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 CA000927004Fuel Control · failed(CAN) UPON APPROACH TO YRT, PILOTS DISCOVERED NR 1 ENGINE WOULD NOT RESPOND TO POWER LEVER COMMANDS. AS A RESULT, THE PILOTS HAD TO SHUT DOWN NR 1 ENGINE TO LAND. FCU WAS REPLACED. ENGINE GROUND TESTED SERVICEABLE. (X)Aug 28, 2000 · Beech B200 · Fuel Control/Turbine EnginesSDR CA000906006Windshield · failed(CAN) WHILE IN CRUISE AT 28,000 FEET, THE R/H WINDSHIELD FAILED. THE INNER LAMINATION SUSTAINED A FAILURE RESULTING IN A LATTICE LIKE SERIES OF CRACKS. (INSTALLED MAY 1997.)Aug 17, 2000 · Beech B200 · Flight Compartment WindowsSDR 20000914SH013Door · out of rigWHILE CONDUCTING A TRAINING EXERCISE, CREW SIMULATED AN ENGINE OUT WITH THE LANDING GEAR DOWN. DURING COURSE OF THE SCENARIO, THE GEAR WAS RETRACTED. THE CREW NOTED THE HYDRAULIC PUMP STAYED ON UNUSUALLY LONG. THE GEAR WAS PUT BACK DOWN AND AIRCRAFT SOON AFAug 14, 2000 · N55FJ · Beech B200 · Landing Gear Door Retract SectionSDR 20000828SH021Motor · failedAGC, AIRCRAFT DEPARTED, UPON RETRACTION, FLIGHT CREW NOTICED GEAR OPERATION SOUNDED SLUGGISH. APPROX HALF WAY UP ON RETRACTION, THE GEAR STOPPED FOR A SECOND OR SO, THEN CONTINUED TO RETRACT. PILOTS NOTICED A RED LIGHT IN THE GEAR HANDLE. CREW SELECTED GEARJul 27, 2000 · N152C · Beech B200 · Landing Gear Retraction/Extension SystemSDR CA000621008Bearing · seized(CAN) DURING CRUISE RT ENGINE FLUXUATES ALL PARAMETERS THAN DROPS TO GROUND IDLE. UNEVENTFUL LANDING. T/S P3,PY ALL SYSTEM FOR LEAKS AND OR BLOCKAGE - NONE FOUND. PULLED FCU AND FOUND DRIVE BEARING SEIZED AND DRIVE COUPLER BROKEN.Jun 7, 2000 · Beech B200 · Fuel Control/Turbine EnginesSDR 20000601SH008Stringer · crackedCOMPLIED WITH AD 93-25-07 IAW SD 2472. NR 10 STRINGER ON THE LEFT SIDE WAS FOUND CRACKED. TOTAL LANDINGS: 7,189. (X)Jun 1, 2000 · N86DD · Beech B200 · Wing, Longeron/StringerSDR 20000613SH026Link · out of toleranceTHE RELEASE LINKS AND PINS IN BOTH MAIN LANDING GEAR DOWNLOCKS WERE REMOVED FROM AIRCRAFT FOR INSPECTION. INSPECTION REVEALED BOTH PINS WERE WORN APPROX .002 INCH BEYOND LIMITS AND BOTH LINK PIN HOLES HAD CIRCUMFERENTIAL SCRATCHES INDICATING THAT PINS HAD ATMay 25, 2000 · N529NA · Beech B200 · Landing Gear Retraction/Extension SystemSDR 20000613SH014Pin · wornTHE RELEASE LINKS AND PINS IN BOTH MAIN LANDING GEAR DOWNLOCKS WERE REMOVED FROM AIRCRAFT FOR INSPECTION. INSPECTION REVEALED BOTH PINS WERE WORN APPROX .002 INCH BEYOND LIMITS AND BOTH LINK PIN HOLES HAD CIRCUMFERENTIAL SCRATCHES INDICATING THAT PINS HAD ATMay 25, 2000 · N529NA · Beech B200 · Landing Gear Retraction/Extension SystemSDR 20000602SH007Motor · inoperativeCONDENSER BLOWER MOTOR NO GOOD.Apr 19, 2000 · N260G · Beech B200 · Humidity Control