Beechcraft B200GT

Service difficulty reports · 30

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 = 'B200GT'
  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 2026FA0000898Structure · damagedNUMEROUS OCCURRENCES OF FAILED BUCK RIVET INSTALLATION IN CRITICAL STRUCTURAL AREAS DISCOVERED. CRACKED TOPCOAT, MISSING TOPCOAT, AND FRETTING RESIDUE DEPOSITED BY WORKING RIVETS DISCOVERED ALONG LEFT CENTER WING MAIN AND AFT SPAR CAP, LEFT FUSELAGE F.S. 116, Oct 22, 2026 · Beech B200GT · Standard Practices/StructuresSDR 2026F00233Latch · unlatchedAS THE AIRCRAFT TAXIED ONTO THE RUNWAY TO DEPART KBIL FOR KGCC, THE MED CREW NOTICED A LATCH ON THE LEFT WING LOCKER NOT LATCHED. THE FLIGHT CREW TAXIED OFF THE RUNWAY TO THE RUNUP AREA WHERE THEY GOT OUT AND CLOSED THE LATCH. THE AIRCRAFT THEN TAXIED BACK TO Oct 14, 2026 · N680TW · Beech B200GT · Cargo/Baggage DoorsSDR QMLA2026101320078Synchrophaser · out of adjustLEFT PROP LEVER ACTING LIKE IT WAS HOOKED UP BACKWARDS. PUSHING THE LEVER FORWARD INCREASED RPM, AND VICE VERSA. ADJUSTED LT ENGINE PROPELLER SYNCHROPHASER MAGNETIC PICKUPS IAW KING AIR B200GT AMM 61-23-01. PERFORMED REQUIRED FUNCTIONAL GROUND CHECKS. NO FAULTOct 12, 2026 · N912SM · Beech B200GT · Engine (Reciprocating)SDR 2026FA0000737Evaporator · leakingWATER DISCOVERED POOLING IN LOW AREAS UNDER FLOOR LEADING TO WETTING OF INSULATION, CLOGGING OF EVAPORATOR DRAINS, AND PREMATURE FAILURE OF LOWER ANTI-COLLISION BEACON LIGHT DUE TO MOISTURE EXPOSURE AND CORROSION. CONDITION DISCOVERED ON FOUR DIFFERENT FLEET Sep 17, 2026 · Beech B200GT · Air Conditioning SystemSDR 2026FA0000632Landing Gear · malfunctionedUNSAFE NOSE LANDING GEAR IN APPROACH PATTERN; NO GREEN LIGHT, RED LIGHT IN HANDLE ON, WARNING HORN ON AT REDUCED N1, “TOO LOW GEAR” AURAL TAWS ALERT. EXECUTED MANUAL GEAR EXTENSION, NO CHANGE. VISUAL FROM TOWER AND ANOTHER AIRCRAFT REPORTED THAT NOSE GEAR APPEAug 7, 2026 · Beech B200GT · Nose/Tail Landing GearSDR 2026F00168Fuel Feed · failedCREW NOTED A TRANSIENT FUEL FLOW INDICATION ERROR AS TAKEOFF CLEARANCE WAS RECEIVED. WHILE STATIONARY WITH INCREASED POWER, THE INDICATOR ERROR PERSISTED AND THE CREW REQUESTED TO RETURN TO PARKING. ATC CANCELLED TAKEOFF CLEARANCE AND CREW TAXIED CLEAR OF THE Jul 31, 2026 · N981HC · Beech B200GT · Aircraft Fuel Distribution SystemSDR NI6R202608260068Strut · wornRIGHT MLG SHOCK STRUT HAS DAMAGE FROM UPLOCK SWITCH, CHROME CHIPPED OFF TO BARE METAL. CHROME ON MLG STRUT ASSEMBLY HAS A DIVOT AT THE LOCATION WHERE UPLOCK PUSH BUTTON APPLIES FORCE TO PLUNGE THE BUTTON FOR GEAR