# Beechcraft B200C - Type: Aircraft model (FAA registry) - Registry code: 4220037 - Manufacturer (registry): BEECHCRAFT CORP - Model: B200C - 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-b200c 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 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 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 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 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 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 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 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 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 None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (169, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR TIMA20240716008](https://openairdocs.org/sdr/TIMA20240716008), Jul 16, 2024: ENGINE. FAULTED. ON FIANL APPROACH TO LANDING PILOT GOAT A NUMBER 1 ENGINE FUEL PRESSURE LIGHT ON QUICKLY FOLLOWED BY THE SAME ENGINE RILLING BACK AND SHUTTING OFF. AT THIS POIN - [SDR 2023FA0000541](https://openairdocs.org/sdr/2023FA0000541), Sep 14, 2023: PANEL. SHORTED. SMELLED ELECTRICAL FIRE 30 MILES FROM ELP, PILOT PFD GOT BRIGHT - LOOKED OVER AND SAW PILOT PFD FUSE HAD POPPED. ONCE AIRCRAFT WAS ON GROUND IN ELP MAINTENANCE - [SDR 2023FA0000537](https://openairdocs.org/sdr/2023FA0000537), Sep 12, 2023: UNKNOWN. UNKNOWN. ENCOUNTERED SEVERE TURBULENCE ABOVE VA DURING FLIGHT. COMPLETED A FIRST LEVEL INSPECTION IN ACCORDANCE WITH AMM CH 5-50-00 TABLE 607 WITH NO DEFECTS NOTED AT TH - [SDR 1EAA2021052700158](https://openairdocs.org/sdr/1EAA2021052700158), Apr 12, 2021: COUPLING. FAILED. FAILURE OF THE #1 ENGINE HP FUEL PUMP DRIVE COUPLING - [SDR 2017FA0000159](https://openairdocs.org/sdr/2017FA0000159), Apr 6, 2017: BOLT. BROKEN. LT MAIN GEAR EXTENDED IN FLIGHT WHILE ENROUTE. AIRCRAFT LANDED AT DESTINATION WITH NO DAMAGE. UPON POST LANDING WALKAROUND, CREW DISCOVERED LEFT MAIN GEAR LOCK - [SDR 2016FA0000473](https://openairdocs.org/sdr/2016FA0000473), Oct 6, 2016: TUBE. CHAFED. DURING PHASE INSPECTION, FOUND THE NR 1 THROTTLE PUSH/PULL TUBE IN CENTER PEDESTAL RUBBING ON WIRE BUNDLE TRAY. NORMAL TUBE OD IS .497 AND OD FOR AREA BEING RUB - [SDR USAR201601050003](https://openairdocs.org/sdr/USAR201601050003), Jan 4, 2016: DOOR FRAME. CRACKED. (00484) AIRSTAIR DOOR FUSELAGE FRAME ENTRY LOWER FWD CORNER CRACK 0.750" LENGTH. - [SDR USAR201601050002](https://openairdocs.org/sdr/USAR201601050002), Jan 4, 2016: DOOR FRAME. CRACKED. (00484) AIR-STAIR DOOR FUSELAGE FRAME ENTRY UPPER FORWARD CORNER CRACKED, 0.500" LENGTH. - [SDR USAR201601050001](https://openairdocs.org/sdr/USAR201601050001), Jan 4, 2016: FRAME. CRACKED. AIRSTAIR DOOR FUSELAGE FRAME ENTRY UPPER AFT CORNER CRACKED, 1.125" LENGTH. - [SDR USAR201508210003](https://openairdocs.org/sdr/USAR201508210003), Aug 19, 2015: DOOR FRAME. CRACKED. DOOR FRAME CRACKED GREATER THAN 1.0" FOUND IN LOWER THRESHOLD SILL CLOSURE. - [SDR USAR201508210002](https://openairdocs.org/sdr/USAR201508210002), Aug 