# Beech A200C - Type: Aircraft model (FAA registry) - Registry code: 1152898 - Manufacturer (registry): BEECH - Model: A200C - 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: 2 - Page: https://openairdocs.org/model/beech-a200c 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 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 98-20-38 R1](https://openairdocs.org/ad/98-20-38-R1): Airplane Flight Manual (AFM) · Textron 200, 200C, 200CT and 15 more. Effective Feb 18, 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 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 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 96-03-13](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 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 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 80-07-05](https://openairdocs.org/ad/80-07-05): Bolt and Nut, Wing Section · Textron 200, 200C, 200T and 10 more. Effective Apr 3, 1980 Historical (superseded or no longer in force): - [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 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) (1) - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 ## Registered aircraft (2) - [N200AN](https://openairdocs.org/aircraft/N200AN): [Airtrex Registration Corp Trustee](https://openairdocs.org/faa-owner/AIRTREX%20REGISTRATION%20CORP%20TRUSTEE), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita), built 1979, S/N BJ-3 - [N321P](https://openairdocs.org/aircraft/N321P): [Dynamic Avlease Inc](https://openairdocs.org/faa-owner/DYNAMIC%20AVLEASE%20INC), [Bridgewater, VA](https://openairdocs.org/faa-place/VA/Bridgewater), built 1980, S/N GR-10 ## STCs approved for it (189, first 50) - [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 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 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 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 SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services 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 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 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 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 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 - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00829CH](https://openairdocs.org/stc/SA00829CH): Installation of Butterfield Industries Air/Oil Separator System, kit Part Number BI 6001-1. Raisbeck Engineering - [STC SA00840LA](https://openairdocs.org/stc/SA00840LA): Installation of Infant Transport Module (ITM).. Lifeport Inc - [STC SA00882CH](https://openairdocs.org/stc/SA00882CH): Install air ambulance conversion.. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SA01051SE](https://openairdocs.org/stc/SA01051SE): Installation of an interior sidewall folding table, part numbers 56300-144-03 or 53600-144-04. Enflite Inc. - [STC SA01110CH](https://openairdocs.org/stc/SA01110CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC - [STC SA01115WI](https://openairdocs.org/stc/SA01115WI): Installation of Medevac Interior.. Hillaero Modification Center - [STC SA01126WI](https://openairdocs.org/stc/SA01126WI): Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632. DER Associates Ltd. - [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head.. Rockwell Collins Inc - [STC SA01157CH](https://openairdocs.org/stc/SA01157CH): Installation of McCauley Propeller Systems 5HFR34C1008/96LTA-0 5 bladed model propeller.. McCauley Propeller Systems - [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc. - [STC SA01169WI](https://openairdocs.org/stc/SA01169WI): Installation of Aero-Mach Labs, Inc. propeller RPM tachometer or percent (gas generator/N1) RPM tachometer instruments.. Aero-Mach Labs Inc. - [STC SA01194WI-D](https://openairdocs.org/stc/SA01194WI-D): Installation of the Honeywell GNS-XLS Flight Management System.. Honeywell International Inc - [STC SA01203SE](https://openairdocs.org/stc/SA01203SE): Installation of the Bendix/King KMD 550/850 Multi-Function Display w/Options Installed and Maintained. Hillsboro Aviation - [STC SA01213CH](https://openairdocs.org/stc/SA01213CH): Install air ambulance conversion in accordance with Spectrum Aeromed Inc. Drawings as listed on AML SA01213CH, or later FAA approved revision.. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA01306WI-D](https://openairdocs.org/stc/SA01306WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation.. Rockwell Collins Inc - [STC SA01473SE (5 OF 5)](https://openairdocs.org/stc/SA01473SE%20(5%20OF%205)): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc. - [STC SA01487SE (4 OF 5)](https://openairdocs.org/stc/SA01487SE%20(4%20OF%205)): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA01565NY](https://openairdocs.org/stc/SA01565NY): Installation of OuterLink CP-2 SATCOM System in accordance with DECA Modification Summary MS01147-01, Revision 2, dated November 1, 2002.. Outerlink Corporation - [STC SA01636WI-D](https://openairdocs.org/stc/SA01636WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc - [STC SA01639NY](https://openairdocs.org/stc/SA01639NY): Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.. Scale Modelbuilders Inc. - [STC SA01692SE (PAGE 1 OF 2)](https://openairdocs.org/stc/SA01692SE%20%20(PAGE%201%20OF%202)): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc All 189: https://openairdocs.org/model/beech-a200c/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 (14) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000676](https://openairdocs.org/sdr/2026FA0000676), Aug 20, 2026: MOTOR. BURNED OUT. CAPTAIN WAS PILOT FLYING. N301PT DEPARTED ANC FOR IGG. WHILE IN THE CLIMB AT ABOUT 7,000FT, SMOKE COULD BE SMELLED INSIDE THE AIRCRAFT. PILOT LEVELED OFF AND NO - [SDR 2017FA0000233](https://openairdocs.org/sdr/2017FA0000233), May 24, 2017: COMBUST CHAMBER. CRACKED. AFTER INITIAL POST PHASE ENGINE RUN, MAINTENANCE WAS INSTALLING THE LT ENGINE COWLING WHEN THEY DISCOVERED THAT THE COMBUSTION CHAMBER CASING WELD WAS CRACKED. - [SDR USAR201507160003](https://openairdocs.org/sdr/USAR201507160003), Jul 16, 2015: STRUCTURE. CRACKED. (51264) A CRACK IN THE UPPER AFT CORNER CLOSURE GREATER THAN 1.00 WAS IDENTIFIED. - [SDR USAR201507160002](https://openairdocs.org/sdr/USAR201507160002), Jul 14, 2015: STRUCTURE. CRACKED. A CRACK WAS FOUND ON UPPER AFT CORNER CLOSURE .910" LONG. - [SDR USAR201507160001](https://openairdocs.org/sdr/USAR201507160001), Jul 14, 2015: STRUCTURE. CRACKED. (00163) A CRACK WAS FOUND AT THE UPPER FORWARD CORNER CLOSURE .300" LONG. - [SDR USAR201507280002](https://openairdocs.org/sdr/USAR201507280002), Jul 13, 2015: STRUCTURE. CRACKED. (24376) LOWER AFT CORNER CRACK ROUTED GREATER THAN 1.0" IN LENGTH. - [SDR USAR201507280001](https://openairdocs.org/sdr/USAR201507280001), Jul 13, 2015: STRUCTURE. CRACKED. (24376) UPPER AFT CORNER CRACKED 1.0" IN LENGTH. - [SDR USAR201505290001](https://openairdocs.org/sdr/USAR201505290001), May 14, 2015: ACTUATOR. BROKEN. (3783) ON APPROACH TO LANDING THE PILOT REPORTED UNSAFE RT MLG, AN UNEVENTFUL LANDING WAS MADE. INSPECTION NOTED THE RT MLG ACTUATOR NUT BARREL BROKE FROM THE N - [SDR 2014FA0000473](https://openairdocs.org/sdr/2014FA0000473), Aug 9, 2014: FCU. FAILED. INSTALLED NEW OVERHAULD FUEL CONTROL UNIT DURING MAINTENANCE. OVERHAULED UNIT THEN FAILED AFTER A FEW SUCCESSFUL ENGINE RUNS. THE SYMPTOMS OF FAILURE WERE SLUGG - [SDR 2013FA0000306](https://openairdocs.org/sdr/2013FA0000306), May 30, 2013: GYRO. INOPERATIVE. WHILE CIRCLING AT A BANK ANGLE OF 30 DEGREES, OCCASIONALLY 45, FOR APPROX 2.0 HOURS, THE PILOT AND CO-PILOT`S EHSI LOST HEADING INFORMATION. BOTH GYROS, SG102, - [SDR 2013FA0000305](https://openairdocs.org/sdr/2013FA0000305), May 30, 2013: GYRO. INOPERATIVE. WHILE CIRCLING AT A BANK ANGLE OF 30 DEGREES, OCCASIONALLY 45, FOR APPROX 2.0 HOURS, THE PILOT AND CO-PILOTS EHSI LOST HEADING INFORMATION. BOTH GYROS, SG102, W - [SDR 2011FA0000722](https://openairdocs.org/sdr/2011FA0000722), Nov 2, 2011: BETA TUBE. OUT OF ADJUST. THE NR 2 PROPELLER WAS REPLACED WITH AN O/H PROPELLER. GROUND RUNS REVEALED NO DISCREPANCIES AND THE ACFT WAS RETURNED TO SERVICE. THE ACFT FLEW A MISSION AND U - [SDR 2011FA0000721](https://openairdocs.org/sdr/2011FA0000721), Nov 1, 2011: STRUCTURE. CRACKED. DURING TROUBLESHOOTING OF AN OIL LEAK ON ACFT, A CRACK WAS FOUND IN THE UPPER LT WHEELWELL, ABOVE THE LANDING GEAR FENDER. FOUND 3 ADDITIONAL CRACKS IN THE LT W - [SDR 2000ZZZX664](https://openairdocs.org/sdr/2000ZZZX664), Jun 10, 1999: SWITCH. MISINSTALLED. THIS PART, NR 1 FIREWALL SHUT-OFF VALVE PULL SWITCH, HAD AT SOME POINT BEEN DISMOUNTED AND THEN REMOUNTED USING A SCREW THAT WAS LONGER THAN THE REQUIRED NAS387 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.