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 AU000661Frame · cracked(AUS) FUSELAGE FRAME 207 LEFT, CRACKED. (X)Sep 1, 2000 · Beech B200C · Fuselage Main, FrameSDR CA000809012Tube · split(CAN) DURING CLIMB CREW OBSERVED A RT BLEED AIR LIGHT. WHEN RT BLEED AIR SWITCHED OFF, LT BLEED WOULD NOT HOLD CABIN PRESSURE. AN EMERGENCY DESCENT WAS CARRIED OUT. AT 7,000 THE AIRCRAFT LEVELED OFF AND RETURNED TO BASE. THE DAMAGED PIECE OF TUBING WAS REPLACEJul 24, 2000 · Beech B200C · Cabin Pressure SensorSDR AU000532Frame · cracked(AUS) LEFT FUSELAGE FRAME NR 207 CRACKED. LEFT AND RIGHT STIFFENER PN 101-120021-17 AND PN 101-120021-18 ALSO CRACKED. (X)Jul 11, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000530Frame · cracked(AUS) FUSELAGE FRAME NR 207 CRACKED ON LEFT SIDE. (X)Jul 9, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000460Gearbox · contaminated(AUS) PROPELLER REDUCTION GEARBOX METAL CONTAMINATION.May 29, 2000 · Beech B200C · Turbine Engine Reduction GearSDR AU000361Bearing · failed(AUS) ENGINE POWER SECTION FAILED. SUSPECT CAUSED BY NR 3 BEARING FAILURE.May 1, 2000 · Beech B200C · Turbine SectionSDR AU000210Panel · missing(AUS) RIGHT NACELLE FUEL DRAIN PANEL NOT REINSTALLED FOLLOWING MAINTENANCE. SAFETY PLUG AND LOCKWIRE ALSO MISSING.Mar 17, 2000 · Beech B200C · Nacelle/Pylon, Plate/SkinSDR CA000404005Fire Detector · shorted(CAN) THE CREW REPORTED THAT DURING FLIGHT THE LEFT ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE LIGHT INDICATION OCCURS ONLY AFTER PRECIPITATION OR AIRCRAFT WASHING. FOUND FIRE DETECTOR TRIGGER VOLTAGE LEAKING THROUGH WIRE INSULATION WHEN IT IS WET.Feb 29, 2000 · Beech B200C · Fire DetectionSDR AU000167Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD TOP WEB CRACKED IN SEVERAL PLACES.Feb 28, 2000 · Beech B200C · Fuselage Main, BulkheadSDR AU000157Bulkhead · cracked(AUS) REAR PRESSURE BULKHEAD LOCATED AT BS 346.75 CRACKED IN TWO PLACES.Feb 28, 2000 · Beech B200C · Fuselage Main, BulkheadSDR AU000160Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Feb 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000158Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Feb 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000045Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000050Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000049Frame · cracked(AUS) FUSELAGE FRAME 207 CRACKED.Jan 22, 2000 · Beech B200C · Fuselage Main, FrameSDR AU000048Frame · cracked(AUS) FUSELAGE FRAME LOCATED AT BS 207 RT CRACKED. CRACKS ALSO FOUND ON FUSELAGE FRAMES AT BS 197.5 AND BS 227.Jan 20, 2000 · Beech B200C · Fuselage Main, FrameSDR AU991026Actuator · faulty(AUS) LANDING GEAR MOTOR FAULTY.Oct 16, 1999 · Beech B200C · Landing Gear ActuatorSDR AU991023Windshield · broken(AUS) INNER PANEL ON PILOT'S WINDSHIELD SHATTERED.Oct 8, 1999 · Beech B200C · Flight Compartment WindowsSDR AU990820Wire · worn(AUS) WIRE BUNDLE CHAFING ON PITOT/STATIC LINE IN AREA BELOW THE CIRCUIT BREAKER PANEL.Aug 12, 1999 · Beech B200C · Electrical Power System WiringSDR