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 CA130403007Pin · migrated(CAN) AFTER PIN MIGRATION AND FAILURE OF ANOTHER COMPANY ACFT, PLATES WERE INSPECTED FOR PIN MIGRATION. LOWER FORWARD PIN WAS FOUND TO BE MOVING AND HAD PARTIALLY DISLODGED. PIN WAS REINSTALLED AND STAKED INTO PLACE WITH NO FURTHER COMPLICATIONS. THERE WAS Mar 28, 2013 · Beech B200 · Passenger/Crew DoorsSDR CA130325024Pin · migrated(CAN) LOUD HISSING FROM CABIN AREA THROUGH 18,000 FT ALTITUDE, FOLLOWED BY A BANG. RAPID DEPRESSURIZATION OCCURRED, OXYGEN MASKS DEPLOYED, EMERGENCY DESCENT CARRIED OUT. INITIALLY THOUGHT TO BE DUE TO A SMALL CUT IN THE CABIN DOOR SEAL, THE SEAL WAS CHANGED,Mar 24, 2013 · Beech B200 · Passenger Oxygen SystemSDR CA130402013Combustion Liner · damaged(CAN) DURING A ROUTINE HOT SECTION INSPECTION A COMBUSTION LINER WAS ORDERED, THEY PROVIDED A COMBUSTION LINER VIA A THIRD PARTY VENDOR. THE HOT SECTION WAS RE-ASSEMBLED AND BROUGHT OUTSIDE FOR GROUND RUNS, IT WAS IMMEDIATELY NOTED THAT THE ENGINE DID NOT MAKMar 22, 2013 · Beech B200 · Turbine Engine Combustion SectionSDR CIEA201303260003Access Door · inoperativeON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. THE ALT WARN ANNUNCIATOR DID NOT ILLUMINATE AND THE PAX O2 MASKS DID NOT Mar 22, 2013 · N203LG · Beech B200 · Passenger Oxygen SystemSDR CIEA201303260002Warning Switch · inaccurateON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. THE ALT WARN ANNUNCIATOR DID NOT ILLUMINATE AND THE PAX O2 MASKS DID NOT DMar 22, 2013 · N203LG · Beech B200 · Cabin Pressure Control SystemSDR CIEA201303260001Controller · erraticON DESCENT FROM FL250, CABIN PRESSURE SPIKED TO 12500, CABIN LIGHTS ILLUMINATED AND NO SMOKING/SEATBELT SIGNS ILLUMINATED. POWER LEVERS WERE AT IDLE DUE TO TURBULENCE. ALTITUDE WARN ANNUNCIATOR DID NOT ILLUMINATE AND PAX O2 MASKS DID NOT DEPLOY. WHEN POWERMar 22, 2013 · N203LG · Beech B200 · Cabin Pressure ControllerSDR CA130321007Pump · leaking(CAN) DURING SCHEDULED MAINTENANCE, AME NOTICED THAT THERE WAS FUEL LEAKING FROM THE BODY OF THE LOW PRESSURE FUEL PUMP. THE PUMP WAS REMOVED, SERVICEABLE PUMP WAS INSTALLED AND ACFT GROUND RUN SERVICEABLE.Mar 19, 2013 · Beech B200 · Engine Fuel PumpSDR CA130405004Adf · malfunctioned(CAN) ON APPROACH IT WAS NOTED BY THE CREW THAT THE ADF BECAME UNRESPONSIVE, FURTHER INSPECTION BY THE CREW INDICATED THAT THE CIRCUIT BREAKER HAD POPPED FOR THE ADF SYSTEM. MAINTENANCE REPLACED THE ADF BOX AND THE SYSTEM TESTED SERVICEABLE.Mar 18, 2013 · Beech B200 · Automatic Direction Finder (ADF) SystemSDR CA130315006Hose · ruptured(CAN) DURING NORMAL POST FLIGHT INSPECTION PROCEDURE, IT WAS NOTED THAT THERE WAS A SMALL HOLE IN THE OUTSIDE FIRE SLEEVE. UPON TESTING IT WAS SHOWN THAT THE INNER HOSE LINER WAS LEAKING