UPLOCK NOTIFICATION. DIVOT BEYOND LIMITS PER CJul 29, 2026 · N115Z · Beech B200GT · Main Landing Gear Strut/Axle/TruckSDR NI6R202608260067Autothrottle Sys · disconnectedL1 AUTO THROTTLE INOP. LT CONTROL ROD FOUND NOT CONNECTED. HARDWARE DISCOVERED LOOSE AND SITTING AT LOW POINT OF BAY USING A BORESCOPE AND RETRIEVAL SUCCESSFUL USING MECHANICAL FINGERS. UNIT ORIGINALLY INSTALLED BY TEXTRON BY STC SA00400B0Jul 29, 2026 · N115Z · Beech B200GT · Auto Throttle SystemSDR 2026FA0000537Autothrottle Sys · abnormalPILOTS HAVE REPORTED MULTIPLE INSTANCES OF AUTOTHROTTLE INDUCED WARNING/RED TORQUE INDICATIONS OCCURRING DURING TAKEOFF, GO-AROUND, AND CLIMB PHASES OF FLIGHT ON SIX DIFFERENT AIRCRAFT (S/N BY-472 AND UP). THREE INSTANCES WERE SEVERE ENOUGH TO ACTIVATE THE MASJun 23, 2026 · Beech B200GT · Auto Throttle SystemSDR 2025FA0000821Autothrottle Sys · disconnectedINNOVATIVE SOLUTIONS AND SUPPORT (IS&S) SA 00400BO AUTOMATIC THROTTLE ASSEMBLY (P/N 9B-89005-3). LINKAGE PUSHROD FOUND DETACHED AT CONNECTION WITH ASSEMBLY'S LINEAR ACTUATOR; LINKAGE FAILED AT ACTUATOR ATTACHMENT POINT. LOOSE FOD DROPPED INTO COMPARTMENT (FASTDec 11, 2025 · Beech B200GT · Auto Throttle SystemSDR 2025F00230Brake · no discrepancyWHILE TAXIING OUT FOR AN AIR AMBULANCE FLIGHT, THE MED TEAM THOUGHT THEY OBSERVED SMOKE FROM THE LEFT MLG AREA. THE FLIGHT CREW RETURNED TO THE BLOCKS AND HAD MAINTENANCE INSPECT THE LEFT MAIN LANDING GEAR, WHEELS AND BRAKES. NO DEFECTS WERE FOUND. THE CREW ANSep 24, 2025 · N680TW · Beech B200GT · Landing Gear Brake SystemSDR 2025FA0000657Inlet Screen · corrodedDISCOVERED GALVANIC CORROSION COMMON TO THE ENGINE SHREDDER SCREEN PLATE (P/N 101-910049-107) ON THE LOWER AFT ENGINE COWLING WHERE THE CRES SHREDDER SCREEN IS SECURED. NO BARRIER APPLIED (I.E. ALODYNE PRIMER, OR SEALER) BETWEEN THE DISSIMILAR METEALS. THE CORSep 19, 2025 · Beech B200GT · Nacelle/Pylon, Main FrameSDR 2025FA0000560Wire Harness · improper stowMAINTENANCE HAS REPORTED OBSERVATIONS OF WIRING INSTALLATION DEFICIENCIES ON NEWLY RECEIVED ZERO-TIME AIRCRAFT (4 OF 18 AIRCRAFT INSPECTED). UNATTACHED ADHESIVE BACKED CABLE TIE MOUNTS, SHARP BEND RADIUS ALONG DATA AND RF CABLES, 180 DEGREE KINKS APPLIED TO DAAug 20, 2025 · Beech B200GT · Electrical Power System WiringSDR 2025FA0000539Receptacle · shortedEXTERNAL POWER RECEPTACLE POSITIVE AND NEGATIVE DC BUS BARS FOUND TOUCHING AT BACK OF RECEPTACLE. RECEPTACLE HAD SHORTED WHICH CAUSED GPU FAULT BLOCKING APPLICATION OF EXTERNAL POWER. PHOTOS AVAILABLE ON REQUEST.Aug 8, 2025 · Beech B200GT · Electrical Power