# Beech A200 (C-12C) - Type: Aircraft model (FAA registry) - Registry code: 115292A - Manufacturer (registry): BEECH - Model: A200 (C-12C) - 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: 1 - Page: https://openairdocs.org/model/beech-a200-c-12c 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 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 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 97-25-03](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 96-03-13](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 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 80-09-03 R1](https://openairdocs.org/ad/80-09-03-R1): Placard -Oxygen · Textron 100, 200, 200C and 9 more. Effective Jun 11, 1980 - [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 - [AD 76-09-02](https://openairdocs.org/ad/76-09-02): Bolt Hole Edge Distance · Textron 200, A100-1 (U-21J) and A200 (C-12A). Effective May 3, 1976 - [AD 76-04-02](https://openairdocs.org/ad/76-04-02): Seat Locking Pins · Textron 200, A100, A200 and 2 more. Effective Feb 26, 1976 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 (1) - [N222KC](https://openairdocs.org/aircraft/N222KC): [U S Army - Owner](https://openairdocs.org/faa-owner/U%20S%20ARMY%20-%20OWNER), [New Century, KS](https://openairdocs.org/faa-place/KS/New%20Century), built 1979, S/N BC-68 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (52, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2025FA0000454](https://openairdocs.org/sdr/2025FA0000454), Jun 20, 2025: ARM. BROKEN. AIRCRAFT BEING OPERATED BY TWO PILOT CREW. SIC WAS BACK TAXIING ON RUNWAY IN PREP FOR TAKEOFF. SIC MANEUVERED FOR A RIGHT 180 ON THE RUNWAY AND MADE THE RIGHT T - [SDR 2018FA0000003](https://openairdocs.org/sdr/2018FA0000003), Jan 26, 2017: BRACKET. CRACKED. ON 26 JAN 2017 BRACKET P/N 100-820018-7 WERE FOUND CRACKED ON THE NOSE LANDING GEAR DRAG BRACE P/N 50-820205-25. - [SDR K5L2014F00001](https://openairdocs.org/sdr/K5L2014F00001), Oct 1, 2014: INDICATOR. FAILED. DURING CLIMB THROUGH 4000 FT, THE CAPTAIN SIDE ATTITUDE INDICATOR FLAGGED "GYRO", THEN STARTED INDICATING A BANK TO THE LEFT. CAPTAIN CALLED THE FAILURE AND POS - [SDR K5L20140110000001](https://openairdocs.org/sdr/K5L20140110000001), Dec 12, 2013: FLAP TRACK. TORN. AIRCRAFT WAS CLEARED TO LAND AND ON A CLOSE LT DOWNWIND, CIRCLING AT 140 KNOTS FROM A GPS13 APPROACH, CONFIGURED WITH FLAPS SET AT APPROACH AND GEAR SELECTED DO - [SDR 4DSR20130425001](https://openairdocs.org/sdr/4DSR20130425001), Apr 3, 2013: STARTER GEN. INOPERATIVE. DURING A POST-MX CHECK FLIGHT FOR REMOVAL AND REINSTALLATION OF THE FUEL CONTROL AND STARTER/GENERATOR THE GOVERNMENT FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN - [SDR K5L2012F00002](https://openairdocs.org/sdr/K5L2012F00002), Jul 13, 2012: FIRE DETECTOR. FAILED. ON SHORT FINAL APPROACH THE LEFT ENGINE FIRE DETECTOR T-HANDLE LIGHT ILLUMINATED. PILOT MADE A NORMAL LANDING AND NO SMOKE WAS NOTICED. PULLED AND RESET CIRCUIT - [SDR K5L2012F00001](https://openairdocs.org/sdr/K5L2012F00001), Jul 13, 2012: FIRE DETECTOR. FAILED. ON SHORT FINAL APPROACH, THE LT ENGINE FIRE DETECTOR T HANDLE LIGHT ILLUMINATED. PILOT MADE NORMAL LANDING AND NO SMOKE WAS NOTICED, PULLED AND RESET CIRCUIT BR - [SDR 2011FA0000787](https://openairdocs.org/sdr/2011FA0000787), Dec 9, 2011: PITOT TUBE. MISMARKED. DURING ALTIMETER AND PITOT STATIC SYSTEM RE-CERTIFICATION, THE TECH OBSERVED THAT THE LT PITOT TUBE WAS INCORRECT AND WAS ACTUALLY A RT PITOT TUBE. UPON FURTHER - [SDR 