AS WELL. HOSE DOES NOT APPEAR TO HAVE BEEN PHYSICALLY DAMAGED SO ASSUMEMar 13, 2013 · Beech B200 · Landing Gear Brake SystemSDR CA130315002Hose · leaking(CAN) AS THE ACFT WAS BEING PULLED OUT OF THE HANGAR, THE PILOTS ARMED THE OXYGEN SYSTEM. SHORTLY AFTER ARMING THE SYS, THE CAPTAIN HEARD A LOUD HISSING NOISE COMING FROM BEHIND THE SIDEWALL. THE ACFT WAS BROUGHT BACK INTO THE HANGAR FOR MAINTENANCE TO INSPEMar 12, 2013 · Beech B200 · Crew Oxygen SystemSDR CA130318004Engine · malfunctioned(CAN) SHORTLY AFTER T/O, A LOUD NOISE WAS HEARD FOLLOWED BY A POWER LOSS AND BURNED OIL ODOR IN THE CABIN. THE ENGINE WAS SECURED AND THE ACFT RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. NO OTHER INFO IS AVAILABLE. THMar 8, 2013 · Beech B200 · Engine (Turbine/Turboprop)SDR 2013FA0000130Cable · out of rigRUDDER TRAVEL LIMITED BY RUDDER BOOST CABLE BEFORE CONTACTING LIMIT STOP. RE-RIGGED BOOST CABLE, CHECKED RIG AND TRAVELS IAW MM AND FOUND WITHIN LIMITS WITHOUT ANY FURTHER ADJUSTMENTS. RUDDER SEEMED TO HAVE POSITIVE STOP AND HAD ALMOST FULL TRAVEL. CLOSE EXFeb 27, 2013 · N716AV · Beech B200 · Rudder Tab Control SystemSDR CA130226004Bolt · corroded(CAN) ON INSPECTION, MAINTENANCE NOTICED THAT CENTER BOLT ON NOSE GEAR DRAG BRACE WOULD NOT ROTATE WHEN TRYING TO GREASE. BOLT WAS LOOSENED AND STILL WOULD NOT ROTATE. BOLT WAS REMOVED, BUSHINGS WERE FOUND TO BE SEIZED ON TO THE BOLT. NEW BOLT/BUSHINGS INSTAFeb 25, 2013 · Beech B200 · Nose/Tail Landing GearSDR CA130402011Altimeter · malfunctioned(CAN) ON CLIMBOUT FROM CFX4 THE CREW NOTICED THAT THE ALTITUDE CAPTURE DID NOT WORK AT THE PLANED ALTITUDE. FURTHER INVESTIGATION REVEALED THAT THE PRE-SELECT WAS FLAGGED. MAINTENANCE REPLACED THE UNIT WITH NEW AND THE SYS GROUND FUNCTION CHECKED SERVICEABLEFeb 18, 2013 · Beech B200 · Altimeter, Barometric/EncoderSDR CA130215002Pcb · failed(CAN) ON APPROACH, 5 MIN BACK, TO LAND, CREW NOTICED SOME SPARKS AND SMOKE COMING FROM RT C/B PANEL. C/B FOR PANEL LIGHTING POPPED AND SPARKS QUIT. CREW LANDED ACFT, AFTER SHUTDOWN INVESTIGATED PROBLEM AND CALLED MAINTENANCE. AME REMOVED C/B PANEL AND FOUND Feb 12, 2013 · Beech B200 · Light System WiringSDR O9IA20130210002Heater · contaminatedACFT WAS AT TOP OF DESCENT, NOTICED A BURNING ODOR AND A LIGHT SHEEN OF SMOKE IN THE CABIN. PERFORMED EMERGENCY PROTOCOL FOR CABIN SMOKE AND LANDED WITHOUT INCIDENT. FOUND NO ELECTRICAL ANOMOLIES WITH EITHER THE ACFT OR ANY OF THE MEDICAL EQUIPMENT ON BOARFeb 10, 2013 · N546LM · Beech B200 · Heating SystemSDR O9IA20130210001Fire Detector · false activationMASTER WARNING AND LT ENGINE FIRE ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF ROLL AND RETURNED TO HANGAR. TROUBLESHOOTING REVEALED FAULTY OPTICAL FIRE DETECTOR. REPLACED FAULTY DETECTOR, OPS