# Beechcraft B200

- Type: Aircraft model (FAA registry)
- Registry code: 4220036
- Manufacturer (registry): BEECHCRAFT CORP
- Model: B200
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 15
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 0
- Page: https://openairdocs.org/model/beechcraft-b200

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-05-17](https://openairdocs.org/ad/2021-05-17): NAVIGATION SYSTEM · Rockwell Collins FDSA-6500, CL-600-2B16 (CL-604), 525B and 7 more. Effective Apr 29, 2021
- [AD 2010-26-03](https://openairdocs.org/ad/2010-26-03): Ice and Rain Protection · Textron B200, B200GT, B300 and 1 more. Effective Dec 20, 2010
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-12-06](https://openairdocs.org/ad/2007-12-06): Flight controls · Textron B200, B200C, B300 and 2 more. Effective Jul 16, 2007
- [AD 2006-12-25](https://openairdocs.org/ad/2006-12-25): Actuator nut assembly · General Machine - Diecron Actuator nut assembly, 100, 200 and 15 more. Effective Jul 28, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-18](https://openairdocs.org/ad/2005-01-18): Fuselage stringers · Textron 200, 200C, 200CT and 24 more. Effective Mar 1, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005
- [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2003-13-16](https://openairdocs.org/ad/2003-13-16): Aft Pressure Bulkhead of Fuselage · Textron 100, 200, 200C and 33 more. Effective Aug 25, 2003
- [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003
- [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001
- [AD 2001-11-03](https://openairdocs.org/ad/2001-11-03): Blower Motor Circuit · Textron 1900D, 58, 58A and 5 more. Effective Jul 20, 2001
- [AD 99-18-15](https://openairdocs.org/ad/99-18-15): Landing Gear Emergency Hand Pumps · Textron 1900D, B200, B300 and 1 more. Effective Sep 27, 1999
- [AD 99-09-10](https://openairdocs.org/ad/99-09-10): Landing Gear Hand Pump · Textron 200CT, 300, A200CT (C-12D) and 19 more. Effective Jun 7, 1999
- [AD 99-09-15](https://openairdocs.org/ad/99-09-15): Flight Control Mechanism · Textron 1900D, 58, 58A and 5 more. Effective May 18, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-21-35](https://openairdocs.org/ad/98-21-35): Actuator Clevis Assembly in Main Landing Gear · Textron 200T, 300, A200CT (C-12D) and 15 more. Effective Nov 23, 1998
- [AD 98-10-05](https://openairdocs.org/ad/98-10-05): Engine Fire Detector System · Textron B200, B200C, B200C (C-12R) and 1 more. Effective Jun 27, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998
- [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997
- [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997
- [AD 96-09-13](https://openairdocs.org/ad/96-09-13): AFM - Icing · Textron 1900, 1900C, 1900D and 7 more. Effective Jun 11, 1996
- [AD 96-03-13](https://openairdocs.org/ad/96-03-13): Main Landing Gear Drag Leg Lock Link · Textron 100, 200, 200C and 24 more. Effective Apr 1, 1996
- [AD 95-13-03](https://openairdocs.org/ad/95-13-03): Electrical Landing Gear Motor · Textron 100, 200, 200C and 22 more. Effective Jul 28, 1995
- [AD 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994
- [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992
- [AD 92-10-12](https://openairdocs.org/ad/92-10-12): Engine Cowling Doors · Textron 200, 200C, 200CT and 18 more. Effective Jun 12, 1992
- [AD 92-06-11](https://openairdocs.org/ad/92-06-11): Autopilot/Flight Director System Wiring · Textron 1900C, 300, B200 and 2 more. Effective Mar 30, 1992
- [AD 91-12-11](https://openairdocs.org/ad/91-12-11): Side Windows · Textron 200, 200C, 200CT and 7 more. Effective Jul 15, 1991
