE.Dec 21, 2004 · N200EW · Beech B200 · Fuselage Main, Longeron/StringerSDR FCPR200500002Oxygen Bottle · rupturedDURING 3 YEAR HYDRO TEST O2 BOTTLE (20 YEARS INSERVICE 3HT 1850) RUPTURED AT OR BELOW 2100 PSI. SIGNIFICANT DAMAGE TO THE BOTTLE AND PRESSURE TEST TANK OCCURED. NO INJURIES TO TEST PERSONNEL.Dec 20, 2004 · N7250T · Beech B200 · Crew Oxygen SystemSDR 2004FA0000935Skin · delaminatedSKIN DELAMINATION ON LT WING CENTER SECTION UPPER SURFACE AFT OF THE SPAR NOTICED BY MAINTENANCE CREW, WHILE MAINTENANCE WAS BEING COMPLETED ON A NON-RELATED MATTER.Dec 20, 2004 · N200EW · Beech B200 · Wing, Plate/SkinSDR CA050110008Engine · failed(CAN) AFTER TAKE-OFF, THE NR 1 ENGINE REPORTEDLY LOST POWER. THE AIRCRAFT SETTLED TO THE GROUND, DEPARTED THE RUNWAY AND WAS CONSUMED BY FIRE. PWC WILL INVESTIGATED THE ENGINE AND WILL SUPPLIMENT THIS REPORT TO PROVIDE ROOT CAUSE, AS AND WHEN DETERMINED.Dec 10, 2004 · Beech B200 · Engine (Turbine/Turboprop)SDR DJFA2004037Windshield · crackedCREW REPORTED, THE PILOTS SIDE WINDSHIELD SHATTERED AT FL250. NORMAL LANDING WAS PERFORMED AT KBED. MAINTENANCE REMOVED AND REPLACED THE PILOTS SIDE WINDSHIELD. WINDSHIELD LEAK CHECK AND HEATING CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE.Nov 24, 2004 · N615TA · Beech B200 · Flight Compartment WindowsSDR CA041025002Diode · burned(CAN) EXPERIENCED NR1 DUAL FED BUS FAILURE IN FLT. NR 1 DUAL FEED BUSS EQUIP BECAME DE-ENERGIZED. AC LANDED WITHOUT INCIDENT. MAINT DISCOVERED BOTH DIODES BURNED OPEN ON NR1 DUAL FEED BUSS SYS. REPLACED DIODES WITH NEW, PERFORMED DUAL BUSS CONFORMITY CHECKOct 14, 2004 · Beech B200 · DC Power Distribution SystemSDR CA041020010Oil Filter · clogged(CAN) ON ROUTINE INSPECTION IT WAS DISCOVERED THAT A PIECE OF THE SCREEN SECTION WAS SEPERATING FROM THE EXTERNAL SECTION OF THE FILTER. NOT SURE IF IT IS A MANUFACTURING DEFECT OR IF THE FILTER WAS COMING APART IN USE.Oct 11, 2004 · Beech B200 · Turbine Engine Oil SystemSDR 2004FA0000794Indicator · malfunctionedTHE TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADINGS GREATER THAN 350 DEGREES OR LESS THAN 0 DEGREES. THIS PROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TESTING OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION IS SOFTWARE. THE ST3400 TAOct 8, 2004 · N2328E · Beech B200 · Directional Gyro and Indicating SystemSDR DJFA2004022Contact · dirtyCREW REPORTED THAT AFTER NORMAL TAKEOFF, THE YAW DAMPER AND AUTOPILOT FAILED TO ENGAGE ON SEVERAL ATTEMPTS. AIRCRAFT THEN DIVERTED TO DAL. MAINTENANCE CLEANED THE CONTACTS AT THE YAW RATE SENSOR AND APS-65. GROUND CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVIOct 7, 2004 · N619TA · Beech B200 · Autopilot SystemSDR KNI2004F00000Vane · crackedDURING PHASE INSPECTION, FOUND THE LT ICE VANE CRACKED THRU IN THE CENTER OF THE HINGE. UPON MORE INVESTIGATION, FOUND THE HINGE PIN HAD WORKED ITS WAY OUT OF THE HINGE. EVENTUALLY IT WORE A HOLE THRU THE DUCT SIDE WALL AND PROCEEDED TO COME OUT OF THE HINGESep 27, 2004 · N60AR · Beech B200 · Air Intake Anti/De-Ice SystemSDR VIBA20040916Fuel Control · failedTHE FUEL PUMP DRIVE SHAFT BEARING ASSEMBLY APPARENTLY FAILED OVER AN UUNDETERMINED PERIOD OF TIME, LEADING TO SHAFT LOCK UP AND SHEARED THE DRIVE COUPLING. BLACK RESIDUE FROM THE BEARING FAILURE WAS FOUND TO BE EMITTING FROM THE GANG DRAIN AND STREAKING BACK Sep 16, 2004 · N771MG · Beech B200 · Fuel Control/Turbine EnginesSDR 