# Service difficulty reports: Textron B200GT

A list on [Textron B200GT](https://openairdocs.org/model/textron-b200gt.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2026FA0000898](https://openairdocs.org/sdr/2026FA0000898.md): Structure · damaged · Oct 22, 2026 · Beech B200GT · Standard Practices/Structures
  > NUMEROUS 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,
- [SDR 2026F00233](https://openairdocs.org/sdr/2026F00233.md): Latch · unlatched · Oct 14, 2026 · N680TW · Beech B200GT · Cargo/Baggage Doors
  > AS 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
- [SDR QMLA2026101320078](https://openairdocs.org/sdr/QMLA2026101320078.md): Synchrophaser · out of adjust · Oct 12, 2026 · N912SM · Beech B200GT · Engine (Reciprocating)
  > LEFT 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 FAULT
- [SDR 2026FA0000737](https://openairdocs.org/sdr/2026FA0000737.md): Evaporator · leaking · Sep 17, 2026 · Beech B200GT · Air Conditioning System
  > WATER 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
- [SDR 2026FA0000632](https://openairdocs.org/sdr/2026FA0000632.md): Landing Gear · malfunctioned · Aug 7, 2026 · Beech B200GT · Nose/Tail Landing Gear
  > UNSAFE 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 APPE
- [SDR 2026F00168](https://openairdocs.org/sdr/2026F00168.md): Fuel Feed · failed · Jul 31, 2026 · N981HC · Beech B200GT · Aircraft Fuel Distribution System
  > CREW 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
- [SDR NI6R202608260068](https://openairdocs.org/sdr/NI6R202608260068.md): Strut · worn · Jul 29, 2026 · N115Z · Beech B200GT · Main Landing Gear Strut/Axle/Truck
  > RIGHT 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 C
- [SDR NI6R202608260067](https://openairdocs.org/sdr/NI6R202608260067.md): Autothrottle Sys · disconnected · Jul 29, 2026 · N115Z · Beech B200GT · Auto Throttle System
  > L1 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 SA00400B0
- [SDR 2026FA0000537](https://openairdocs.org/sdr/2026FA0000537.md): Autothrottle Sys · abnormal · Jun 23, 2026 · Beech B200GT · Auto Throttle System
  > PILOTS 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 MAS
- [SDR 2025FA0000821](https://openairdocs.org/sdr/2025FA0000821.md): Autothrottle Sys · disconnected · Dec 11, 2025 · Beech B200GT · Auto Throttle System
  > INNOVATIVE 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 (FAST
- [SDR 2025F00230](https://openairdocs.org/sdr/2025F00230.md): Brake · no discrepancy · Sep 24, 2025 · N680TW · Beech B200GT · Landing Gear Brake System
  > WHILE 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 AN
- [SDR 2025FA0000657](https://openairdocs.org/sdr/2025FA0000657.md): Inlet Screen · corroded · Sep 19, 2025 · Beech B200GT · Nacelle/Pylon, Main Frame
  > DISCOVERED 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 COR
- [SDR 2025FA0000560](https://openairdocs.org/sdr/2025FA0000560.md): Wire Harness · improper stow · Aug 20, 2025 · Beech B200GT · Electrical Power System Wiring
  > MAINTENANCE 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 DA
- [SDR 2025FA0000539](https://openairdocs.org/sdr/2025FA0000539.md): Receptacle · shorted · Aug 8, 2025 · Beech B200GT · Electrical Power System
  > EXTERNAL 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.
- [SDR 2025FA0000534](https://openairdocs.org/sdr/2025FA0000534.md): Pcb · corroded · Aug 4, 2025 · Beech B200GT · Instrument System Wiring
  > MOISTURE 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 MALFUNCT
- [SDR 2025FA0000469](https://openairdocs.org/sdr/2025FA0000469.md): Beacon · failed · Jul 10, 2025 · Beech B200GT · Exterior Lighting
  > ON 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 EXPE
- [SDR 2025FA0000403](https://openairdocs.org/sdr/2025FA0000403.md): Inlet Guide Vane · corroded · Jun 16, 2025 · Beech B200GT · Engine Anti-Icing System
  > ACCELERATED 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.
- [SDR 2025FA0000402](https://openairdocs.org/sdr/2025FA0000402.md): Structure · corroded · Jun 16, 2025 · Beech B200GT · Horizontal Stabilizer Structure
  > ACCELERATED CORROSION DISCOVERED ON HORIZONTAL STABILIZER; NEW AIRCRAFT DELIVERED 5/20/2024. 341.1 HOURS TIME SINCE NEW 484 TOTAL LANDINGS.
- [SDR 2025FA0000224](https://openairdocs.org/sdr/2025FA0000224.md): Beacon · intermittent · Mar 31, 2025 · Beech B200GT · Exterior Lighting
  > UPPER 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
- [SDR QMLA2024100320128](https://openairdocs.org/sdr/QMLA2024100320128.md): Feathering Sys · faulted · Oct 2, 2024 · N912SM · Beech B200GT · Propeller Feathering/Reversing
  > DURING 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 FEA
- [SDR CA190807006](https://openairdocs.org/sdr/CA190807006.md): Nut · missing · Aug 2, 2019 · Beech B200GT · Elevator Control System
  > (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 W
- [SDR CA190424027](https://openairdocs.org/sdr/CA190424027.md): Downlock Switch · failed · Apr 18, 2019 · Beech B200GT · Landing Gear Position and Warning
  > (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. AIR
- [SDR CA190320025](https://openairdocs.org/sdr/CA190320025.md): Bolt · sheared · Mar 20, 2019 · Beech B200GT · Passenger/Crew Doors
  > (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)
- [SDR CA180808026](https://openairdocs.org/sdr/CA180808026.md): Compressor · leaking · Jul 29, 2018 · Beech B200GT · Cabin Compressor System
  > (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#
- [SDR CA180808021](https://openairdocs.org/sdr/CA180808021.md): Display · inoperative · Jul 25, 2018 · Beech B200GT · Flight Management Computing Hardware System
  > (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 EXCHANGED
- [SDR 2017FA0000316](https://openairdocs.org/sdr/2017FA0000316.md): Wire Harness · open · Jul 5, 2017 · N925GA · Beech B200GT · Fuel System Wiring
  > WHEN 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 P
- [SDR 2016F00199](https://openairdocs.org/sdr/2016F00199.md): Wire · chafed · Oct 11, 2016 · N785AM · Beech B200GT · Landing Gear System Wiring
  > AIRCRAFT 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 LANDING
- [SDR 2016FA0000399](https://openairdocs.org/sdr/2016FA0000399.md): Fuel Cell · leaking · Aug 31, 2016 · N1459W · Beech B200GT · Fuel Storage
  > NEW FUEL CELL INSTALLED, FOUND TO LEAK AT OTBD SEAM. FUEL CELL WAS REPLACED WITH REPAIRED FUEL CELL.
- [SDR CA130614006](https://openairdocs.org/sdr/CA130614006.md): Engine · shutdown · Jun 10, 2013 · Beech B200GT · Engine (Turbine/Turboprop)
  > (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
- [SDR CA121114005](https://openairdocs.org/sdr/CA121114005.md): Fairing · cracked · Oct 20, 2012 · Beech B200GT · Trailing Edge Flaps
  > (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.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/textron-b200gt/reports

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