- [AD 91-12-10](https://openairdocs.org/ad/91-12-10): Wing Spar Attachment · Textron 300, 300LW, B200 and 2 more. Effective Jul 15, 1991
- [AD 89-19-04 R1](https://openairdocs.org/ad/89-19-04-R1): Wing Fuel Bay Skin Panels · Textron 200, 200C, 200CT and 6 more. Effective Jul 9, 1990
- [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990
- [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987
- [AD 85-22-05](https://openairdocs.org/ad/85-22-05): Nuts and Bolts Replacement · Textron 100, 200, 200C and 60 more. Effective Nov 12, 1985
- [AD 83-07-14](https://openairdocs.org/ad/83-07-14): One-Ply Window Replacement · Textron 200, 200C, 200CT and 4 more. Effective Apr 18, 1983
- [AD 76-10-12](https://openairdocs.org/ad/76-10-12): Textron 214, B200 (propeller), R201 and 2 more. Effective Jun 2, 1976

Historical (superseded or no longer in force):

- [AD 2019-12-09](https://openairdocs.org/ad/2019-12-09) (historical): Navigation · Bombardier CL-600-2B16 (CL-604), Flight Display System Application FDSA-6500, 525B and 13 more. Effective Jul 23, 2019
- [AD 2008-07-10](https://openairdocs.org/ad/2008-07-10) (historical): Pneumatic supply tube · Hawker Beechcraft B200, B200GT, B300 and 1 more. Effective Apr 10, 2008
- [AD 2006-23-02](https://openairdocs.org/ad/2006-23-02) (historical): Flight controls for improper assembly or damage · Raytheon B200, B200C, B300 and 2 more. Effective Dec 13, 2006
- [AD 98-20-38](https://openairdocs.org/ad/98-20-38) (historical): AFM - Limitations - Icing · Raytheon 200 Model or Series (all), 200C, 200CT and 21 more. Effective Nov 4, 1998
- [AD 98-15-13](https://openairdocs.org/ad/98-15-13) (historical): Fuel Hose · Raytheon 100 Model or Series (all), 200 Model or Series (all), 200C and 32 more. Effective Aug 28, 1998
- [AD 96-17-10](https://openairdocs.org/ad/96-17-10) (historical): Outflow/Safety Valve · Raytheon 200 Model or Series (all), 2000, 300 and 5 more. Effective Sep 24, 1996
- [AD 93-25-07](https://openairdocs.org/ad/93-25-07) (historical): Fuselage Stringers · Raytheon 200 Model or Series (all), 200C, 200CT and 22 more. Effective Feb 15, 1994
- [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989

## Information bulletins (advisory) (2)

- [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage  Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012

## Registered aircraft

None registered with this model now.

## STCs approved for it (430, first 50)

- [STC SA00034IB](https://openairdocs.org/stc/SA00034IB): Installation/Upgrade of Sandel ST3400 Terrain Awareness Warning System with Enhanced Altitude 
     Accuracy. Maxcraft Avionics Ltd.
- [STC SA00044DE](https://openairdocs.org/stc/SA00044DE): Installation of nose compartment door ice shield.. Stevens Aviation, Inc
- [STC SA00061DE](https://openairdocs.org/stc/SA00061DE): Installation of Traffic Alert and Collision Avoidance System I (TCAS I) Model TCAS791/791A. Acron Aviation Inc.
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA00088DE-D](https://openairdocs.org/stc/SA00088DE-D): Nine-place seating configuration.. Air Methods Corporation
- [STC SA00095BO](https://openairdocs.org/stc/SA00095BO): Installation of Pratt & Whitney Engine Services, Inc. Twin Engine Aircraft Data Acquisition System ADAS/ADAS+ Upgrade, P/N TWIN-K-010,. Pratt & Whitney Engine Services Inc.
- [STC SA00099BO](https://openairdocs.org/stc/SA00099BO): Installation of a Universal Avionics Systems Corp. UNS-1K Flight Management System.. Pro Star Aviation, LLC
- [STC SA00110AT](https://openairdocs.org/stc/SA00110AT): Installation of a Marathon KSP 400 battery.. Aviall Services, Inc.
- [STC SA00116IB](https://openairdocs.org/stc/SA00116IB): Manufacturing of Lightweight Passenger Seats. Miccar Aerial Ltd.