19, 2015: DOOR FRAME. CRACKED. DOOR FRAME CRACKED GREATER THAN 1.0" FOUND IN UPPER FORWARD CLOSURE. - [SDR USAR201508210001](https://openairdocs.org/sdr/USAR201508210001), Aug 19, 2015: STRUCTURE. CRACKED. CRACKS GREATER THAN 1.0" FOUND IN UPPER AFT CLOSURE. - [SDR USAR201508190001](https://openairdocs.org/sdr/USAR201508190001), Aug 14, 2015: DOOR SILL. CRACKED. (00155) ENTRY DOOR SILL CLOSURE WAS INSPECTED AND FOUND TO HAVE 1 EA, 0.75" CRACK IN THE UPPER AFT CORNER CLOSURE. - [SDR CA150817003](https://openairdocs.org/sdr/CA150817003), Aug 4, 2015: ENGINE. FLAMED OUT. (CAN) ENGINE FLAMEOUT IN CRUISE 4 HRS INTO THE FLIGHT. PILOT NOTICED INCREASING FUEL FLOW FLUCTUATION ON ONE ENGINE FOLLOWED BY A FLAMEOUT. THE PILOT LOWERED AL - [SDR USAR201508060003](https://openairdocs.org/sdr/USAR201508060003), Aug 4, 2015: THRESHOLD. CRACKED. (00150) INSPECTOR FOUND .250 INCH CRACK IN THE LOWER THRESHOLD ENTRY DOOR CLOSURE. - [SDR USAR201508060002](https://openairdocs.org/sdr/USAR201508060002), Aug 4, 2015: DOOR FRAME. CRACKED. (00150) INSPECTOR FOUND ONE INCH CRACK IN THE UPPER FORWARD CORNER OF ENTRY DOOR CLOSURE. - [SDR USAR201508060001](https://openairdocs.org/sdr/USAR201508060001), Aug 4, 2015: DOOR FRAME. CRACKED. (00150) INSPECTOR FOUND A ONE INCH CRACK IN UPPER AFT CORNER OF ENTRY DOOR CLOSURE. - [SDR USAR201508060004](https://openairdocs.org/sdr/USAR201508060004), Aug 3, 2015: DOOR FRAME. CRACKED. (03329) CRACKS LESS THAN .7 INCH WERE FOUND IN THE LOWER FORWARD AND LOWER AFT CORNER CLOSURE. - [SDR USAR201507280003](https://openairdocs.org/sdr/USAR201507280003), Jul 17, 2015: DOOR FRAME. CRACKED. (00320) INSPECTOR FOUND .2 INCH CRACK IN UPPER FORWARD CORNER OF ENTRY DOOR CLOSURE AT WELL NUT HOLE. - [SDR USAR201506120002](https://openairdocs.org/sdr/USAR201506120002), Jun 8, 2015: STRUCTURE. CRACKED. ENTRY DOOR: DURING INSPECTION A .080" CRACK AT WELL NUT HOLE ON FORWARD VERTICAL CLOSURE WAS NOTED. - [SDR USAR201506120001](https://openairdocs.org/sdr/USAR201506120001), Jun 8, 2015: DOOR FRAME. CRACKED. ENTRY DOOR FRAME: LOWER CLOSURE HAS A .100" CRACK AT A WELL NUT HOLE. - [SDR CA150521002](https://openairdocs.org/sdr/CA150521002), May 19, 2015: MOTOR. FAILED. (CAN) ON DEPARTURE, THE LANDING GEAR WAS SELECTED UP BUT DID NOT MOVE FROM THE EXTENDED POSITION. TROUBLESHOOTING IDENTIFIED THE HYDRAULIC PUMP DC MOTOR WAS INO - [SDR USAR2015004240001](https://openairdocs.org/sdr/USAR2015004240001), Apr 17, 2015: STRUCTURE. CRACKED. (00489) DOOR SILL CLOSURE FATIGUE CRACK, UPPER FORWARD CORNER .250" APPROXIMATELY. - [SDR CA140318003](https://openairdocs.org/sdr/CA140318003), Feb 28, 2014: MOTOR. FAILED. (CAN) ON APPROACH THE LANDING GEAR WAS SELECTED DOWN THERE WAS NO MOVEMENT OF THE MLG, NO IN TRANSIT LIGHT AND THE CREW RECEIVED A MASTER CAUTION INDICATION. TH - [SDR CA131021015](https://openairdocs.org/sdr/CA131021015), Oct 12, 2013: COUPLING. DISENGAGED. (CAN) AN UNCONTROLLED ACCELERATION WAS EXPERIENCED DURING THE STARTING PROCEDURE FOR MEDICAL RETRIEVAL