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 CA150714008Gyro · faulty(CAN) ON APPROACH, THE CREW NOTED THAT THE HSI WAS STICKING ON PREVIOUS HEADINGS IN BOTH SLAVE & FREE MODES. THE ACFT WAS SELECTED TO GPS RNAV FOR THE REMAINDER OF THE APPROACH & THE ACFT LANDED WITHOUT DIFFICULTY. IT WAS FOUND TO BE THE GYRO AS THE FAULT, IJul 12, 2015 · Beech B200 · Directional Gyro and Indicating SystemSDR CA150710021Actuator · worn(CAN) DURING A PHASE INSPECTION, ALL THE FLAP ACTUATORS WHERE REPLACED DUE TO EXCESSIVE WEAR. UPON RIGGING THE FLAPS A LARGE BANG WAS HEARD FROM THE LT OTBD FLAP. THE FLAP FLEX CABLE HAD SNAPPED DURING THE FLAP DOWN TEST. AN INVESTIGATION REVEALED THAT THE Jul 9, 2015 · Beech B200 · Trailing Edge Flap ActuatorSDR USAR201507130001Structure · cracked(00166) FATIGUE CRACK IN ENTRY DOOR SILL CLOSURE UPPER AFT CORNER. CRACK MEASURES .75".Jul 6, 2015 · Beech B200 · Fuselage Main, StructureSDR CA151215013Fuel Control · malfunctioned(CAN) THE AIRCRAFT WAS IN LEVEL FLIGHT AT FL 280. THE RIGHT HAND ENGINE TORQUE FLUCTUATION WAS NOTED WHICH LED UP TO AN ENGINE FLAME OUT. DURING THE PROCESS TO SECURE THE ENGINE, ENGINE POWER WAS REGAINED. THE CREW ELECTED TO RETURN TO THE MAIN BASE OF OPERATIJul 3, 2015 · Beech B200 · Fuel Control/Turbine EnginesSDR CA150720005Fuel Control · malfunctioned(CAN) THE AIRCRAFT WAS IN LEVEL AT FL 280. THE RT TORQUE FLUCTUATION WAS NOTED WHICH LED UP TO AN ENGINE FLAME OUT . DURING THE PROCESS TO SECURE THE ENGINE , ENGINE POWER WAS REGAINED . THE CREW ELECTED TO RETURN TO THE MAIN BASE OF OPERATION DURING THE DECENJul 3, 2015 · Beech B200 · Fuel Control/Turbine EnginesSDR CA150702008Cover · broken(CAN) DURING FLIGHT THE COVER ON THE RT UPPER WING BOLT FITTING PEELED BACK. IT DID NOT SEPARATE FROM THE AIRCRAFT. THERE ARE 4 COVERS ON THESE AIRCRAFT AND ARE PRONE TO DEPARTING THE AIRCRAFT IN FLIGHT.Jun 30, 2015 · Beech B200 · Wing Miscellaneous StructureSDR CA150617003Tire · flat(CAN) ON THE TAXI IT WAS DISCOVERED A FLAT TIRE HAD OCCURRED DURING LANDING. THE ACFT WAS ABLE TO MANEUVER UNDER ITS OWN POWER & WAS TAXIED BACK TO THE HANGAR UNEVENTFUL. REPLACED THE WHEEL ASSEMBLY & INSPECTED THE BRAKE SYS FOR DEFECTS. NO DEFECTS WHERE FOJun 15, 2015 · Beech B200 · TireSDR 2015FA0000282Compressor · seizedAIR CONDITIONER SYS INOPERATIVE WITH COMPRESSOR SEIZED AND DRIVE BELT BURNED OFF. FOUND HALF OF THE BEARING BALLS MISSING FROM THE DRIVE BEARING. THESE ARE CAPTURED BEARINGS AND