- [STC SA00139WI](https://openairdocs.org/stc/SA00139WI): Installation of medical storage cabinet.. Textron Aviation Inc
- [STC SA00154DE](https://openairdocs.org/stc/SA00154DE): Installation of medical interior.. Mayo Aviation Inc
- [STC SA00157BO](https://openairdocs.org/stc/SA00157BO): Installation of Honeywell MK VI EGPWS Terrain Awareness and Warning System (TAWS) with optional Honeywell TRA-45 Terrain Display Unit/Radio Altitude Indicator.. Pro Star Aviation, LLC
- [STC SA00161BO (3 OF 3](https://openairdocs.org/stc/SA00161BO%20(3%20OF%203): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation
- [STC SA00165BO](https://openairdocs.org/stc/SA00165BO): Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.. Avidyne Corporation
- [STC SA00167WI](https://openairdocs.org/stc/SA00167WI): Installation of an AlliedSignal Avionics, Inc. (Sundstrand) Mark VI Ground Proximity Warning System.. Textron Aviation Inc
- [STC SA00183WI](https://openairdocs.org/stc/SA00183WI): Installation of overhead console cabinets.. LifePort LLC
- [STC SA00184LA](https://openairdocs.org/stc/SA00184LA): Installation of Alternate Main Landing Gear Tires, Michelin P/N 026-335-0.. Metrea Special Aerospace ISR Inc.
- [STC SA00227NY](https://openairdocs.org/stc/SA00227NY): Installation of Sky Harbour Aircraft Refinishing Ltd. Ice Damage Prevention Plates.. Sky Harbour Aircraft Refinishing
- [STC SA00243BO (4 OF 5)](https://openairdocs.org/stc/SA00243BO%20(4%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC
- [STC SA00273WI](https://openairdocs.org/stc/SA00273WI): Installation of Stretcher, Patient Loading, and Support system.. Lifeport Inc
- [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation
- [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number  700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation
- [STC SA00294BO](https://openairdocs.org/stc/SA00294BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC
- [STC SA00295BO](https://openairdocs.org/stc/SA00295BO): Installation of the Pratt & Whitney Engine Services ADASd. Pratt & Whitney Engine Services Inc.
- [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC
- [STC SA00335BO](https://openairdocs.org/stc/SA00335BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC
- [STC SA00336BO](https://openairdocs.org/stc/SA00336BO): Installation of a Thrane & Thrane AVIATOR 200 SwiftBroadband System. Pro Star Aviation, LLC
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA00367SE](https://openairdocs.org/stc/SA00367SE): Installation of a Nose Baggage Compartment on Beech KingAir Models.. Sierra Nevada Corporation/Integrated Mission Systems
- [STC SA00381NY](https://openairdocs.org/stc/SA00381NY): Installation of forward lower wing spar cap reinforcing kit.. SK Aircraft Company, Inc
- [STC SA00400BO](https://openairdocs.org/stc/SA00400BO): Installation of an Autothrottle System (ATS). Innovative Solutions & Support Inc
- [STC SA00404BO](https://openairdocs.org/stc/SA00404BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC
- [STC SA00415WI](https://openairdocs.org/stc/SA00415WI): Installation of a baggage door.. Avcon Industries Inc
- [STC SA00416BO](https://openairdocs.org/stc/SA00416BO): Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit. Outerlink Corporation