2011FA0000723](https://openairdocs.org/sdr/2011FA0000723), Nov 2, 2011: SPAR. CRACKED. INSPECTION OF FLEET ACFT SN IN THE BC AND BD RANGE HAVE REVEALED CRACKING OF THE MAIN WING SPAR WEB IN CARRY THROUGH OPENINGS AND END CAP SUPPORTS. IN THE WHEEL - [SDR 2009FA0000755](https://openairdocs.org/sdr/2009FA0000755), Aug 31, 2009: RELIEF VALVE. LOOSE. DURING SCHEDULED PHASE INSP, FOUND RELIEF VALVE BACKED OUT OF FUEL FILTER PN 50-389110. THIS FIREWALL-MOUNTED FILTER HAS A BALL-AND-SPRING TYPE RELIEF VALVE THR - [SDR 2009FA0000292](https://openairdocs.org/sdr/2009FA0000292), Apr 3, 2009: FLOW VALVE. FAILED. DURING CLIMB TO ALTITUDE CABIN FAILED TO MAKE MAXIMUM DIFFERENTIAL PRESSURE AND HAD A HIGHER THAN NORMAL CABIN. FOUND A P3 AIR TUBE DISSCONNECTED AT RT HEAT EXC - [SDR 2009FA0000269](https://openairdocs.org/sdr/2009FA0000269), Apr 1, 2009: BOLT. FAILED. WHILE REPLACING THE RT WING FWD WING BOLT AND BARREL NUT, HEARD A POP WHILE TIGHTENING THE NEW BOLT BEFORE REACHING FINAL TORQUE. REMOVED NEW BOLT/BARREL NUT AN - [SDR K5LA050908001](https://openairdocs.org/sdr/K5LA050908001), May 5, 2008: BELLCRANK. TWISTED. DRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEGREES FROM WHAT A NEW ONE IS.. ALSO THE B - [SDR K5L2007F00002](https://openairdocs.org/sdr/K5L2007F00002), Nov 25, 2007: POWER SUPPLY. FAILED. AWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WA - [SDR K5L2007F00001](https://openairdocs.org/sdr/K5L2007F00001), Nov 25, 2007: ACTUATOR. INOPERATIVE. DESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL - [SDR 2007FA0000995](https://openairdocs.org/sdr/2007FA0000995), Nov 7, 2007: RELAY. MELTED. RT STARTER GENERATOR RELAY P/N: 6041H190 MELTED AT BUSS BAR CONNECTION. - [SDR 2007FA0000785](https://openairdocs.org/sdr/2007FA0000785), Aug 7, 2007: SENSOR. FAULTY. AT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED. ALL ENGINE G - [SDR K5L2007F00000](https://openairdocs.org/sdr/K5L2007F00000), Mar 6, 2007: WINDSHIELD. FAILED. WHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDIN - [SDR 15462006H1](https://openairdocs.org/sdr/15462006H1), Jul 10, 2006: RELAY. BURNED. NR 2 START RELAY SHORTED TO GROUND DURING ENGINE START, APPARENTLY DUE TO WATER INCURSION OR CONTACT CORROSION. RELAY BURNED BUT START WAS SECURED BEFORE ADJACE - [SDR K5L2005F00002](https://openairdocs.org/sdr/K5L2005F00002), Nov 11, 2005: SHUTOFF VALVE. FAILED. AFTER NORMAL ENGINE START, DURING RUN UP NOTICED THAT THE LEFT INSTRUMENT SHUTOFF VALVE PN 101381000-9 WOULD NOT CLOSE WHEN SELECTED OFF. FOUND VALVE SOLENOID T - [SDR K5L2005F00001](https://openairdocs.org/sdr/K5L2005F00001), Jan 3, 2005: FUSE. FAILED. SELECTED APPROACH FLAPS DESCENDING, FLAPS FAILED TO EXTEND. RESET CIRCUIT BREAKER AND CYCLED FLAP SELECTOR BUT STILL NO FLAP MOVEMENT. MADE UNEVENTFUL NO FLAP L - [SDR K5L2005F00000](https://openairdocs.org/sdr/K5L2005F00000), Dec 27, 2004: UPLOCK SWITCH. FAILED. ON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS STAY ON, PUSH FWD AND LIGHTS GO OFF. REMOV - [SDR B3OR20041029](https://openairdocs.org/sdr/B3OR20041029), Sep 22, 2004: ATTACH FITTING. DAMAGED. ON 22 SEPTEMBER 2004 A 5 YEAR WING BOLT INSPECTION WAS COMPLIED WITH ON A BEECHCRAFT A200 AIRCRAFT. THREE OF THE WING ATTACH FITTINGS WERE FOUND TO HAVE DAMAGE - [SDR WK1](https://openairdocs.org/sdr/WK1), May 13, 2004: MOTOR. FAILED. SHORTLY AFTER TAKEOFF SMOKE WAS OBSERVED IN THE COCKPIT WITH ELECTRICAL ODOR. FORWARD CABIN VENT BLOWER WAS DISABLED AND THE SMOKE CLEARED. VENT BLOWER HAD FAIL - [SDR 2004FA0000402](https://openairdocs.org/sdr/2004FA0000402), Mar 10, 2004: ACTUATOR. SEPARATED. CREW RETRACTED FLAPS, FLAPS STOPPED .5000 WAY UP. SPLIT FLAP SAFETY CIRCUIT STOPPED FLAP RETRACTION. REVEALED THAT LT IB FLAP ACTUATOR HAD FAILED. 