SystemSDR CA000322019Probe · leaking(CAN) PILOT NOTICED FUEL TRAILING FROM AIRCRAFT DURING FLIGHT. DISCOVERED FUEL PROBE WAS LEAKING OUT THROUGH CENTER OF PROBE. PROBE REPLACED.Mar 13, 2000 · Beech B200 · Fuel Quantity SensorSDR 20000622SH016Retainer · brokenLANDING GEAR DOWN AND LOCKED ANNUNCIATOR BULB LOST ELECTRICAL POWER DUE TO WORN ANNUNCIATOR CAP RETAINING PINS ALLOWING CAP TO SEPARATE FROM ANNUNCIATOR ASSEMBLY. REF: B200 WIRING MANUAL 32-61-00, PAGE 2. (X)Feb 10, 2000 · N3127K · Beech B200 · Landing Gear Retraction/Extension SystemSDR 2000ZZZX643Windshield · broken1-14-00 - FLYING AT 27,000 FEET, THE RIGHT SIDE COPILOT WINDWHIELD BROKE ON THE INSIDE PORTION OF THE WINDOW. THE OUTSIDE PORTION OF THE WINDSHIELD REMAINED INTACT. THE CREW DEPRESSURIZED THE CABIN PER EMERGENCY PROCEDURES AND RETURNED TO PDX. 1-16-00 - AFTJan 14, 2000 · N63791 · Beech B200 · Flight Compartment WindowsSDR CA000118002Squat Switch · out of adjust(CAN) AFTER TAKEOFF, THE GEAR FAILED TO RETRACT WHEN SELECTED UP. RETRACTION CHECKED CARRIED OUT IN HANGAR. FAILURE FOUND TO BE RIGHT SQUAT SWITCH OUT OF ADJUSTMENT.Dec 31, 1999 · Beech B200 · Landing Gear Position and WarningSDR CA991229043Lever · slipped(CAN) CAMBOX INPUT LEVER SLIPPING ON SHAFT, DUE TO INTERFERENCE FROM IMPROPERLY RIGGED FUEL SHUTOFF LINKAGE. OPERATOR REQUESTS TORQUE VALUE FOR IMPUT LEVERFROM MANUFACTURER, NOTE SHAFT IS SERRATED STANDARD MAINTENANCE PRACTICES CAN BE IMPLOYED.Dec 21, 1999 · Beech B200 · Power LeverSDR CA991229044Attach Fitting · damaged(CAN) DAMAGE FOUND ON COUNTERBORE FITTINGS FACE OF UPPER AND LOWER AFT WING ATTACH POINTS.FOUND INCORRECT PART NUMBER WASHER, USED ON BOLT STACK-UP FOR AFT FITTINGS.Dec 17, 1999 · Beech B200 · Wing, Attach FittingsSDR CA991229042Windshield · cracked(CAN) WINDSHIELD CRACKED IN FLIGHT BELIEVED TO HAVE BEEN CAUSED BY HAILSTONE STRIKING WINDSCREEN AND PREVIOUS DELAMINATION. UPON REMOVAL OF WINDSCREEN IT WAS DISCOVERED THAT THE MINIMUM ALLOWABLE CLEARANCE BETWEEN THE WINDSCREEN FLANGEAND THE AIRFRAME WAS BELODec 10, 1999 · Beech B200 · Flight Compartment WindowsSDR CA991229041Probe · worn(CAN) MAINTENANCE LOCATED FUEL QUANTITY ERRATIC READINGS TO BE FROM THE LT CENTRE AUX TANK PROBE.UPON EXAMINATION IT WAS DISCOVERED THAT THE FUEL PROBE SOUTER SHEATH OF THE CAPACITOR WAS LOOSE AT THE UPPER ATTACH RIVETS. THIS MOVEMENT WOULD HAVE VARIED THE ELEDec 8, 1999 · Beech B200 · Fuel Quantity SensorSDR 2000ZZZX415Tie Strap · brokenDURING ROUTINE INSPECTION, THIS TIE STRAP WAS FOUND BROKEN. THE AIRPLANE AT ALL OTHER LIKE LOCATIONS WAS INSPECTED FOR MORE CRACKS OR BREAKS. NONE WERE FOUND OTHER THAN THE ONE AT STA 227.125, RIGHT SIDE. THE POSSIBLE CAUSE WAS THAT THE PARTS WERE NOT PROPEDec 1, 1999 · N63791 · Beech B200 · Fuselage Miscellaneous StructureSDR 99ZZZX4397Fcu · leakingFOUND FUEL LEAKING OUT OF IDLE CUT-OFF SHAFT OF FUEL CONTROL UNIT.Nov 3, 1999 · N500LP · Beech B200 · Fuel Control/Turbine EnginesSDR 2000ZZZX666Windshield · crackedBTV/RDU - FLT 260 - EN ROUTE, THE INSIDE GLASS LAYER OF THE PILOT'S WINDSHIELD CRACKED. OUTSIDE LAYER REMAINED INTACT. NO CHANGE IN CABIN PRESSURE. IMMEDIATELY DESCENDED AND DIVERTED TO POU WHERE PILOT'S WINDSCREEN WAS REPLACED.Oct 14, 1999 · N55PC · Beech B200 · Flight Compartment WindowsSDR 99ZZZX3979Rod End · bentDURING ROUTINE POST-FLIGHT INSPECTION, FOUND ROD-END, PN 115-555026-15 (FOR THE FREON COMPRESSOR BELT TENSIONER), BENT APPROXIMATELY 10 DEGREES. REPLACED PART WITH NEW.Aug 27, 1999 · N260G · Beech B200 · Cabin Cooling SystemSDR 99ZZZX3381Indicator · failedNR 1 ITT GAUGE DROPPED TO ZERO ON APPROACH. TROUBLESHOT TO BAD ITT GAUGE. REPLACED GAUGE, PN 41-402-1, SN 483 OFF, PN 130-380041-7, SN 543 ON. OPERATIONS CHECKED OK.Aug 11, 1999 · N670DF · Beech B200 · Engine EGT/TIT Indicating SystemSDR 99ZZZX3001Cooler · failedWHILE PERFORMING RUN-UP CHECKS, NR 1 ENGINE WOULD NOT ACCELERATE. TROUBLESHOT TO BAD FUEL/OIL HEAT EXCHANGE P/N 3039259, S/N WA11014. INSTALLED NEW FUEL OIL HEAT EXCHANGE P/N 3039259, S/N W11769. OPERATIONS CHECKED OK.Jul 30, 1999 · N670DF · Beech B200 · Engine Fuel/Oil CoolerSDR 99ZZZX2910Piston · crackedINSPECTION OF FLAP SYSTEM REVEALED DEFECTIVE LEFT OUTBOARD FLAP ACTUATOR DRIVE PISTON. DRIVE PISTON FOUND CRACKED AT FLAP ROD END EXTENDING 1.5 INCHES LONGITUDINALLY, FORWARD WITH RESPECT TO AIRCRAFT INSTALLATION.Jul 22, 1999 · N87JE · Beech B200 · Trailing Edge Flap ActuatorSDR 99ZZZX3457Windshield · crackedPILOT'S WINDSHIELD CRACKED IN-FLIGHT ON GAL/FAI LEG. LANDED AT FAI.Jul 16, 1999 · N575T · Beech B200 · Flight Compartment WindowsSDR 99ZZZX2970Bracket · brokeON TAKEOFF, BOTH SEAT BACK SUPPORT ADJUSTER BRACKETS BROKEN ON NR 6 PASSENGER SEAT. THIS IS THE THIRD OCCURRENCE WITH THIS PART.Jul 13, 1999 · N223HC · Beech B200 · Passenger Compartment EquipmentSDR 99ZZZX2969Bracket · brokeON TAKEOFF, BOTH SEAT BACK SUPPORT ADJUSTER BRACKETS BROKEN ON NR 6 PASSENGER SEAT. THIS IS THE THIRD OCCURRENCE WITH THIS PART.Jul 13, 1999 · N223HC · Beech B200 · Passenger Compartment EquipmentSDR 99ZZZX1963Fuel Cell · mismanufacturedFUEL CELL MANUFACTURED WITH MOUNTING HOLES MISALIGNED CAUSING FUEL LEAK.Apr 23, 1999 · N975SC · Beech B200 · Fuel StorageSDR R7MA0000595Transmitter · fluctuatingTRANSMITTER CAUSES INDICATING FLUCTUATIONS. (X)Apr 8, 1999 · N301HC · Beech B200 · Fuel Flow IndicatingSDR R7MA0000594Gyro Compass · inoperativeNR 1 SYSTEM FAILED ON GROUND DURING TROUBLESHOOTING OF NR 2 SYSTEM. NR 1 SYSTEM INOPERATIVE. (X)Apr 7, 