CHECKS NORMAL.Feb 10, 2013 · N546LM · Beech B200 · Fire DetectionSDR CA130211009Windshield · cracked(CAN) IN CRUISE, ENROUTE, PILOT HEARD A CRACKING NOISE, LOOKED UP AND NOTICED SEVERAL SPIDER CRACKS IN THE CAPTAINS WINDSHIELD. THE APPROPRIATE ACTIONS IAW THE ABNORMAL CHECKLIST FOR THE ACFT WERE CARRIED OUT AND THE ACFT LANDED UNEVENTFULLY. WINDSHIELD WAS IFeb 7, 2013 · Beech B200 · Flight Compartment WindowsSDR CA130405010Lock · defective(CAN) ON A ROUTINE MEDEVAC FLIGHT, THE CAPTAIN PROCEEDED WITH THE ENGINE STARTS WHILE THE CO-PILOT SECURED THE DOOR AND CABIN FOR FLIGHT. THE CREW NOTICED THEY HAD A DOOR LIGHT WARNING ON PRE TAXI CHECKS, THE ACFT WAS SHUTDOWN AND THE FLIGHT CANCELLED. MAINTFeb 6, 2013 · Beech B200 · Passenger/Crew DoorsSDR CA130212017Engine · malfunctioned(CAN) DURING THE DESCENT AT 20K FT, THE PILOT REPORTED A HIGH FUEL FLOW AND TORQUE FLUCTUATIONS. THEY FLEW TO A LOWER ALTITUDE TO ELIMINATE A POSSIBLE ICING CONDITION WITHOUT CHANGE. THEY DIVERTED THE FLIGHT WHERE A UNEVENTFUL LANDING WAS PERFORMED. DURING Feb 5, 2013 · Beech B200 · Engine (Turbine/Turboprop)SDR O9IA020313Clevis Pin · failedCLIMBING THROUGH ABOUT 23,000 FT, FLIGHT CREW HEARD A LOUD POP FOLLOWED IMMEDIATELY BY A LOSS OF CABIN PRESSURE. THE FLIGHT CREW IMMEDIATELY IMPLEMENTED THE EMERGENCY PROTOCOL FOR LOSS OF CABIN PRESSURE AN STARTED A DESCENT BACK TO DEPARTURE. THE MEDICAL CREFeb 3, 2013 · N546LM · Beech B200 · Passenger/Crew DoorsSDR CA130130003Arm · broken(CAN) DURING GROUND RUNS, THE AME NOTICED THAT PILOT`S RT RUDDER PEDAL WAS LOOSE. ACFT WAS TAKEN BACK TO THE HANGAR AND PROBLEM WAS INVESTIGATED. MAINTENANCE FOUND THAT THE ARM FOR THE RT RUDDER PEDAL HAD BROKEN AT THE TOP ATTACH FOR THE RUDDER PEDAL. RUDDERJan 29, 2013 · Beech B200 · Rudder Control SystemSDR HSRR2013FA0000061Retainer · brokenDURING TAXI OUT FOR A TEST FLIGHT, PILOT REPORTED THE STEERING PULLING HARD TO THE RIGHT REQUIRING EXTREME BRAKING TO KEEP THE ACFT STRAIGHT. INSPECTION IN MX DISCOVERED THE RETAINER IN THE END OF THE STEERING BARREL HAD BROKEN CAUSING THE CONTENTS OF THE BARJan 27, 2013 · N791DC · Beech B200 · Landing Gear Steering SystemSDR CA130118013Tire · bulged(CAN) DURING MAINTENANCE DAILY INSPECTION, THE NR 1 TIRE WAS NOTED TO HAVE A LARGE BULGE IN THE OTBD RIB. AFTER ALLOWING TIRE TO COOL, TIRE WAS DEFLATED AND REMOVED FROM WHEEL. TIRE APPEARS TO HAVE A TREAD SEPARATION FROM THE CORDS FOR ABOUT 6". TREAD WEAR IJan 17, 2013 · Beech B200 · TireSDR CA130403003Anti-Ice Valve · intermittent(CAN) AFTER LANDING AND SHUTTING DOWN THE CREW NOTICED AN ACCUMULATION OF ICE ON THE HORIZONTAL STABILIZER DE-ICE BOOTS. MAINTENANCE FOUND AN INTERMITTENT DISTRIBUTOR VALVE AS THE CAUSE, THE VALVE WAS REPLACED WITH NEW AND THE SYS WAS GROUND FUNCTION CHECKED