CAGED. THE BEARING BALLS SEEM TO HAVE NEVER BEEN INSTALLED AT MFG. THE OPERATIJun 4, 2015 · N187JP · Beech B200 · Cabin Cooling SystemSDR CA150523001Blade · damaged(CAN) ON A ROUTINE HOT SECTION INSPECTION IT WAS FOUND THAT 1 COMPRESSOR TURBINE BLADE WAS MISSING A PIECE. IT WAS FOUND THE BLADE LOSS WAS FROM METAL FATIGUE OF THE BLADES AND NOT FROM FOD. THE BLADES WERE ALL REPLACED WITH NEW.May 20, 2015 · Beech B200 · Turbine SectionSDR CA150521003Duct · cracked(CAN) DURING PHASE 3 INSPECTIONS, THE NR 2 ENGINE LOWER FOWARD COWLING, HEATED AIR INLET "HOT-LIP" AFT OVERBOARD VENT DUCT FOUND CRACKED AROUND WELDING AND LARGE HOLEM MATERIAL MISSING. THIS ACFT HAS THE BUTTERFIELD FLOW-THROUGH EXHAUST STC SA2905NM EMBODIED OMay 20, 2015 · Beech B200 · Air Intake Anti/De-Ice SystemSDR CA150419003Support · misinstalled(CAN) RESTRICTOR SUPPORT ASSEMBLY APPEARS TO HAVE BEEN INSTALL 180 DEGREES OUT OF THE CORRECT ORIENTATION IN THE NLG TRUNION ALLOWING THE NOSE GEAR STRAIGHTENER ROLLER ASSY TO BE INSTALLED IN THE INCORRECT POSITION CAUSING DAMAGE TO THE NOSE WHEEL STRAIGHTENERApr 15, 2015 · Beech B200 · Nose/Tail Landing GearSDR CA150324007Door Frame · cracked(CAN) DURING PHASE 3 INSPECTIONS, ACA FOUND EMERGENCY EXIT LOWER FWD CORNER CRACKED, ONE INCH LONG RADIATING FROM CORNER EDGE GOING AFT.Mar 24, 2015 · Beech B200 · Fuselage Main, StructureSDR CA150320003Screw · wrong part(CAN) CHECKING SB 57-4144, ALL THE SCREWS WERE REMOVED AND FOUND MANY WERE NOT THE CORRECT LENGTH. ALL SCREWS WERE REPLACED WITH NEW ONES IAW SB 57-4144.Mar 18, 2015 · Beech B200 · Wing StructureSDR CA150320002Bolt · corroded(CAN) WHILE CHECKING COMMUNIQUE 2015-01-ATA27, IT WAS NOTICED THAT THE BOLT WAS BADLY CORRODED. A NEW BOLT WAS INSTALLED.Mar 18, 2015 · Beech B200 · Flight Control SystemSDR CA150312007Screw · wrong part(CAN) CHECKING SB 57-4144, ALL THE SCREWS WERE REMOVED AND FOUND MANY WERE NOT THE CORRECT LENGTH. ALL SCREWS WERE REPLACED WITH NEW ONES IAW SB 57-4144.Mar 12, 2015 · Beech B200 · AileronsSDR CA150312006Bolt · loose(CAN) WHILE CHECKING COMMUNIQUE 2015-01-ATA27 IT, WAS NOTICED THAT THE BOLTS HOLDING THE RUDDER HORN WERE LOOSE. BECAUSE THEY HAD BEEN LOOSE FOR SOME THE BOLT HAD WORE, 3 NEW BOLTS WERE INSTALLED AND TIGHTENED.Mar 12, 2015 · Beech B200 · Rudder StructureSDR G1IA20150311001Engine · malfunctionedWHILE ON FLIGHT, IN VMC CONDITIONS AT APPROX 0620 AST FL 270 & AT MOUNTAIN INTERSECTION, EXPERIENCED MECHANICAL IRREGULARITIES OF THE