1999 · N501HC · Beech B200 · Directional Gyro and Indicating SystemSDR 99ZZZX1728Transducer · failedNR 1 ENGINE OIL PRESSURE FLUCTUATES HIGH. TROUBLESHOT TO OIL PRESSURE TRANSMITTER. REPLACED TRANSMITTER, PN 101-389023-5, SN 6013-6-42 OFF, SN 5624-5-29 ON. OPERATIONS CHECKED OK.Mar 31, 1999 · N670DF · Beech B200 · Engine Oil PressureSDR CA990412005Windshield · shattered(CAN) COPILOT WINDSHIELD INNER PLY SHATTERED. AIRCRAFT WAS IN CRUISE AT 27,000 FEET AT MAXIMUM CABIN DIFFERENTIAL (6.0 PSI). FLIGHT CREW DEPRESSURIZED AIRCRAFT AND DESCENDED TO 12,000 FEET.Mar 27, 1999 · Beech B200 · Flight Compartment WindowsSDR 99ZZZX1825Relay · contaminatedCOPILOT'S GLIDESLOPE REMAINS CENTERED AT ALL ITEMS ON ILS APPROACH. NO FLAG ON HSI. TROUBLESHOOTING REVEALED THAT PINS ON RELAY M39016/6-209L OR CONTACTS ON PRINTED CIRCUIT BOARD WERE DIRTY OR OXIDATED. RELAY K1 IN RELAY BOX PL-A. SAME RELAY FOR GLIDESLOPEFeb 24, 1999 · N200QS · Beech B200 · Glide Slope SystemSDR 99ZZZX3298Compressor · seizedCOMPRESSOR LOCKED UP. REF: MCN NR 4.Jan 31, 1999 · N75LV · Beech B200 · Turbine Engine Compressor SectionSDR 99ZZZM245Fuel System · contaminatedRIGHT ENGINE SURGED WITH LARGE FUEL FLOW FLUCTUATIONS, AND WAS SHUT DOWN AFTER TRYING STANDBY FUEL PUMPS, OAT -47 DEGREES CELSIUS. DRAINED FUEL SUMPS. CLEANED FUEL BOWLS. INSPECTED TANKS FOR CONTAMINATION, ETC. OPERATIONAL CHECK AFTERWARDS WAS AIRWORTHY. Jan 24, 1999 · N4277C · Beech B200 · Fuel StorageSDR 99ZZZX1137Blade · damagedPROPELLER DAMAGED DUE TO PROPELLER STRIKE. THREE EACH BLADES REMOVED, P/N 100LA-2. S/N'S EJ-015, EJ-023, EJ-046. TIME SINCE NEW: 1,008.2 HOURS.Jan 8, 1999 · N301HC · Beech B200 · Propeller Blade SectionSDR 99ZZZX1136Turbine · damagedPROPELLER STRIKE. DUE INSPECTION DUE TO SUDDEN STOPPAGE. PART CYCLES: 3192.Jan 8, 1999 · N301HC · Beech B200 · Turbine SectionSDR 99ZZZX885Fuel Probe · malfunctionedFUEL PROBE MALFUNCTIONEDJan 5, 1999 · N401HC · Beech B200 · Fuel Indicating SystemSDR 99ZZZX884Valve · failedFUEL SHUT-OFF VALVE FAILED.Jan 5, 1999 · N401HC · Beech B200 · Fuel Selector/Shut-Off ValveSDR 99ZZZX883Fuel Probe · malfunctionedFUEL PROBE MALFUNCTIONED.Jan 5, 1999 · N401HC · Beech B200 · Fuel Indicating SystemSDR 99ZZZX393Floorboards · crackedCENTER ISLE FLOORBOARDS FORWARD OF SPAR ARE SPLIT DOWN THE CENTER WITH A SINGLE CAMLOC FASTENER TO HOLD EACH SET OF PANELS TOGETHER. PANELS ARE VERY SPONGY FEELING WHEN WALKED ON, AND THE FORWARD PANEL FLEXES DOWN AND RESTS ON THE NON-STRUCTURAL THIN PLASTIC Jan 5, 1999 · N260G · Beech B200 · Fuselage Floor PanelSDR 99ZZZX355Chain · loosePILOT REPORTED LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER RETRACTING GEAR. TROUBLESHOT AND FOUND FORWARD CHAIN PARTIALLY OFF IDLER SPROCKET. RE-INSTALLED