AU990810Circlip · separated(AUS) EMERGENCY UNDERCARRIAGE HAND PUMP PISTON RETAINING CIRCLIP DISLODGED ALLOWING LOSS OF HYDRAULIC FLUID.Aug 6, 1999 · Beech B200C · Landing Gear Retraction/Extension SystemSDR AU990799Disc · broken(AUS) BRAKE ROTATING DISC BROKEN. SUSPECT CAUSED BY OVERHEATING.Jul 30, 1999 · Beech B200C · BrakeSDR AU990725Propeller Assy · fod(AUS) PROPELLER CONTAINED FOD LEFT OVER FROM THE LAST ASSEMBLY. A BRIDGING TOOL USED TO PREVENT CUTTING OF THE PISTON O-RING DURING ASSEMBLY WAS FOUND ON THE PRESSURE SIDE OF THE PISTON. THE PISTON SKIRT HAD BEEN DAMAGED AND THE CYLINDER SCORED. FOD.Jul 16, 1999 · Beech B200C · Propeller AssemblySDR AU990711Hub · fod(AUS) PROPELLER FOD. A SMALL BRIDING TOOL WAS FOUND INSIDE THE PROPELLER CAUSING DAMAGE TO PARTS. METAL CONTAMINATION OF OIL SYSTEM.Jul 14, 1999 · Beech B200C · Propeller Hub SectionSDR AU990093Warning System · contaminated(AUS) FIRE WARNING SYSTEM CONTAMINATED WITH MOISTURE CAUSING FALSE FIRE WARNING.Feb 5, 1999 · Beech B200C · Fire DetectionSDR CA990119006Guard · missing(CAN) AIRCRAFT IN-FLIGHT WHEN ELEVATOR TRIM JAMMED. NO DIFFICULTIES ENCOUNTERED. INVESTIGATION REVEALED THAT THE ELEVATOR TRIM CABLE HAD JUMPED OFF THE DRUM OF THE COCKPIT CONTROL QUADRANT. ICE MAY HAVE BEEN A FACTOR CAUSING TRIM TO BE STIFF. WHEN OPERATEDJan 1, 1999 · Beech B200C · Elevator Tab Control SystemSDR AU981357Nut · cracked(AUS) LEFT MAIN LANDING GEAR ACTUATOR NUT CRACKED CIRCUMFERENTIALLY FOR APPROXIMATELY 25 PERCENT OF THE CIRCUMFERENCE 31.75 MM (1.25 INCH FROM THE TOP OF THE NUT.Oct 19, 1998 · Beech B200C · Landing Gear ActuatorSDR AU981113Control Cable · worn(AUS) RIGHT OUTBOARD FLAP DRIVE CABLE WORN AT THE MOTOR END. PART TC: 9,693.Sep 4, 1998 · Beech B200C · Trailing Edge Flap Control SystemSDR AU981009Windshield · bird strike(AUS) LEFT WINDSHIELD OUTER PANE EXTENSIVELY CRACKED DUE TO BIRDSTRIKE.Aug 13, 1998 · Beech B200C · Flight Compartment WindowsSDR CA980819011Fire Detector · failed(CAN) DURING FLIGHT, MASTER CAUTION AND RIGHT FIRE LIGHT ILLUMINATED. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK FOUND FAULTY FIRE DETECTOR SENSOR AND THERE WAS NO EVIDENCE OF FIRE.Aug 11, 1998 · Beech B200C · Fire DetectionSDR AU981027Pin · defective(AUS) POWER LEVER GROOVED PIN IS IMPRESSING GROOVES INTO LIGHT ALLOY OF POWER LEVER ARM.Aug 5, 1998 · Beech B200C · Power LeverSDR AU981026Lever · loose(AUS) ENGINE POWER LEVER ARM SLIPPING ON THE GROOVED PIN OF THE REVERSING MECHANISM. SUSPECT LEVER ARM CLAMPING BOLT AND NUT INSUFFICIENTLY TORQUED DURING INSTALLATION 47.2 HOURS PREVIOUSLY.Aug 5, 1998 · Beech B200C · Power LeverSDR AU981232Regulator · failed(AUS) LKH VOLTAGE REGULATOR FAULTY.Jul 28, 1998 · Beech B200C · DC RegulatorSDR AU981233Regulator · failed(AUS) LEFT VOLTAGE REGULATOR FAILED.Jul 27, 1998 · Beech B200C · DC RegulatorSDR AU981015Bearing · failed(AUS) LEFT ENGINE NR 4 BEARING CAGE FAILED. METAL CONTAMINATION OF OIL SYSTEM.May 21, 1998 · Beech B200C · Turbine SectionSDR AU980527Switch · failed(AUS) ICE VANE MICROSWITCH FAILED