- [STC SA00453WI](https://openairdocs.org/stc/SA00453WI): Installation of a Lateral Tracking Seat Base.. Aviation Fabricators Inc
- [STC SA00504NY](https://openairdocs.org/stc/SA00504NY): Installation of Rosemount Aerospace, Inc. advisory ice detectors, P/N0871HL1 & 0871HT3.. Rosemount Aerospace Inc
- [STC SA00523SE](https://openairdocs.org/stc/SA00523SE): Replacement of certain BF Goodrich pneumatic deicer boots.. SMR Technologies
- [STC SA00558DE-D](https://openairdocs.org/stc/SA00558DE-D): Installation of a Pilot and Co-Pilot Digital Air Data Display Unit.. AeroMech Incorporated
- [STC SA00622WI](https://openairdocs.org/stc/SA00622WI): Shoulder harness anchor installation. Aviation Fabricators Inc
- [STC SA00635WI](https://openairdocs.org/stc/SA00635WI): Jump seat installation.. Aviation Fabricators Inc
- [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation.. Rockwell Collins Inc
- [STC SA00681WI-D](https://openairdocs.org/stc/SA00681WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Rockwell Collins Inc
- [STC SA00727AT-D](https://openairdocs.org/stc/SA00727AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing
- [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC
- [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc
- [STC SA00752SE](https://openairdocs.org/stc/SA00752SE): Installation of Raisbeck Enhanced Performance Leading Edge (SA3831NM), Dual Aft Body Strakes (SA3591NM), Ram Air recovery Systems (SA3366NM), High Flotation Gear Doors (SA4175NM) and Hartzel/Beechcraft Turbofan Propeller System. Raisbeck Engineering
- [STC SA00754CH](https://openairdocs.org/stc/SA00754CH): Installation of a Shadin ADC-2000fuel/Airdata System, p/n 962830AR-3-S.. Shadin Company Inc
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine

All 430: https://openairdocs.org/model/beechcraft-b200/stcs.md

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (830, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 55YR202610130001](https://openairdocs.org/sdr/55YR202610130001), Oct 5, 2026: STRUT. DAMAGED. CAME IN FOR PHASE MAINTENANCE, AND THE OPERATOR REQUESTED AN EARLY LANDING GEAR REPLACEMENT. THE LANDING GEAR WAS DUE SOON FOR REPLACEMENT, AND REPRESENTATIVES 
- [SDR O9IA202609140206](https://openairdocs.org/sdr/O9IA202609140206), Sep 14, 2026: UNKNOWN. SMOKE. PILOTS NOTED SMOKE IN THE COCKPIT. MEDICAL CREW ONBOARD CONFIRMED SMOKE IN THE CABIN. SMOKE WAS EMITTING FROM THE COPILOTS INSTRUMENT PANEL NEAR THE SIDEWALL. T
- [SDR G1IA20260821116](https://openairdocs.org/sdr/G1IA20260821116), Aug 21, 2026: SOCKET. BACKED OUT. SELECTED GEAR DOWN ON FINAL IN PAYA AND GEAR FAILED TO EXTEND. DID NOT LAND, DIVERTED TO PANC. EXTENDED GEAR MANUALLY AT PANC, GOT THREE GREEN AND LANDED.
- [SDR 55YR2026080400919](https://openairdocs.org/sdr/55YR2026080400919), Jul 31, 2026: ACTUATOR. CRACKED. ACFT IN FOR A PHASE 1 INSPECTION. GEAR SWINGS REQUIRED FOR PHASE AND MAINT PERFORMED. 10 SWINGS REQUIRED TO BLEED SYS AFTER OPENING LINES. 6 SWINGS WERE PERFORM
- [SDR 2026FA0000611](https://openairdocs.org/sdr/2026FA0000611), Jul 30, 2026: PIN. BROKEN. FLAP DRIVE PIN IN FLAP GEAR BOX WAS BROKEN IN 1/2 WHEN REMOVED FOR 1200 HR LUBRICATION