MISSION. THE PILOT SHUTDOWN THE ENGINE AND NO ACCIDENCES - [SDR CA131021013](https://openairdocs.org/sdr/CA131021013), Oct 10, 2013: ENGINE. UNKNOWN. (CAN) UPON LANDING, THE ACFT EXITED THE RUNWAY. DURING THE ON GROUND INVESTIGATION, THE ENGINEER AND THE PILOT ON SITE TRIED TO START THE ACFT ENGINES AND THE L - [SDR CA130824001](https://openairdocs.org/sdr/CA130824001), Aug 22, 2013: ENGINE. POWER LOSS. (CAN) A CHARTERED ACFT WAS FORCED TO CARRY OUT A DITCHING IN THE LAKE. THE AIRPLANE HAD REPORTEDLY LOSS ENGINE POWER WHILE ENROUTE. ALL 7 OCCUPANTS WERE RESCUED - [SDR CA130318002](https://openairdocs.org/sdr/CA130318002), Feb 18, 2013: FUEL CONTROL. FAILED. (CAN) DURING LANDING ROLLOUT THE ENGINE MADE AN UNCOMMANDED POWER INCREASE, TORQUE LIMITER CUT IN. THE PILOT SHUT THE ENGINE DOWN. TROUBLESHOOTING FOUND A FAULT - [SDR EHAA20120225002](https://openairdocs.org/sdr/EHAA20120225002), Feb 25, 2012: WINDSHIELD. CRACKED. ON CLIMBOUT, HEARD A STRANGE SOUND AS THE GEAR WAS RETRACTED. IT WAS DARK. UPON FURTHER INVESTIGATION, SAW CRACKS ON THE CO-PILOTS WINDSHIELD. - [SDR 2011FA0000112](https://openairdocs.org/sdr/2011FA0000112), Feb 15, 2011: DISPLAY. MALFUNCTIONED. THE PILOT REPORTED THE EX600 MFD DISPLAY REMAINED DIM AND NOT LEGIBLE FOR APPROX 10 TO 15 MINUTES DURING THE ACFT GROUND RUN-UP CHECKS PRIOR TO TAXI. WHEN THE D - [SDR 2011FA0000111](https://openairdocs.org/sdr/2011FA0000111), Dec 16, 2010: DISPLAY. MALFUNCTIONED. ON THE EX600 MFD WHICH HAD JUST BEEN INSTALLED IN AUGUST OF 2010, THE PILOT REPORTED THE FOLLOWING MESSAGES WERE DISPLAYED: BROADCAST RECEIVER NOT COMMUNICATING - [SDR CA090526009](https://openairdocs.org/sdr/CA090526009), May 20, 2009: SKIN. CRACKED. (CAN) DURING A PHASE 4 INSP, A CRACK WAS FOUND ON THE BELLY SKIN ALONG A STRINGER AT THE CENTERLINE OF THE ACFT. THIS CRACK MEASURED TO BE 3.5 INCHES LONG BETWE - [SDR CA081002005](https://openairdocs.org/sdr/CA081002005), Sep 29, 2008: LINE. LEAKING. (CAN) DURING DAILY INSP, WITH POWER ON A FEW MOMENTS, NOTICED FUEL LEAKING FROM LT GEAR WELL. POWER TURNED OFF, NOTED FUEL LEAKING FROM SUPPLY LINE WHICH IS LOC - [SDR 2008FA0000377](https://openairdocs.org/sdr/2008FA0000377), Jul 1, 2008: SKIN. CRACKED. DURING A PREFLIGHT INSPECTION, MAINTENANCE TECH NOTED A 3.75 INCH LONG CRACK IN THE RT WING LOWER WING SKIN JUST FWD OF THE IB SECTION OF THE OB FLAP. ADDITIONA - [SDR CA061221003](https://openairdocs.org/sdr/CA061221003), Dec 18, 2006: MOTOR. FAILED. (CAN) DURING FLIGHT THE LANDING GEAR WOULD NOT EXTEND AND AN EMERGENCY WAS DECLARED. A MANUAL GEAR EXTENSION WAS COMPLETED THE (3) GREEN LIGHTS ILLUMINATED AND - [SDR AU510001942](https://openairdocs.org/sdr/AU510001942), Dec 12, 2005: RING. CRACKED. (AUS) POWER TURBINE STATOR VANE RING CRACKED AND SEPARATED AT THE ROOT ENDS WITH CURLING OF THE TIPS. (OTHER CAUSE: NOT KNOWN AT THIS STAGE ) (CASA# 510001942) - [SDR AU510001575](https://openairdocs.org/sdr/AU510001575), Dec 12, 2005: SERVO. FAULTY. RUDDER AUTOPILOT SERVO/YAW DAMPER FAULTY, OTHER CAUSE: FAILURE OF INTERNAL