RT ENG. INITIALLY THERE WAS A SLOW FLUCTUATION OF TQ, N1 & FF, JUST SUBSEQUENT TO ENCOUNTERING SOME MILD MOUNTAIN WAVE TURBULMar 6, 2015 · N411WA · Beech B200 · Engine (Turbine/Turboprop)SDR CA150310009Engine · malfunctioned(CAN) THE CREW NOTIFIED MAINTENANCE THAT AN ODOR WAS COMING INTO THE ACFT FROM THE RT ENGINE WHEN THE BLEED VALVE WAS ON. MAINTENANCE SUSPECTED A BURNED BLEED AIR GASKET ON THE ENGINE SINCE A NEW GASKET HAD JUST BEEN INSTALLED PRIOR AT THE PHASE INSPECTION. Mar 4, 2015 · Beech B200 · Engine (Turbine/Turboprop)SDR CA150309006Bearing · seized(CAN) WHILE CHECKING COMMUNIQUE 2015-01-ATA27 IT WAS NOTICED THAT THE BOLT WAS BADLY CORRODED AND THE BEARING WAS SEIZED. A NEW BOLT AND BEARING WAS INSTALLED.Mar 4, 2015 · Beech B200 · Flight Control SystemSDR PAIR20150605S2599Spar Cap · corrodedDURING SCHEDULED 12 MONTH INSPECTION OF HORIZONTAL STABILIZER AS REQUIRED BY ACFT AIRWORTHINESS LIMITATIONS, FOUND LT HORIZONTAL STABILIZER AFT SPAR LOWER CAP WITH AN AREA OF PITTING CORROSION APPROXIMATELY 3" IN LENGTH APPROXIMATELY 2 FT FROM INBD END. INSTAMar 2, 2015 · N28KM · Beech B200 · Horizontal Stabilizer, Spar/RibSDR CA150323016Indicator · malfunctioned(CAN) HORIZON REF INDICATOR WAS LAGGING. UNIT REMOVED AND O/H. FOUND MULTIPLE BEARINGS REQUIRED REPLACEMENT.Feb 3, 2015 · Beech B200 · Attitude and Direction Data SystemSDR 2015FA0000021Diode · failedLOSS OF POWER TO LEFT NR 1 BUSS FEEDER DUE TO FAILURE OF RECTIFIER DIODE CR1 IN THE DUAL BUSS DIODE ASSEMBLY.Jan 10, 2015 · N65TW · Beech B200 · Electrical Power System WiringSDR CA150105011Rib · cracked(CAN) DURING PHASE 2 INSPECTIONS, ON THE RT AILERON CENTRE HINGE CUT-OUT, THE I/B LEADING EDGE RIB ASSY, FOUND CRACK RADIATING FROM RIVET.Jan 5, 2015 · Beech B200 · AileronsSDR CA150105010Skin · cracked(CAN) DURING PHASE 2 INSPECTIONS, ON THE LT O/B WING UPPER SKIN AT APPROX WS 149.735 AND 3" AFT OF FWD SPAR, FOUND 1" CRACKING AROUND BLIND HOLE FASTENER.Jan 5, 2015 · Beech B200 · Wing, Plate/SkinSDR G1IA20150107001Fire Detector · faultyWHILE ON A MEDEVAC FLIGHT LT ENG FIRE LIGHT CAME ON, THE INDICATIONS VARIED FROM FLICKERING RAPIDLY TO HOLDING STEADY FOR A BIT. LASTED NO MORE THAN 30 SECONDS, PROBABLY LESS, THEN WENT OUT. VISUALLY INSPECTED LT ENG, WHILE FLYING NOTICED NOTHING ABNORMAL, ALJan 4, 2015 · N6728H · Beech B200 · Fire DetectionSDR CA150421006Gasket · broken(CAN) DURING TROUBLESHOOTING AN AVIONICS/BLEED AIR PROBLEM, TEST AIR PRESSURE WAS INTRODUCED