Jan 15, 2013 · Beech B200 · Airfoil Anti/De-ice SystemSDR DJX2013F00001Rivet · looseRIVETS LOOSE, HOLDING INBD ATTACH BELLCRANK LEVER TO TORQUE TUBE. BELLCRANK LEVER HAS PLAY TO TORQUE TUBE.Jan 11, 2013 · N948CE · Beech B200 · Elevator Control SystemSDR CA130117006Engine · fluctuates(CAN) DURING REVENUE FLIGHT, THE ENGINE FUEL FLOW AND THE TORQUE WERE FLUCTUATING. THE PILOT ELECTED TO FOLLOW THE EMERGENCY PROCEDURE AND SECURED THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED.Jan 2, 2013 · Beech B200 · Engine (Turbine/Turboprop)SDR VQMA20121229001Landing Gear · collapsedON APPROACH, ACTIVATED GEAR DOWN CYCLE, DISCOVERED THAT THE TWO MAIN GEARS DID EXTEND AND LOCK, NOSE GEAR HAD NOT FULLY EXTENDED OR LOCKED INTO ITS CORRECT POSITION. ASCERTAINED THE PROBLEM COULD NOT BE FIXED IN FLIGHT, IT WAS DECIDED TO DIVERT FOR A LANDINGDec 29, 2012 · N918TC · Beech B200 · Nose/Tail Landing GearSDR CA121204010O-Ring · failed(CAN) NR 4 BRAKE ASSY HAD BEEN REPLACED THE DAY PRIOR TO THIS FAILURE, BOTH BRAKES BLED AND TESTED. LINING CONDITIONING WAS CARRIED OUT ON NEW BRAKE INSTALL. ON THE FIRST LANDING, PILOT NOTED SOFT BRAKES RT SIDE REQUIRING PUMPING. AFTER TAXI IT WAS NOTED CONDec 4, 2012 · Beech B200 · Landing Gear Brake SystemSDR CA121212010O-Ring · leaking(CAN) OIL WAS LEAKING OUT FROM THE PROP AND GETTING THE DE-ICE BRUSHES WET. WE REMOVED THE PROP AND SENT IT IN FOR REPAIR. WHEN THEY DISSASEMBLED IT THEY FOUND AN O-RING THAT HAD BEEN DAMAGED IN ASSY.Nov 19, 2012 · Beech B200 · Propeller AssemblySDR CA121120013Line · leaking(CAN) ON ENGINE SHUTDOWN RAMP PERSONNEL NOTICED A MIST COMING FROM THE LT ENGINE. MAINTENANCE BROUGHT THE AIRPLANE INTO THE HANGAR AND STARTED TO TROUBLESHOOT THE PROBLEM. WITH THE ACFT FUEL BOOST PUMP SELECTED ON, A MIST OF FUEL WAS NOTICED COMING FROM A FUENov 15, 2012 · Beech B200 · Engine Fuel DistributionSDR CA121114009Elbow · defective(CAN) THE NOSE GEAR ACTUATOR DOWN PORT FITTING, PN AN 837-6 WAS NOT PENETRATING THE NOSE GEAR ACTUATOR FITTING BOSS FAR ENOUGH TO ALLOW PROPER SEATING OF PACKING PN MS28778-6. THE FITTING, REDUNDANT END THAT ENTERS THE ACTUATOR BOSS WAS SHORTENED TO ALLOW ANONov 13, 2012 · Beech B200 · Landing Gear ActuatorSDR CA121109003Vane · burned(CAN) UPON A ROUTINE SCHEDULED HOT SECTION INSPECTION ON ENGINE SN 94208 IT WAS NOTED THAT THE PT VANE HAD SEVERE BURN THROUGH AND CRACKING ON THE BOTTOM 6 O`CLOCK POSITION. THIS IS VERY COMMON ON PT6A-42 ENGINES AND A HOT SECTION WEEK SPOT. YOU TYPICALLY JUNov 8, 2012 · Beech B200 · Turbine SectionSDR CA121106011Pcb · burned(CAN) CREW REPORTED PLASTIC BURNING ODOR IN FLIGHT. MAINTENANCE FOUND PILOT`S LOWER EDGE LIGHTED PANEL PRINTED CIRCUIT BOARD BURNED AT THE AFT LOWER SIDE WITH EVIDENCE OF MELTED PLASTIC AND PANEL CIRCUITS. NEW