INTERNALLY.May 2, 1998 · Beech B200C · Ice/Rain Protection SystemSDR AU980751Windshield · cracked(AUS) PILOT'S WINDSCREEN OUTER PLY CRACKED. PART TOTAL CYCLES: 1,967.Apr 23, 1998 · Beech B200C · Flight Compartment WindowsSDR AU980519Switch · faulty(AUS) NOSE LANDING GEAR POSITION MICROSWITCH FAULTY.Mar 12, 1998 · Beech B200C · Landing Gear Position and WarningSDR AU980248Skin · debonded(AUS) LT WING CENTER SECTION LOWER SKIN DEBONDED.Feb 25, 1998 · Beech B200C · Wing, Plate/SkinSDR AU980247Web · corroded(AUS) LT LANDING GEAR DRAG BRACE OUTBOARD ATTACHMENT WEB CORRODED.Feb 17, 1998 · Beech B200C · Wing, Landing Gear Attach FittingsSDR AU980246Detector · contaminated(AUS) LT ENGINE FIRE DETECTORS CONTAMINATED WITH MOISTURE. FALSE FIRE WARNING RESULTED IN ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGE.Feb 15, 1998 · Beech B200C · Fire DetectionSDR AU980157Brake Disc · worn(AUS) RH OUTBOARD BRAKE ROTOR CRACKED. RH OUTBOARD WHEEL CRACKED AT BRAKE DRIVE LUG.Feb 2, 1998 · Beech B200C · BrakeSDR AU980285Panel · shorted(AUS) CIRCUIT BREAKER (CB) PANEL BUS FEEDER SHORT CIRCUITING TO AIRFRAME ADJACENT TO CBS. SHORT CIRCUIT OCCURRED DUE TO WATER LEAKAGE FROM WINDOW.Jan 20, 1998 · Beech B200C · DC Power Distribution SystemSDR AU971563Hose · failed(AUS) OXYGEN SYSTEM ON/OFF CONTROL CABLE FAILED. OXYGEN SYSTEM REMAINED ON FOR AN EXTENDED TIME CAUSING THE SUPPLY HOSE TO THE CASUALTY OXYGEN MASK TO RUPTURE AND ALLOWING THE OXYGEN SYSTEM TO DISCHARGE TO 0PSI.Dec 3, 1997 · Beech B200C · Passenger Oxygen SystemSDR AU971516Switch · intermittent(AUS) LANDING GEAR DOWNLOCK MICROSWITCH INTERMITTENT OPERATION.Nov 13, 1997 · Beech B200C · Landing Gear Position and WarningSDR AU971515Windshield · bird strike(AUS) BIRDSTRIKE ON RH WINDSCREEN. NIL DAMAGE.Nov 8, 1997 · Beech B200C · Flight Compartment WindowsSDR AU971439Blade · fod(AUS) LH PROPELLER BLADE TIP BENT. BLOOD ON THE BLADE LEADS TO THE ASSUMPTION OF AND ANIMAL STRIKE.Oct 21, 1997 · Beech B200C · Propeller Blade SectionSDR AU970834Trim System · malfunction(AUS) ELEVATOR TRIM FAULTY - MAINTENANCE CHECKS COULD FIND NO FAULTSWITH THE TRIM SYSTEM - SUSPECT CAUSED BY ICINGJun 26, 1997 · Beech B200C · Elevator Tab Control SystemSDR AU970833Rudder System · malfunction(AUS) RUDDER BOOST SYSTEM FAULTY - MAINTENANCE CHECKS OF SYSTEM COULD FIND NO FAULTSJun 12, 1997 · Beech B200C · Rudder Control SystemSDR AU970666Landing Gear · faulty(AUS) LANDING GEAR EXTENSION SYSTEM FAULTY - UNABLE TO MOVE EMERGENCY EXTENSION LEVER - LANDING GEAR 60AMP CIRCUIT BREAKER POPPED - CIRCUIT BREAKER RESET, EMERGENCY SYSTEM DISENGAGED AND LANDING GEAR EXTENDED NORMALLY - INSPECTION COULD FIND NO APPARENT DEFECTMay 31, 1997 · Beech B200C · Landing Gear Retraction/Extension SystemSDR AU970370Clip · cracked(AUS) CLIPS ATTACHING CHANNEL TO STRINGERS AT REAR PRESSURE BULKHEAD CRACKED ON LH SIDE - CLIP PNO 8050-30, PNO 8050-31, PNO 8050-32,PNO 8050-33 AND PN0 8050-36Mar 15, 1997 · Beech B200C · Fuselage Miscellaneous Structure
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