TO THE SYSTEM. A VERY LOUD RUSHING OF AIR WAS NOTED COMING FROM THE ENGINE AREA. IT WAS DISCOVERED THAT THE GASKET HAD BLOWN OUT OF THE BLEED AIR FLOW CONTROL VALVE.Nov 27, 2014 · Beech B200 · Pneumatic Distribution SystemSDR CA141103015Engine · unknown(CAN) DURING TAKEOFF THE PILOT RADIOED ENGINE PROBLEM. UPON RETURN TO THE AIRPORT, THE AIRPLANE IMPACTED AN AIRPORT BUILDING LOCATED ABOUT 1775 FEET (540 M) LEFT OF THE RUNWAY.Oct 30, 2014 · Beech B200 · Engine (Turbine/Turboprop)SDR CA141104009Ahrs · malfunctioned(CAN) - ON DEPARTURE OPERATING ON AHRS NR 1, "RED" ROLL AND PITCH ANNUNCIATORS ON BOTH PILOT AND COPILOT PFD`S. NR 1 PFD THEN SWITCHED TO AHRS NR 2. THEN BOTH PFD`S TUMBLED. AFTER 30 SECONDS BOTH PFD`S TURNED "BLACK" WITH "RED" X`S THROUGH THE EHSI AND EADIOct 29, 2014 · Beech B200 · Attitude and Direction Data SystemSDR CA141103024Hinge · cracked(CAN) ON INSPECTION IT WAS NOTICED THAT THE RH ICE VANE HINGE WAS FOUND CRACKED ABOUT 4 INCHES LONG. THE HINGE WAS REPLACED WITH A NEW ONE. THE LH ICE VANE HINGE WAS ALSO FOUND CRACKED ABOUT 2 INCHES. IT WAS ALSO CHANGED.Oct 29, 2014 · Beech B200 · Air Intake Anti/De-Ice SystemSDR CA141030004Relay · failed(CAN) ON APPROACH, CREW SELECTED LANDING GEAR DOWN, GEAR DID NOT EXTEND. CREW NOTICED THAT LANDING GEAR CONTROL CIRCUIT BREAKER HAD TRIPPED, CIRCUIT BREAKER WAS RESET AND GEAR SELECTED CIRCUIT BREAKER TRIPPED AGAIN. CREW NOTIFIED THE TOWER AND DID A MISSED APOct 28, 2014 · Beech B200 · Landing Gear Retraction/Extension SystemSDR CA141026001Motor · failed(CAN) AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GEAR SYS 2 AMP CIRCUIT BREAKER FOUND TRIPPED. CIRCUIT BREAKER WAS NOT ATTEMPTED TO RESET. ACFT RETURNED TO BASE FOR MAINTENANCE TO TROUBLESHOOT. ACFT JACKED. CIRCUIT BREAKER PUSHED IN, LANDING GEAR SYSTOct 23, 2014 · Beech B200 · Landing Gear Retraction/Extension SystemSDR CA141020009Skin · cracked(CAN) DURING PHASE 2 INSPECTIONS: L/H O/B WING AT APPROX WS147.735, A 1.5 INCH CRACK FOUND AT FASTENER IN THE UPPER SKIN SURFACE ON AFT-SIDE OF FWD SPAR. THERE IS A TRIANGULAR DOUBLER SKIN I/B FROM CRACK. NOT ABLE TO FIND P/N OF THE DOUBLER SKIN IN BE20 IPC, Oct 18, 2014 · Beech B200 · Wing, Plate/SkinSDR CA141028010Seal · damaged(CAN) DURING AN INSPECTION IT WAS NOTICE THERE WAS A LOT OF OIL COMING FROM THE STARTER GENERATOR DRAIN. THE STARTER WAS REMOVED AND IT WAS NOTICE THAT CARBON HAD GOT BETWEEN THE SEAL AND THE SHAFT CAUSING THE SEAL TO PILE UP AND WEAR