- [SDR 2026F00162](https://openairdocs.org/sdr/2026F00162), Jul 24, 2026: CLEVIS PIN. SHEARED. PIN ATTACHING FOWARD DOOR HOOK ON UPPER MAIN DOOR LOCKING MECHANISM SHEARED ALLOWING HOOK TO COME LOOSE ALLOWING ENOUGH MOVEMENT IN THE MAIN CABIN DOOR IN FLIGH
- [SDR GRTA20260715002](https://openairdocs.org/sdr/GRTA20260715002), Jul 1, 2026: ANGLE. CRACKED. LEFT MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED LEFT MLG ACTUATOR, ASSOCIATED PLUMBING/ELECTRICLA WIRING, AND LEFT MLG DRAG BRACE. REMOVED LH INBOARD
- [SDR GRTA20260715001](https://openairdocs.org/sdr/GRTA20260715001), Jul 1, 2026: ANGLE. CRACKED. RIGHT INBD MLG ACTUATOR SUPPORT BRACKET CRACKED. REMOVED RT MLG ACTUATOR, ASSOCIATED PLUMBING, ELECTRICLA WIRING, AND RT MLG DRAG BRACE. REMOVED RT INBD AND OTB
- [SDR TIMA202604297003](https://openairdocs.org/sdr/TIMA202604297003), Apr 28, 2026: INDICATION SYS. FAULTED. RIGHT LANDING GEAR DOWN LIGHT DIDN’T ILLUMINATE, APPROPRIATE CHECKLIST WAS PREFORMED, EMERGENCY GEAR EXTENSION WAS INEFFECTIVE AND THE AIRCRAFT WAS LANDED AS PR
- [SDR TIMA2026042900701](https://openairdocs.org/sdr/TIMA2026042900701), Apr 27, 2026: LANDING GEAR. FAULTED. ON DECENT WHEN GEAR WAS SELECTED DOWN ONLY THE NOSE AND LEFT GEAR DOWN LIGHTS ILLUMINATED, THE PRESS TO TEST WAS CHECKED AND THE BULB WAS NOT BURNT OUT SO ATC W
- [SDR 2026FA0000188](https://openairdocs.org/sdr/2026FA0000188), Mar 13, 2026: WINDSHIELD. CRACKED. DURING TAKEOFF FROM KBIL TO KHLN, THE CREW OBSERVED THE LEFT WINDSHIELD CRACK. THE CREW RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR 2026F00026](https://openairdocs.org/sdr/2026F00026), Mar 10, 2026: DOOR. NO DISCREPANCY. DURING A RETURN FLIGHT FROM KMLK TO KBIL, THE MED CREW NOTICED THAT THE LEFT WING LOCKER HAD OPENED. THE CREW CONTINUED TO KBIL AND LANDED WITHOUT INCIDENT. MAI
- [SDR G1IA2026012219103](https://openairdocs.org/sdr/G1IA2026012219103), Jan 19, 2026: DOWNLOCK SWITCH. FAILED. LANDING GEAR NOSE WHEEL DOWN LIGHT EXTINGUISHED ON SHORT FINAL IN KENAI. WENT MISSED, CYCLED THE GEAR TWICE, GOT THE LIGHT BACK, WHICH THEN EXTINGUISHED ON SHOR
- [SDR G1IA20250928098](https://openairdocs.org/sdr/G1IA20250928098), Sep 28, 2025: CHECK VALVE. FAULTED. DURING CRUISE LT FUEL PRESSURE LIGHT ILLUMINATED. LT FUEL FLOW GAUGE ERRATIC. TURNING ON LT STNDBY PUMP HAD NO EFFECT ON FUEL FLOW. LT ENG BEGAN SPOOLING DOWN O
- [SDR 2025FA0000639](https://openairdocs.org/sdr/2025FA0000639), Sep 11, 2025: CROSS TIE. CRACKED. DURING PHASE INSPECTION FOUND THE LEFT CROSS TIE AT FUSELAGE STATION 201.775 CRACKED IN HALF. CRACK RUNS HORIZONTAL AND GOES THROUGH A RIVET HOLE. CRACK IS LOCA
- [SDR ENHA 20250721001](https://openairdocs.org/sdr/ENHA%2020250721001), Jul 20, 2025: ANNUNCIATOR. ACTIVATED. LEFT ENGINE FIRE ANNUNCIATOR CAME ON IN FLIGHT. MECHANICS INSPECTED AND TESTED THE SYSTEM IAW THE KING AIR 200 MM SECTIONS 26-10-00 AND 26-10-01. ALL CHECKS WER
- [SDR JBZA20250714001](https://openairdocs.org/sdr/JBZA20250714001), Jul 9, 2025: ELEC CONNECTOR. LOOSE. DURING FLIGHT LEFT ENGINE FIRE WARNING LIGHT ERRATICALLY FLASHES. ELECTED TO PRECAUTIONARY LAND BACK TO BASE. MAINTENACE DISCOVERED LOOSE FIRE DETECTION AMPLIFI