PANEL ON ORDER.Nov 6, 2012 · Beech B200 · Light System WiringSDR CA121102003Indicator · malfunctioned(CAN) AFTER LANDING AND UNLOADING THE AIRCRAFT, THE CREW DURING THE TAXI FOR DEPARTURE NOTICED THAT THE COPILOT`S ATTITUDE INDICATOR HAD TOPPLED AND WOULD NOT ERECT. CREW TAXIED BACK TO PARKING AND NOTIFIED MAINTENANCE. THE INDICATOR WAS OVERHAULED FEBRUARY 8,Oct 29, 2012 · Beech B200 · Attitude Gyro and Indicating SystemSDR CA121025010Line · ruptured(CAN) ON A ROUTINE, THE CREW HAD A A BLEED AIR FAIL LIGHT ILLUMINATE IN FLIGHT, THE ACFT CONTINUED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A BRAKE DE-ICE LINE HAD RUPTURED AND MELTED THE WARNING TUBE. THE HOSE WAS REPLACED WITHOUT FURTHER INCIDENT.Oct 24, 2012 · Beech B200 · Bleed Air Indicating SystemSDR CA121119002Engine · power loss(CAN) DURING ROTATION, THE NR 2 ENGINE LOST POWER. THE CREW ABORTED THE T/O AND SET THE ACFT BACK ON THE RUNWAY BUT THEY WERE UNABLE TO STOP BEFORE EXITING THE END, ROLLING DOWN AN EMBANKMENT AND COMING TO REST APPROXIMATELY 100 FT FROM THE RUNWAY THRESHOLD. Oct 20, 2012 · Beech B200 · Engine (Turbine/Turboprop)SDR CA121019013Detector · contaminated(CAN) THE RT ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF, NO OTHER INDICATORS OF A FIRE WERE PRESENT. AFTER LANDING, THE RT ENGINE COWLINGS WERE REMOVED AND THE ENGINE NACELLE INSPECTED. THERE NO EVIDENCE OF FIRE WAS WITHIN THE NACELLE. THE FIRE DEOct 18, 2012 · Beech B200 · Fire DetectionSDR G1IA20121018001Downlock Switch · sticksON APPROACH INTO BRW THE PILOTS SELECTED GEAR DOWN AND THE RIGHT GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AND THE RED IN-TRANSIT LIGHT WAS ILLUMINATED AND IF POWER WAS REDUCED THE GEAR WARNING HORN WOULD SOUND. THE PILOTS PUMPED THE GEAR DOWN AND THE SAOct 17, 2012 · N6728H · Beech B200 · Landing Gear Position and WarningSDR CA121009013Windshield · cracked(CAN) ACFT WAS IN LEVEL FLIGHT THE LT WINDSHIELD OUTER PANE CRACKED. THE ACFT RETURNED TO BASE. THE WINDSHIELD WAS REPLACED.Oct 4, 2012 · Beech B200 · Flight Compartment WindowsSDR CA121025008Battery · shorted(CAN) AFTER START IT WAS NOTED THAT THE RT GENERATOR HAD A 80 PERCENT LOAD. THE CREW SHUTDOWN AND CONTACTED MAINTENANCE, IT WAS DISCOVERED THAT THE BATTERY HAD SHORTED OUT INTERNALLY. THE BATTERY WAS REPLACED AND THE ACFT WAS STARTED WITHOUT FURTHER INCIDENTSep 24, 2012 · Beech B200 · Battery/Charger SystemSDR CA120905007Lever · out of rig(CAN) LEVER ASSY FOUND TO HAVE ARM AT INCORRECT ANGLE. THIS CAUSED THE CLEVIS FORK TO CONTACT THE ARM WHEN THE LEVER WAS MOVED, EVENTUALLY BENDING THE FORWARD UPPER DOOR HOOK PUSH PULL TUBE. DOOR RIGGING WAS STILL ABLE TO BE ACCOMPLISHED AND PUSH PULL TUBE Aug 30, 2012 · Beech B200 · Passenger/Crew DoorsSDR CA121009001Valve · leaking(CAN) CONDITIONS OF FLIGHT: CLEAR DAY ON CLIMBOUT THROUGH 10,000 FEET, RT BLEED AIR FAIL LIGHT CAME ON, PILOT TURNED RT BLEED AIR AND ENVIRONMENTAL AIR OFF AND PROCEEDED WITH CHECKLIST PROCEDURES. RT BRAKE DEVICE VALVE STUCK PARTLY OPEN CAUSING FAILURE OF BLEAug 28, 2012 · Beech B200 · Compressor Bleed ValveSDR CA120917007Heat Exchanger · malfunctioned(CAN) DURING TAXI PRIOR TO T/O, AS THE PILOT APPLIED POWER TO BOTH ENGINES, ONE DID NOT RESPOND AND IS REPORTED TO HAVE ROLLED BACK TO SUB IDLE OR MIN FLOW. THE ACFT RETURNED TO BASE WHERE TROUBLESHOOTING LED TO THE REPLACEMENT OF A FAULTY FUEL-OIL HEAT EXCHAug 28, 2012 · Beech B200 · Fuel HeaterSDR CA120925003Controller · malfunctioned(CAN) ON DESCENT WITH WINDSHIELD HEAT SELECTED ON, THE ACFT HAD CLEARED ICING SO SYSTEM WAS THEN TURNED OFF. THROUGH 24,000 FT, A SHORT TIME LATER, ICE WAS ENCOUNTERED AND SYS WAS TURNED BACK ON. SHORTLY THEREAFTER, THE CENTER HIGH ELEMENT PANEL AREA CRACKEAug 27, 2012 · Beech B200 · Windshield/Door Rain/Ice RemovalSDR CA120823010Clevis · cracked(CAN) ACFT IN FOR ROUTINE PHASE 4 INSPECTION. DURING THE PHASE 4 INSPECTIONS, THE LANDING GEAR ACTUATOR CLEVISES WERE REMOVED FOR NDT MAG PARTICLE INSPECTION, AS PART OF A IN-HOUSE INSPECTION FLEET CAMPAIGN. THE ACTUATOR CLEVISES WERE SENT FOR NDT MAG PARTIAug 23, 2012 · Beech B200 · Landing Gear ActuatorSDR CA120822017Seal · malfunctioned(CAN) ON AUGUST 17, 2012, ACFT WAS ON DEPARTURE AND AT FL 20 A LOUD WHISTLING SOUND WAS HEARD FROM THE MAIN CABIN DOOR. THE PILOT FLYING, ELECTED TO RETURN TO DEPARTURE FOR MAINTENANCE TO CHECK THE PROBLEM. THE TUBE FOR THE CABIN DOOR SEAL WAS FOUND NOT SEAAug 17, 2012 · Beech B200 · Passenger/Crew DoorsSDR CA120918022Nut · missing(CAN) PROPELLER WAS IN SHOP FOR OVERHAUL. 1 BETA RING NUT WAS MISSING FROM ASSY. 2 REMAINING BETA RING NUTS WERE LOOSE AND BACKED OFF FROM THE BETA RING. SPINNER BACKPLATE HAD SEVERAL VERY LOOSE NUTS AND WAS MISSING 1 NUT. SPINNER MOUNTING PLATE HOLES WEREAug 10, 2012 · Beech B200 · Propeller AssemblySDR CA120811004Processor · failed(CAN) ON A ROUTINE FLIGHT, THROUGH THE CLIMBOUT THE RT ELECTRONIC HEADING SITUATIONAL INDICATOR DISPLAYED A FAILED FLAG BUT SEEMED TO FUNCTION NORMALLY. THE CREW CONTINUED WITHOUT INCIDENT, MAINTENANCE DISCOVERED A FAILED DATA PROCESSOR UNIT, THE UNIT WAS REPAug 3, 2012 · Beech B200 · Attitude and Direction Data SystemSDR CA120811003Adc · malfunctioned(CAN) ON A ROUTINE FLIGHT, THE CREW NOTICED THE LT ALTIMETER UNSERVICEABLE, STUCK IN THE DESCENT. THE RT SYSTEM WAS USED TO CONTINUE THE DECENT AND THE FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A FAULTY AIR DATA COMPUTER, THE COMPUTER WAS REPAug 1, 2012 · Beech B200 · Air Data Computer
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