A CURVE IN THE SHAFT AND Oct 8, 2014 · Beech B200 · Turbine Engine Oil SystemSDR CA141024013Engine · flamed out(CAN) DURING APPROACH THE ENGINE HAD A FLAME OUT. TORQUE FLUCTUATION AND FUEL FLOW FLUCTUATION WAS NOTICED 4 TIMES BEFORE THE IFSD. 1ST TIME AT FL 170, POWER FLUCTUATION, 4TH TIME AT FL 080, IFSD. FSR WILL BE ONSITE TO DO THE GROUND RUN ON 7TH OCTOBER.Oct 5, 2014 · Beech B200 · Engine (Turbine/Turboprop)SDR CIER2014092601Skin · crackedREMOVED PREVIOUS REPAIR STRAP THAT WAS INBD OF CRACKED SKIN AT RIVET HOLE & FABRICATED NEW EXTENDED REPAIR STRAP TO INCORPORATE THREE EXTRA RIVET HOLES. THE NEW REPAIR STRIP IS MADE USING 0.050 INCH THICK 2024-T3 ALUMINUM. THE REPAIR STRIP & LE SKIN WERE PRESep 26, 2014 · N5ST · Beech B200 · Wing, Plate/SkinSDR CA141104010Ahrs · failed(CAN) ERRONEOUS ATTITUDE INDICATIONS IN FLIGHT. INSTALLED NEW NR 1 AND NR 2, GRS 7800 AHRS UNITS. ACFT RETURNED TO SERVICE.Sep 21, 2014 · Beech B200 · Attitude and Direction Data SystemSDR CA140923010Bayonet · broken(CAN) DURING GROUND HANDLING, CABIN DOOR WOULD NOT REOPEN AFTER ACFT HAD BEEN TOWED. MAINTENANCE FOUND THE UPPER AFT BAYONET BROKEN, WITH THE BLADE STILL ENGAGED IN THE DOOR FRAME. THIS IS A CHAPTER 4 CYCLE LIMITED ITEM WITH 3851 CYCLES SINCE NEW, 5000 CYCLESep 21, 2014 · Beech B200 · Passenger/Crew DoorsSDR CA150323015Adc · faulted(CAN) LT ALTIMETER INTERMITTENT. FOUND ADC PN: 622-4365-221 TO BE FAULTY.Aug 25, 2014 · Beech B200 · Altimeter, Barometric/EncoderSDR MGOR2014082759615Turbine Blades · separatedPILOT REPORTED 60 DEGREE TEMP SPLIT AT IDLE. BORESCOPE OF ENGINE REVEALED COMPRESSOR TURBINE BLADE SEPARATION.Aug 25, 2014 · N89WA · Beech B200 · Turbine SectionSDR 7EMA20140815003Fuel Line · chafedFUEL LINE FROM RT OTBD FUEL TANK TO RT NACELLE TANK CHAFING WHERE IT PASSES THROUGH LIGHTNING HOLE IN FWD SPAR.Aug 15, 2014 · N53AR · Beech B200 · Aircraft Fuel Distribution SystemSDR 7EMA20140815002Fuel Line · chafedFUEL LINE FROM LT OTBD FUEL TANK TO LT NACELLE TANK CHAFING WHERE IT PASSES THROUGH LIGHTNING HOLE IN FWD SPAR.Aug 15, 2014 · N53AR · Beech B200 · Aircraft Fuel Distribution SystemSDR CA140929010Engine · surges(CAN) NR 1 ENGINE SURGED 2 TO 3 TIME. PILOTS CONFIRMED WITH ENGINE GAUGES AND VISUALLY DETERMINE ENGINE HAD SHUT DOWN AND THEY PROCEEDED WITH EMERGENCY PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT.Aug 8, 2014 · Beech B200 · Engine (Turbine/Turboprop)SDR CA150323011Probe · failed(CAN) LT AUX FUEL PROBE FOUND