- [SDR GRTA20250910001](https://openairdocs.org/sdr/GRTA20250910001), Jul 7, 2025: STIFFENER. CRACKED. WHILE PERFORMING THE AFT PRESSURE BULKHEAD INSPECTION FOUND A CRACK AT THE # 5 ZEE STIFFENER FROM THE TOP OF THE BULHEAD ON THE FWD SIDE OF THE BULKHEAD THE CRA
- [SDR O9IA202505270132](https://openairdocs.org/sdr/O9IA202505270132), May 27, 2025: FIRE WARNING. FALSE ACTIVATION. DEPARTING PANC. WHILE PASSING THRU FL310 THE LH ENG FIRE LIGHT ILLUMINATED. PILOT DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT. NO INDICATIONS OUTSIDE OF T
- [SDR G1IA20250127482](https://openairdocs.org/sdr/G1IA20250127482), Jan 24, 2025: SWITCH. FAILED. ONCE WERE ON VISUAL APPROACH IN ANCHORAGE, I SELECTED THE GEAR LEVER DOWN. THE PLANE'S NOSEWHEEL FAILED TO ILLUMINATE GREEN. AFTER VERIFYING THAT IT WASN'T A BU
- [SDR 2025FA0000053](https://openairdocs.org/sdr/2025FA0000053), Jan 24, 2025: INDICATOR. NO INDICATION. THE NOSEWHEEL GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE. THE ACTUAL NOSEWHEEL HAD COME DOWN AND LOCKED, BUT WITH NO INDICATION TO THE PILOT OF ITS STATUS, 
- [SDR ENHA2024F00292](https://openairdocs.org/sdr/ENHA2024F00292), Nov 19, 2024: BULKHEAD. CORRODED. DURING INSPECTION, THE AFT PRESSURE BULKHEAD SHOWED CORROSION ON THE AFT SIDE. THE CORROSION WAS BEYOND THE STRUCTURAL REPAIR MANUAL SO ENGINEERING WAS NEED AIN
- [SDR 2024FA0000823](https://openairdocs.org/sdr/2024FA0000823), Nov 5, 2024: WINDSHIELD. FRACTURED. AIRCRAFT WAS IN CRUISE FLIGHT AT 16,000 FT ENROUTE KBZN FROM KBIL WHEN THE RIGHT (COPILOT) WINDSHIELD SHATTERED. AT THAT TIME, THE FLIGHT CREW RETURNED TO KBIL 
- [SDR O9IA20241015530LM](https://openairdocs.org/sdr/O9IA20241015530LM), Oct 14, 2024: PRESSURE SWITCH. FAULTED. FROM PILOTS REPORT THRU PRISM SMS: IN CRUISE AT 28,000 FT LEFT HAND ENGINE SEEMED TO WANT TO GO INTO FEATHER. HAPPENED TWO TIMES. DID A PRECAUTIONARY LANDING IN
- [SDR J95A202410230001](https://openairdocs.org/sdr/J95A202410230001), Sep 24, 2024: LANDING GEAR. FAILED. WHEN PILOT CAME IN FOR LANDING, THE LANDING GEAR FAILED TO EXTEND. AFTER PERFORMING THE LANDING GEAR EMERGENCY EXTENTION PROCEDURE, THE NOSE LANDING GEAR FAILED
- [SDR 2025F00078](https://openairdocs.org/sdr/2025F00078), Aug 31, 2024: LANDING GEAR. INOPERATIVE. REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS PLACED IN THE DOWN POSITION ON APPROACH TO KPHX ON 8-31-2024 WITH A PATIENT ON BOARD. HE WE
- [SDR 2024F00167](https://openairdocs.org/sdr/2024F00167), Jul 10, 2024: FAN. SHORTED. CABIN ENECTRICAL SMELL WITH SOME SMOKE. UPON INVESTIGATION FOUND FORWARD CABIN DISTRUBTION FAN FAILURE.
- [SDR 2024FA0000463](https://openairdocs.org/sdr/2024FA0000463), Jun 24, 2024: HYDRAULIC SYSTEM. LOW QUANTITY. CREW RECCIVED A LOW HYDRALIC WARRNING LIGHT ON TAKE OFF AFTER PHASE INSPECTION. CREW ABORTED TAKEOFF TAXIED BACK TO MAINTENANCE. MAINTENANCE SERVICED HYDRALIC S
- [SDR 2024F00100](https://openairdocs.org/sdr/2024F00100), Mar 21, 2024: MOTOR. FAILED. DEPARTED KBIL ENROUTE KMSO. AFTER TAKEOFF THE CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT BEYOND THE APPROACH POSITION. THEY THEN RETURNED TO KBIL WITHOUT IN
- [SDR GRTA20240315004](https://openairdocs.org/sdr/GRTA20240315004), Mar 14, 2024: SKIN. CRACKED. BELLY SKIN CRACKED 3/8"AT APPROX FS 181.0 AT STRINGER 16. REPAIRED IAW KING AIR SIRM 20-10-16.