MECHANISM. - [SDR CA051215001](https://openairdocs.org/sdr/CA051215001), Dec 6, 2005: ACTUATOR. FAILED. AFTER T/O, GEAR WAS SELECTED UP AND CLUNK WAS HEARD, T/O CONTINUED TO SAFE ALT AND WAS VISUALLY CONFIRMED THAT RT GEAR HAD NOT RETRACTED. THE GEAR WAS RECYCLED - [SDR CA050117001](https://openairdocs.org/sdr/CA050117001), Jan 13, 2005: FRAME. CRACKED. (CAN) DURING A ROUTINE INSPECTION A CRACK WAS FOUND PROPAGATING FROM THE OVAL HOLE IN THE RT FRAME AT STATION 207.125 (HALF WAY BETWEEN THE FLOOR AND THE WINDOW - [SDR 2005FA0000034](https://openairdocs.org/sdr/2005FA0000034), Oct 19, 2004: RELAY. FAILED. WHILE THE AIRCRAFT WAS IN FLIGHT, THE FLAPS FAILED TO EXTEND TO THE SELELCTED APPROACH POSITION. THE PILOT CYCLED THE FLAP SELECT SWITCH TO UP AD BACK TO APPROA - [SDR CA040922005](https://openairdocs.org/sdr/CA040922005), Sep 21, 2004: ACTUATOR. WORN. (CAN) DURING ROUTINE 1000 CYCLE ENDPLAY CHECK OF THE NOSE GEAR ACTUATOR, THE ACTUATOR FAILED WITH 0.020 OF AN INCH ENDPLAY THE MAX ALLOWABLE IS 0.016. THIS UNIT - [SDR CA040922001](https://openairdocs.org/sdr/CA040922001), Sep 21, 2004: SNAP RING. OUT OF POSITION. (CAN) DURING ENDPLAY CHECK (1000 CYCLES) ON LT MAIN GEAR ACTUATOR, INPUT GEAR WAS FOUND TO HAVE 0.090 INCH ENDPLAY. THIS CHECK USED TO VERIFY THAT THRUST BEARIN - [SDR EHA2004F00006](https://openairdocs.org/sdr/EHA2004F00006), Jul 26, 2004: UNKNOWN. MALFUNCTIONED. PRELIMINARY - AIRCRAFT DEPARTED ON MEDICAL EVACUATION TRIP. AIRCRAFT DID NOT PRESSURIZE. PIC NOTED LACK OF PRESSURIZATION BY THE EMERGENCY OXYGEN MASK AUTOMATIC - [SDR 2004FA0000524](https://openairdocs.org/sdr/2004FA0000524), Jul 1, 2004: TORQUE TUBE. LOOSE. DURING AN INSPECTION, THE LT ELEVATOR CORNTOL TORQUE TUBE THAT ATTACHES TO IB END RIB OF THE LT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE ACTUATING HORN AND T - [SDR CA040624001](https://openairdocs.org/sdr/CA040624001), Jun 17, 2004: MOUNT. MISMANUFACTURED. (CAN) DURING ENGINE MOUNT REPLACEMENT IT WAS NOTICED THAT THE NEW MOUNTS WERE MANUFACTURED WITH THE BEVEL ON THE WRONG SIDE OF THE METAL PART OF THE CORE (R2070 - [SDR 2004FA0000523](https://openairdocs.org/sdr/2004FA0000523), Jun 1, 2004: TORQUE TUBE. LOOSE. DURING PHASE INSPECTION, THE RT ELEVATOR CONTROL TORQUE TUBE THAT ATTACHES TO THE IB END RIB OF THE RT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE COLLAR WITH T - [SDR AUS20040433](https://openairdocs.org/sdr/AUS20040433), May 20, 2004: SEAL. WORN. (AUS) ENGINE ACCESSORY GEARBOX STARTER-GENERATOR DRIVE SHAFT SEAL WORN. LOSS OF ENGINE OIL. - [SDR AUS20040400](https://openairdocs.org/sdr/AUS20040400), May 12, 2004: TURBINE BLADES. CRACKED. (AUS) COMPRESSOR TURBINE BLADES (3 OFF) CRACKED. CRACKS EMANATE FROM BLADE TIP RADIALLY TOWARDS BLADE ROOT. CRACK LENGTHS UP TO APPROXIMATELY 7MM (0.27IN). FOUN - [SDR AUS20040222](https://openairdocs.org/sdr/AUS20040222), Mar 23, 2004: SHAFT. FAILED. (AUS) LT MAIN LANDING GEAR RETRACTION DRIVE TUBE FAILED DUE TO INTERFERENCE WITH PNEUMATIC DUCTING CLAMP. - [SDR