SystemSDR 2025FA0000534Pcb · corrodedMOISTURE AND CORROSION DAMAGE ARE BEING FOUND ON CIRCUIT BOARDS FOLLOWING POSSIBLE WATER INTRUSION THROUGH UPPER WING SKIN ACCESS PANEL. TO DATE, 24 FUEL QUANTITY MATRIX BLOCKS AND 7 UNENCAPSULATED PCB BOARDS (P/N 101-361096-3) ACROSS 13 AIRCRAFT HAVE MALFUNCTAug 4, 2025 · Beech B200GT · Instrument System WiringSDR 2025FA0000469Beacon · failedON OCCASION, THE UPPER AND LOWER ANTICOLLISION BEACON LIGHTS HAVE FAILED (STOPPED FLASHING) AFTER FIRST ENGINE START USING BOTH 24V BATTERY POWER AND EXTERNAL 28V GPU POWER. SUSPECTED ROOT CAUSE IS LOW VOLTAGE ON THE DC BUS, INCURRED BY HIGH DC BUS LOADS EXPEJul 10, 2025 · Beech B200GT · Exterior LightingSDR 2025FA0000403Inlet Guide Vane · corrodedACCELERATED CORROSION DISCOVERED ON ENGINE INLET ANTI-ICE VANE, BY-471 (NEW 4/16/2024) THRU BY-488 (NEW 10/3/2024). PICTURES AVAILABLE UPON REQUEST.Jun 16, 2025 · Beech B200GT · Engine Anti-Icing SystemSDR 2025FA0000402Structure · corrodedACCELERATED CORROSION DISCOVERED ON HORIZONTAL STABILIZER; NEW AIRCRAFT DELIVERED 5/20/2024. 341.1 HOURS TIME SINCE NEW 484 TOTAL LANDINGS.Jun 16, 2025 · Beech B200GT · Horizontal Stabilizer StructureSDR 2025FA0000224Beacon · intermittentUPPER AND LOWER LED ANTICOLLISION BEACONS OCCASIONALLY CEASE OPERATING FOLLOWING BATTERY ENGINE START OR GPU ENGINE START. KING AIR MODEL B200GT, SERIAL BY-470 (BUNO 170744) AND ON. OPERATION MAY BE RESTORED BY CYCLING THE COCKPIT BEACON SWITCH (OFF AND BACK Mar 31, 2025 · Beech B200GT · Exterior LightingSDR QMLA2024100320128Feathering Sys · faultedDURING LANDING, THE RIGHT PROP ATTEMPTED TO FEATHER WITH THE AUTO FEATHER SYSTEM ON (AS THROTTLES WERE PULLED BACK FOR LANDING). PILOT SECURED THE AUTO FEATHER SYSTEM AND LANDED SAFELY. LOGBOOK ENTRY MADE AND TURNED AIRCRAFT OVER TO MAINT. ADJUSTED AUTO FEAOct 2, 2024 · N912SM · Beech B200GT · Propeller Feathering/ReversingSDR CA190807006Nut · missing(CAN) WHILE CONDUCTING A PHASE 4 INSPECTION ON THE EMPENNAGE SECTION OF C-XXXX, ONE OF THE ENGINEERS OPENED A BUTTON SIZE COVER (APPROXIMATELY 1 AND A HALF INCH DIAMETER) TO HAVE A LOOK AT THE ELEVATOR BELLCRANK. AFTER REMOVING THE COVER, HE FOUND THAT THERE WAug 2, 2019 · Beech B200GT · Elevator Control SystemSDR CA190424027Downlock Switch · failed(CAN) NOSE LANDING GEAR DOWN/LOCK INDICATION ILLUMINATED THEN WENT OUT WHILE ON APPROACH.AIRCRAFT ABORTED APPROACH AND WENT AROUND LIGHT ILLUMINATED AGAIN WHILE AIRCRAFT WAS ON APPROACH AND LANDED SAFELY. UPON ARRIVAL AT THE HANGAR THE LIGHT WAS AGAIN OUT. AIRApr 18, 2019 · Beech B200GT · Landing