- [SDR GAYA2024031300002](https://openairdocs.org/sdr/GAYA2024031300002), Mar 12, 2024: LANDING GEAR. MALFUNCTIONED. PILOT REPORTED ON CLIMB JUST PRIOR TO LEVEL OFF HE SAW AN AMBER RA INOP ON THE PILOT PFD FOLLOWED BY PT TRIM AND AMBER INOP AP RED FAIL. THE RIGHT PFD WENT BLAN
- [SDR 2024F00053](https://openairdocs.org/sdr/2024F00053), Mar 7, 2024: HOSE. DETERIORATED. WHILE TAXIING OUT AT 0630 IN KBIL ENROUTE KMLS, PILOT REPORTED THAT LEFT AIRSPEED INDICATOR NEVER ROSE ABOVE 0. AVIONICS TROUBLESHOT AND FOUND A ROTTED HOSE TO 
- [SDR GRTA20240315003](https://openairdocs.org/sdr/GRTA20240315003), Mar 6, 2024: FRAME. CRACKED. FRAME CRACKED CENTER LINE ABOVE BELLY SKIN @ APPROXIMATE F.S. 167.625. REPAIRED IAW SIRM 20-10-34.
- [SDR GRTA20240315002](https://openairdocs.org/sdr/GRTA20240315002), Mar 6, 2024: FRAME. CRACKED. FRAME CRACKED AT FS 236.5 BETWEEN STRINGERS 12L AND 13L. REPAIRED IAW KING AIR SIRM 20-10-34.
- [SDR GRTA20240315001](https://openairdocs.org/sdr/GRTA20240315001), Mar 6, 2024: SKIN. CRACKED. BELLY SKIN CRACKED APPROX 3 1/2" ON FRAME AT FS 167.625 BETWEEN STRINGERS 15L AND 16. C/W SKIN DAMAGE REPAIR (PRESSURIZED AREA) COVER PATCH METHOD AND SHIM INST
- [SDR GRTA20240221001](https://openairdocs.org/sdr/GRTA20240221001), Feb 20, 2024: DOOR SEAL. DAMAGED. AFTER TAKE OFF FROM LAS VEGAS, NM, WE HAD A RAPID DECOMPRESSION AT FL260 WITH AIRFLOW HEARD AT THE CABIN DOOR FOLLOWED BY CABIN ALT HI ANNUNCIATOR AND MASTER WA
- [SDR G1IA20240215258](https://openairdocs.org/sdr/G1IA20240215258), Feb 12, 2024: CIRCUIT BREAKER. TRIPPED. LANDING GEAR CIRCUIT BREAKER ACTIVATED ON APPROACH, GEAR WAS PUMPED DOWN MANUALLY.
- [SDR G1IA202402095055](https://openairdocs.org/sdr/G1IA202402095055), Feb 5, 2024: DOWNLOCK SWITCH. INOPERATIVE. NOSE GEAR DOWN AND LOCKED GREEN INDICATOR LIGHT DID NOT ILLUMINATE.