2004FA0000889Turbine · shiftedNEW STYLE, PN SEGMENT INSTALLED AT HSI 258 HRS PRIOR. THIS NEW STYLE SEGMENT SHIFTS AFT RESULTING IN HOT SECTION FAILURE. VERY COMMON WITH THIS PN SEGMENT 3053094/ MFG NEEDS TO CHANGE DESIGN.Sep 9, 2004 · N40PT · Beech B200 · Turbine SectionSDR 2004FA0000738Turbine · shiftedNEW STYLE PN SEGMENT INSTALLED AT HSI 258 HOURS PRIOR. THIS NEW STYLE SEGMENT SHIFTS AFT RESULTING IN HOT SECTION FAILURE. VERY COMMON WITH THIS PN SEGMENT, MFG NEEDS TO CHANGE DESIGN.Sep 9, 2004 · N40PT · Beech B200 · Turbine SectionSDR CA040908003Glide Slope · erratic(CAN) RT GLIDESLOPE INDICATION VERY ERRATIC AND NO WARNING FLAP IN VIEW TELLING PILOT SIGNAL INVALID. MEL'ED SYSTEM AND TROUBLESHOOTING IN PROGRESS.Sep 7, 2004 · Beech B200 · Glide Slope SystemSDR CA040831021Gps · out of adjust(CAN) PILOT REPORTS GPS 60 DEGREES OFF TRACK. T/S INDICATES CALIBRATION OF UNIT 60 DEGREES OUT. RECALIBRATED.Aug 30, 2004 · Beech B200 · Global Positioning SystemSDR 2004FA0000695Fuel Control · seizedPILOT NOTED UNCOMMANDED LEFT ENGINE TORQUE AND ITT INCREASE IN FILGHT ON INITIAL APPROACH TO MKE. NO RESPONSE TO POWER LEVER INPUT. PILOT SHUTDOWN ENGIEN AND DIVERTED TO RFD. DURING REMOVAL OF FCU FOR TROUBLESHOOTING NOTED FCU INPUT SHAFT COUPLING SHEARED, Aug 16, 2004 · N698P · Beech B200 · Fuel Control/Turbine EnginesSDR CA040805016Sensor · faulty(CAN) UPON REGULAR PHASE INSPECTION, THE FIRE DETECTION SYSTEM FAILED TO TEST CORRECTLY ON RT ENGINE. TROUBLESHOT AND FOUND SENSOR AT FAULT. REPLACED SENSOR, OPERATION RESTORED TO NORMAL.Aug 4, 2004 · Beech B200 · Fire DetectionSDR DJX2004F00000Solenoid · inoperativeDURING A RUDDER BOOST TEST THE RT RUDDER PEDAL, REMAINED AT FULL DEFLECTION EVEN WITH THE ENGINES AT IDLE. BY TURNING THE SYSTEM OFF BOTH PDEALS WOULD RETURN TO CENTER. IF THE SYSTEM FAILED ON FINAL AND OR DURING TAKE OFF THE END RESULT COULD BE DEVASTATING.Jul 24, 2004 · N946CE · Beech B200 · Rudder Control SystemSDR 2004F00307Bearing · failedAFT BEARING ON FREON COMPRESSOR BELT DRIVE FAILED, BURNED UP AND DISINTEGRATED. THE BEARINGS ARE SEALED, AND HAVE NON REPLACEMENT INTERVAL. REPLACED BOTH BEARINGS, QUILL SHIFT, AND BELT WITH NEW. WILL REPLACE BEARINGS ON A 1200 HOUR INTERVAL. (M)Jul 23, 2004 · N260G · Beech B200 · Cabin Compressor SystemSDR CA040628009Skin · cracked(CAN) COMBINATION VHF/GPS ANTENNA DOUBLER AND FUSELAGE SKIN CRACKED UNDER COMANT ANTENNA WHICH WAS ENGINEERED AND INSTALLED IAW LSTC NR C-LSA01-625/D. FUSELAGE REPAIRED AND ANTENNA REMOVED. NEW REPAIR DOUBLER INSTALLED.Jun 28, 2004 · Beech B200 · Fuselage Main, Plate/SkinSDR CA040628008Skin · cracked(CAN) COMBINATION VHF/GPS ANTENNA DOUBLER AND FUSELAGE SKIN CRACKED UNDER ANTENNA WHICH WAS ENGINEERED AND INSTALLED IAW LSTC NR C-LSA01-625/D. FUSELAGE REPAIRED AND ANTENNA REMOVED. NEW REPAIR DOUBLER INSTALLED.Jun 28, 2004 · Beech B200 · Fuselage Main, Plate/SkinSDR CA040621006Receptacle · corrodedCOURTESY AND ENTRANCE DOOR LIGHTS REPORTED U/S. TROUBLESHOOTING LED TO CONNECTOR P406 LOCATED IN THE AIRCRAFT SIDEWALL FORWARD OF THE ENTRANCE DOOR. FOUND CONNECTOR PINS CORRODED, PRIMARILY PIN 7 THATSUPPLIES 28VDC TO THE CIRCUIT. WIRING REPAIRED AND AIRCRAJun 17, 2004 · Beech B200 · Passenger Compartment LightingSDR CA040519004Rudder Pedal · worn(CAN) RUDDER PEDAL ATTACH POINT BROKEN AT BUSHING ATTACH.May 12, 2004 · Beech B200 · Rudder Control System
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