Gear Position and WarningSDR CA190320025Bolt · sheared(CAN) PILOT REPORTED AFT UPPER DOOR PIN SHEARED, AIRSTAIR DOOR DISASSEMBLED AND INSPECTED ,ALL FOUR BAYONETS REPLACED WITH LATCH BOLT KIT,AIRSTAIR DOOR FUNCTIONED CHECKED AND INSPECTED SERVICEABLE (TC# 20190320025)Mar 20, 2019 · Beech B200GT · Passenger/Crew DoorsSDR CA180808026Compressor · leaking(CAN) AIR CONDITIONING COMPRESSOR WEEPING OIL FROM AFT SEAL. ADDITIONAL AIRCRAFT IN THE COMPANY FLEET HAVE ENCOUNTERED THIS SAME PART NUMBER OF COMPRESSOR TO HAVE FAILED. THE SYSTEM WAS DEFERRED IN ACCORDANCE WITH COMPANY PROCEDURES FOR PARTS ON ORDER. (TC# Jul 29, 2018 · Beech B200GT · Cabin Compressor SystemSDR CA180808021Display · inoperative(CAN) ROCKWELL COLLINS PROLINE FUSION EQUIPPED AIRCRAFT, ADAPTIVE FLIGHT DISPLAY AFD-3700. DEFECT REPORTED AS CHECK MAINTENANCE CAS MESSAGE GNSS-1 FAILURE FLAG CAME ON. TROUBLESHOOTING INCLUDED REMOVAL AND REPLACEMENT OF AFD WITH ORIGINAL UNIT (NOT EXCHANGEDJul 25, 2018 · Beech B200GT · Flight Management Computing Hardware SystemSDR 2017FA0000316Wire Harness · openWHEN AIRCRAFT IS FULL OF FUEL, AIRCRAFT HAS A DIFFERENTIAL QUANTITY INDICATION OF 200 POUNDS. THE INDICATOR GOES FROM 100 TO ZERO POUNDS IN FLIGHT. TESTED SYSTEM AND FOUND INSULATION AND CAPACITY CHECK OK. OPENING UP INTEGRAL WING PANELS TO GAIN ACCESS TO PJul 5, 2017 · N925GA · Beech B200GT · Fuel System WiringSDR 2016F00199Wire · chafedAIRCRAFT DEPARTING SGR, PILOT CALLED FOR "GEAR UP", GEAR RESPONDED FOR A FEW SECONDS, THEN HALTED IN MID RETRACT. PILOT ASKED TOWER TO VERIFY, WHO SAID "NOSE WAS UP AND MAINS ONLY PARTIALLY UP". PILOT TRIED SEVERAL TIMES WITH NO FURTHER RESPONSE FROM LANDINGOct 11, 2016 · N785AM · Beech B200GT · Landing Gear System WiringSDR 2016FA0000399Fuel Cell · leakingNEW FUEL CELL INSTALLED, FOUND TO LEAK AT OTBD SEAM. FUEL CELL WAS REPLACED WITH REPAIRED FUEL CELL.Aug 31, 2016 · N1459W · Beech B200GT · Fuel StorageSDR CA130614006Engine · shutdown(CAN) SHORTLY AFTER DEPARTURE, THE ACFT CRASHED IN A RESIDENTIAL AREA. POST CRASH FIRE OCCURRED, SETTING 2 HOUSES ON FIRE AND DAMAGING A 3RD. NO ONE ON THE GROUND WAS HURT. ON SITE WRECKAGE DID NOT SHOW ANY OBVIOUS CAUSES FOR THE ACCIDENT AND AS SUCH, THE Jun 10, 2013 · Beech B200GT · Engine (Turbine/Turboprop)SDR CA121114005Fairing · cracked(CAN) 1.5" CRACK FOUND IN FLAP FAIRING SKIN ON RT WING JUST OTBD OF OTBD FLAP SCREWJACK ON UPPER PORTION OF SKIN STRUCTURE. MFG CONSULTED AND REPLACED WITH NEW.Oct 20, 2012 · Beech B200GT · Trailing Edge Flaps
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