UNSERVICEABLE CAUSING THE LT FUEL GAUGE TO BE UNSERVICEABLE.Jul 20, 2014 · Beech B200 · Fuel Indicating SystemSDR CA140721009Line · damaged(CAN) PILOTS REPORTED ENGINE BECAME NON RESPONSIVE TO PLA INPUT DURING TAXI. THE COMPRESSOR SPEED (NG) ROLLED BACK ALL THE WAY DOWN TO 42 PERCENT. DURING THE ON GROUND TROUBLESHOOTING, THE PROBLEM WAS RESOLVED WHEN PLA LINES WERE REPLACED. THE ACFT RETURNED Jul 8, 2014 · Beech B200 · Fuel Control/Turbine EnginesSDR CA140701014Engine · malfunctioned(CAN) WHEN APPROACHING AIRPORT, THE PILOT HEARD A LOUD BANG ON LT ENGINE, ASSOCIATED WITH ACFT TENDENCY TO THE LT. LEFT ENGINE LOST POWER AND ITT INCREASED. THE PILOT ELECTED TO SHUTDOWN ENGINE AND PERFORM A SINGLE ENGINE LANDING. TROUBLESHOOTING ONGOING.Jun 26, 2014 · Beech B200 · Engine (Turbine/Turboprop)SDR CA140701008Engine · unknown(CAN) CUSTOMER REPORTED AN IFSD OF THE LT ENGINE DURING CLIMB THROUGH 3500FT, INITIAL REPORT IS THAT THE ENGINE MADE A LOUD NOISE, FOLLOWED BY A VERY SHORT SPIKE IN FUEL FLOW, WF, AND SUDDEN DROP IN TORQUE, TQ, AND COMPRESSOR SPED, NG. THE ITT INCREASED TO A MJun 26, 2014 · Beech B200 · Engine (Turbine/Turboprop)SDR ZP7A20140623001Battery · failedGENERATORS FAILED SHORTLY AFTER TAKEOFF. STARTED LOSING ELECTRICAL POWER BY EVIDENCE OF THE AIR CONDITIONING FANS TURNING OFF, GETTING FLAGS ON THE EFIS SCREENS, AND EVENTUALLY LOSING ALL AVIONICS POWER. HAD TO MANUALLY PUMP GEAR DOWN FOR LANDING. AFTER AN UJun 23, 2014 · N805AH · Beech B200 · Battery/Charger SystemSDR CA140630018Warning Message · activated(CAN) DURING REVENUE FLIGHT, THE PILOT NOTICED A HIGH OIL TEMPERATURE DURING CLIMB. THEY REDUCED THE ENGINE POWER TO MAINTAIN THE OIL TEMPERATURE WITHIN LIMITS. THE CREW ELECTED TO RETURN TO HOME BASE AND LANDED UNEVENTFULLY. TROUBLESHOOTING ONGOING.Jun 20, 2014 · Beech B200 · Turbine Engine Oil SystemSDR CA140620015Torque Tube · cracked(CAN) DURING PHASE 4 INSPECTIONS, FOUND APPROX 1.5" RADIAL CRACK IN THE WELDING OF THE TORQUE TUBE TO THE ATTACH BRACKET. (TC# 20140620015)Jun 19, 2014 · Beech B200 · Rudder StructureSDR CA140620014Shim · damaged(CAN) DURING PHASE 4 INSPECTIONS, AME FOUND THE NLG SIMMY DAMPNER ATTACH BRACKET ARM HAD SHEARED THE HEADS OFF OF THE TWO ATTACH BOLTS. THE ARM WAS ABLE TO MOVE FROM SIDE TO SIDE AT ITS ATTACH AREA ON THE NLG TRUNNION, WHILE THE NLG WAS TURNED FROM LEFT TO RIGJun 19, 2014 · Beech B200 · Nose/Tail Landing Gear
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