- [SDR 2024F00005](https://openairdocs.org/sdr/2024F00005), Jan 8, 2024: PITOT SYSTEM. FALSE INDICATION. AFTER DEPARTING KBIL FOR KGGW THE CREW OBSERVED LOSS OF PRIMARY AIRSPEED INDICATION SO THEY RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR 2023FA0000851](https://openairdocs.org/sdr/2023FA0000851), Dec 11, 2023: UNKNOWN. UNKNOWN. LH FUEL QUANTITY DROPPED DURING CLIMB FROM FAI. PILOT NOTICED A MIST COMING FROM THE COWLING AND RETURNED TO BASE. MAINTENANCE MET THE AIRCRAFT AND NOTICED FUEL
- [SDR ENHA202311160001](https://openairdocs.org/sdr/ENHA202311160001), Nov 16, 2023: UNKNOWN. UNKNOWN. DURING SCHEDULED INSPECTION IT WAS NOTED THAT FORWARD DOOR FRAME AT STATION 273.520 BUCKLED, CROSS TIE AT STATION 246.750 ON LEFT SIDE BUCKLED, CROSS TIE AT STA
- [SDR 2023FA0000739](https://openairdocs.org/sdr/2023FA0000739), Nov 3, 2023: WIRE. CORRODED. SHORTLY AFTER DEPARTURE THE CAPTAIN NOTICED THE COCKPIT LIGHTING OSCILLATING BETWEEN NORMAL AND SLIGHTLY DIMMER. THE CAPTAIN TURNED THE STROBES OFF AND THEN BAC
- [SDR 2023F00320](https://openairdocs.org/sdr/2023F00320), Oct 31, 2023: HYDRAULIC LINE. RUPTURED. WHILE ON APPROACH INTO BFI FROM BIL, THE LANDING GEAR EXTENDED UN-COMMANDED, THE LANDING GEAR HANDLE LIGHT (IN-TRANSIT LIGHT) ILLUMINATED, THE "HYD LOW" ANNUNCI
- [SDR 2023FA0000536](https://openairdocs.org/sdr/2023FA0000536), Sep 12, 2023: UNKNOWN. UNKNOWN. ON DEPARTURE IN CLIMB MASTER WARNING (ILLUMINATED) AND A/P DISENGAGED. RESET ELEVATOR TRIM AND WHEN ENGAGED YAW (DAMPENER) THE PLANE WENT INTO A DIVE TO THE LEF
- [SDR GRTA20230809001](https://openairdocs.org/sdr/GRTA20230809001), Aug 4, 2023: AILERON. CUT. LH AILERON TIP CAP DAMAGE DUE TO COLLISION WITH HANGAR DOOR FRAME. REPAIRED LEFT HAND AILERON, P/N 101-130001-325 S/N BB1755, TIP DAMAGE BY REPLACING TIP PN 101
- [SDR E5WR202305180001](https://openairdocs.org/sdr/E5WR202305180001), May 18, 2023: WHEEL. CRACKED. USING EDDY CURRENT TESTING, A FLAW WAS FOUND ON THE WHEEL HALF IN THE BEAD AREA. INSPECTION WAS PERFORMED IAW MM 32-45-23.
- [SDR G1IA20230420044](https://openairdocs.org/sdr/G1IA20230420044), Apr 20, 2023: LUG. BROKEN. AIRCRAFT DEPRESSURIZED AT 23,000 FEET. WOULD NOT PRESSURIZE AFTER THAT. MADE A "PAN PAN" CALL TO ATC AS I PERFORMED AN EMERGENCY DECENT AND DONNING MY OXYGEN MA
- [SDR GRTA20230506002](https://openairdocs.org/sdr/GRTA20230506002), Apr 18, 2023: FRAME. CRACKED. FRAME CRACKED AT FS 256.250 AND STRINGER 13L, PN 50-420068-31. REPAIRED CRACKED FRAME AT FS 256.250 AND STRINGER 13L USING 2024-T3, 0.063" ALCLAD IAW SIRM 20-10
- [SDR GRTA20230506001](https://openairdocs.org/sdr/GRTA20230506001), Apr 18, 2023: UNKNOWN. UNKNOWN. FRAME CRACKED AT LIGHTNING HOLE AT FS 187.383 JUST ABOVE STRINGER 10R. REPAIRED CRACK FS 187.383 ABOVE STRINGER 10R USING 0.071", 2024-T3 ALCLAD IAW SIRM 20-10-
- [SDR GRTA20230420001](https://openairdocs.org/sdr/GRTA20230420001), Apr 11, 2023: UNKNOWN. UNKNOWN. IMPACT DAMAGE NOTED ON RH SIDE FUSELAGE, BELOW AND AFT RH AVIONICS DOOR (PROP ARC). REPAIRED IMPACT DAMAGE TO PRESSURE VESSEL AT FS 94.0, WL 84.0 RH SIDE, AFT O

All 830: https://openairdocs.org/model/beechcraft-b200/reports.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Beech B200](https://openairdocs.org/model/beech-b200): 281 registered aircraft, registry code 1152922
- [Raytheon B200](https://openairdocs.org/model/raytheon-b200): 206 registered aircraft, registry code 7150006
- [Hawker Beechcraft B200](https://openairdocs.org/model/hawker-beechcraft-b200): 12 registered aircraft, registry code 4220004
- [Textron B200 KING AIR](https://openairdocs.org/model/textron-b200-king-air): 1 registered aircraft, registry code 4222081

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