CHAIN ON SPROCKET. ADJUSTED CHAIN TENSION AND ADJUSTED UPLOCK SWITCH IAW BEECH KA200 MM. Dec 1, 1998 · N72GG · Beech B200 · Landing Gear Retraction/Extension SystemSDR 99ZZZX245Circuit Breaker · failedNR 1 BUSS CIRCUIT BREAKER TRIPPED, LEFT HAND SIDE. LOSS OF POWER TO ESSENTIAL BUSS. NR 1 RIGHT HAND BUSS FEED CIRCUIT BREAKER BAD. REMOVED AND REPLACED NR 1 RIGHT HAND CIRCUIT BREAKER WITH NEW UNIT P/N 700-001-50.Nov 11, 1998 · N72GG · Beech B200 · AC Generation SystemSDR 98ZZZX4424Valve · malfunctionedVALVE, FLOW CONTROL HAS LOW OUTPUT. PROBLEM FOLLOWED UNIT WHILE SWAPPING FROM SIDE-TO-SIDE. REPLACED IWTH NEW UNIT, CORRECTED PROBLEM.Nov 7, 1998 · N220TB · Beech B200 · Pressure Regulator/Outflow ValveSDR 98ZZZX4132Wire · chafedCUSTOMER SAID MFD WAS STAYING A BLUE COLOR IN-FLIGHT. REMOVED RADIO PANEL, FOUND CHAFED WIRES (4 TWISTED PAIRS) 50FD054, 50FD055, 50FD062, 50FD063, 50FD066, 50FD067, 50FD120, AND 50FD124. 52AA052 AND 52AC018, ALSO, FOUND 2 BARE WIRES GOING TO THE FCP-65 A/PSep 30, 1998 · N151CF · Beech B200 · Instrument System WiringSDR 98ZZZX4213Wheel · corrodedDURING A ROUTINE TIRE CHANGE OF THE LISTED COMPONENT, VISIBLE SIGNS OF CORROSION THROUGH THE WHEELS PAINT JOB WAS APPARENT. UPON FURTHER INVESTIGATION, THE CORROSION WAS NOTED AS EXCESSIVE AND BEYOND STATED LIMITS NOTED IN THE COMPONENT MM. AREAS OF CORROSISep 28, 1998 · N200MJ · Beech B200 · Wheel/Ski/FloatSDR 99ZZZX109Bellcrank · failedDOOR WOULD NOT LATCH PROPERLY, AND SOMETIMES GET LOCKED IN CLOSED POSITION. ALSO, LARGE PRESSURIZATION LEAK DEVELOPED AT FORWARD UPPER CORNER OF DOOR. UPON FURTHER INSPECTION, FOUND FORWARD BELLCRANK, P/N 50-430031-15, BENT AND IMPROPERLY MANUFACTURED AT 60 Jul 31, 1998 · N3092S · Beech B200 · Passenger/Crew DoorsSDR 98ZZZX1976Windshield · shatteredWHILE AT 22,000 FEET AND IN CRUISE FLIGHT, THE PILOT TURNED ON WINDSHIELD HEAT AND IMMEDIATELY THE WINDSHIELD SHATTERED. BOTH PPG AND RAYTHEON ADMIT THIS IS A COMMON OCCURRENCE. THE EXACT DATE WHEN THE DISCREPANT WINDSHIELD WAS INSTALLED IS NOT CLEAR. REPLACMar 19, 1998 · N220TB · Beech B200 · Flight Compartment WindowsSDR 99ZZZX663Nut · strippedTHE NOSE GEAR FAILED TO EXTEND FULLY BEFORE LANDING. ELECTRICAL AND MANUAL EXTENSION PROCEDURE WERE NOT SUCCESSFUL CAUSING THE NOSE GEAR TO COLLAPSE DURING LANDING. INSPECTION OF THE NOSE GEAR ACTUATOR, P/N 50-820208-5, REVEALED THAT NUT ASSY, P/N 90-820015Mar 11, 1998 · N75ZT · Beech B200 · Landing Gear ActuatorSDR 98ZZZX1382Stand-Off · brokenSTAND-OFF FOR FIRE PROTECTION SENSOR FOUND BROKEN ON RT AND LT ENGINES. STAND-OFF IS BOLTED TO EXHAUST STACK FLANGE BOLT AND ADEL CLAMP FOR SENSOR.Mar 11, 1998 · N909J · Beech B200 · Fire Detection
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