AUS20040213](https://openairdocs.org/sdr/AUS20040213), Mar 12, 2004: VALVE. FAULTY. (AUS) DEFECT REPORT NR WAS CREATED IN LIEU OF DATA BEING ATTACHED TO MDR 04/0176. CANCELLED, DATED 25TH MARCH 2004. All 169: https://openairdocs.org/model/beechcraft-b200c/reports.md ## STCs that may be installed (OpenAirDocs) (371, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA03025CH](https://openairdocs.org/stc/SA03025CH): Installation of weather research equipment and weather modification equipment for the purpose of modifying weather conditions. 3S Certification, LLC - [STC SA04617NY](https://openairdocs.org/stc/SA04617NY): Installation of the Medivac Audio System. Avmax Aviation Services Inc - [STC SA4175NM](https://openairdocs.org/stc/SA4175NM): Installation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft. Raisbeck Engineering Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04221CH](https://openairdocs.org/stc/SA04221CH): Installation of Thermal Acoustic Kit. Skandia Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC - [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH - [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC - [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc - [STC SA01638WI](https://openairdocs.org/stc/SA01638WI): Part Fabrication and Installation of Arm Ledge System and Table Assembly for aircraft cabin interior. Aviation Fabricators Inc - [STC ST04442CH](https://openairdocs.org/stc/ST04442CH): Installation of SmartSky LiTE System. Apcela IFC JV, LLC dba Apcela ATG - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd - [STC SA10800SC](https://openairdocs.org/stc/SA10800SC): Installation of a 3-tube Rockwell Collins IDS-3000 Electronic Flight Instrument System with File Server Unit (FSU). BHE & Associates LTD - [STC SA01535WI-D](https://openairdocs.org/stc/SA01535WI-D): Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP). Garmin International Inc - [STC SA10941SC](https://openairdocs.org/stc/SA10941SC): Installation of a 3-Tube Rockwell Collins Pro Line 21 Avionics System with Rockwell Collins Integrated Flight Information System 5000, TCAS II, and Honeywell Enhanced Ground Proximity Warning System. BHE and Associates - [STC SA10965SC](https://openairdocs.org/stc/SA10965SC): Installation of upgraded hardware to the Rockwell Collins Pro Line 21 FMS-3000 to provide Localizer Performance with Vertical Guidance (LPV). BHE & Associates LTD - [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd - [STC SA2300CE](https://openairdocs.org/stc/SA2300CE): Installation of Removable External Baggage Compartment. Avcon Industries Inc - [STC SA2404CE](https://openairdocs.org/stc/SA2404CE): Installation of engine low oil pressure warning system. Metrea Special Aerospace ISR Inc - [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 SA8986SW](https://openairdocs.org/stc/SA8986SW): Installation of full turning contoured engine exhaust stacks on Pratt & Whitney Canada PT6A-38, PT6A-41, or PT6A-42 engines. Metrea Special Aerospace ISR Inc - [STC SA00400BO](https://openairdocs.org/stc/SA00400BO): Installation of an Autothrottle System (ATS). Innovative Solutions & Support Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc - [STC SA02013WI](https://openairdocs.org/stc/SA02013WI): Installation of BLR Winglet Performance Analysis at Centex Increased Gross Weight. BLR Aerospace LLC - [STC SA00197MC](https://openairdocs.org/stc/SA00197MC): Ground Idle Reset System Removal. Raisbeck Engineering Inc - [STC SA11133SC](https://openairdocs.org/stc/SA11133SC): Installation of a Rockwell Collins Pro Line 21 update to include optional TAWS mode 5 warnings during LPV approaches, optional ADS-B Out, optional synthetic vision system (SVS), optional Communication Management Unit (CMU) and 3rd VHF to support Controller Pilot Data Link. BHE & Associates LTD - [STC SA00416BO](https://openairdocs.org/stc/SA00416BO): Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit. Outerlink Corporation - [STC SA11855IB](https://openairdocs.org/stc/SA11855IB): Installation of the Flap Roller Bearing Assembly. Marsh Brothers Aviation Inc - [STC SA11301DS](https://openairdocs.org/stc/SA11301DS): Installation of an AirSync flight data monitoring system. BHE & Associates Ltd - [STC SA02038WI](https://openairdocs.org/stc/SA02038WI): Installation of the Universal Avionics ClearVision and Enhanced Vision System (EVS) equipment. Global Aviation Tech LLC - [STC SA01848WI](https://openairdocs.org/stc/SA01848WI): Modification of a Rockwell Collins Global Positioning System (GPS). Rockwell Collins Inc - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA00294BO](https://openairdocs.org/stc/SA00294BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC - [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 SA00113MC](https://openairdocs.org/stc/SA00113MC): Installation of mission equipment for TACAN, Storm Scope, Data Link, TA-24 GPS, military radio and APX-119 Transponder and provides for Synthetic Vision. Sierra Nevada Company LLC - [STC SA02033WI](https://openairdocs.org/stc/SA02033WI): Installation of the SmartSky LITE System. Aeronautix - [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC SA01615SE](https://openairdocs.org/stc/SA01615SE): Installation of winglets and related system changes. BLR Aerospace LLC - [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC. Lists 200 Series - [STC ST02752SE](https://openairdocs.org/stc/ST02752SE): Installation of the Starlink Aviation System. AeroMech Incorporated - [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc All 371: https://openairdocs.org/model/beechcraft-b200c/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech B200C](https://openairdocs.org/model/beech-b200c): 16 registered aircraft, registry code 1152924 - [Raytheon B200C](https://openairdocs.org/model/raytheon-b200c): 5 registered aircraft, registry code 7150041 - [Hawker Beechcraft B200C](https://openairdocs.org/model/hawker-beechcraft-b200c): 0 registered aircraft, registry code 4220019 --- 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.