90 DEGREE DRI - [SDR K5LA620JS](https://openairdocs.org/sdr/K5LA620JS), Jan 2, 2004: WINDSHIELD. CRACKED. CLIMBING THROUGH 14000 FT IN THE CLOUDS WITH W/S HEAT ON, OAT-5C PILOTS WINDSHIELD OUTER PLY CRACKED ACROSS ENTIRE WINDSHIELD. RETURNED TO AIRPORT AND LANDED. R - [SDR K5LA620J](https://openairdocs.org/sdr/K5LA620J), Aug 5, 2003: SAFETY SWITCH. BROKEN. AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. GEAR REMAINED DOWN AND LOCKED. AFTER LANDING IT WAS DETERMINED A WIRE ON THE LANDING GEAR EMERGENCY SAFETY SWITCH - [SDR B3OR20033014](https://openairdocs.org/sdr/B3OR20033014), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE LEFT OUTBOARD FLAP TACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVERE ENOU - [SDR B3OR20033013](https://openairdocs.org/sdr/B3OR20033013), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND OUTBOARD FLAP TRACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVE - [SDR B3OR20033012](https://openairdocs.org/sdr/B3OR20033012), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND INBORAD FLAP TRACK WAS FOUND TO HAVE DEEP EXIFOLLIATION FLAKING CORROSION ON THE INBOARD SIDE OF THE TRACK.T - [SDR B3OR2003009](https://openairdocs.org/sdr/B3OR2003009), Jun 5, 2003: HINGE BRACKET. CORRODED. MECH NOTICED (PAINT BUBBLING) ON, UPPER RUDDER HINGE BRACKET. ON INVESTIGATION, CORROSION WAS FOUND. FLAKING, CORROSION WAS TOO DEEP INTO METAL OF HINGE BRACKET - [SDR B3OR2003008](https://openairdocs.org/sdr/B3OR2003008), Jun 5, 2003: HINGE. CORRODED. DURING A 15 DAY CORROSION INSP, MECH NOTICED "PAINT BUBBLEING" ON MIDDLE RUDDER HINGE BRACKET. UPON INVESTIGATION, CORROSION FOUND. ATTEMPT WAS MADE TO CLEAN & - [SDR B3OR2003007](https://openairdocs.org/sdr/B3OR2003007), Jun 5, 2003: HINGE BRACKET. CORRODED. DURING CORR INSP, MECH NOTICED "PAINT BUBBLING" ON LT, IB ELEV HINGE BRACKET. FURTHER INVESTIGATION BY SCRAPING-OFF PAINT BUBBLE, CORR WAS FOUND. ATTEMPT WAS MA - [SDR B3OR2003006](https://openairdocs.org/sdr/B3OR2003006), Jun 5, 2003: HINGE BRACKET. CORRODED. MECH NOTICED (PAINT BUBBLING) ON LT AND RT, MIDDLE ELEVATOR HINGE. FURTHER INVESTIGATION BY SCRAPEING-OFF PAINT BUBBLE, CORROSION WAS FOUND. ATTEMPT WAS MADE TO - [SDR B3OR2003005](https://openairdocs.org/sdr/B3OR2003005), Jun 5, 2003: HINGE BRACKET. CORRODED. MECHANIC NOTICED (PAINT BUBBLING) ON LT OB ELEVATOR HINGE .UPON FURTHER INVESTIGATION BY SCRAPING-OFF THE PAINT BUBBLE, CORROSION WAS FOUND. AN ATTEMPT WAS MADE - [SDR B30R20033011](https://openairdocs.org/sdr/B30R20033011), Jun 4, 2003: HINGE BRACKET. DAMAGED. DURING A 14 DAY CORROSION INSPECTION, MECHANIC NOTED PAINT BLISTERING ON THE RIGHT INBOARD ELEVATOR HINGE BRACKET. REMOVAL OF THE PAINT BLISTERS FROM HINGE BRAC - [SDR B30R20033010](https://openairdocs.org/sdr/B30R20033010), Jun 4, 2003: HINGE FITTING. CORRODED. DURING A 14 DAY CORROSION INSP, MECH NOTED PAINT BLISTERING AROUND RIGHT ELEVATOR HINGE FITTING MOUNTING HARDWARE. REMOVAL OF PAINT BLISTERS FROM HINGE FITTING - [SDR 2002FA0001175](https://openairdocs.org/sdr/2002FA0001175), Aug 20, 2002: RIVET. MISSING. ELEVATOR TRIM TABS ON AIRCRAFT WERE INSPECTED FOR RIVETS. FOUND LT ELEVATOR TRIM TAB THAT WAS INSTALLED 10 HOURS PRIOR, TO BE MISSING ALL RIVETS. THE SKINS WERE - [SDR B3OR20020018](https://openairdocs.org/sdr/B3OR20020018), Aug 7, 2002: RIVET. MISSING. TRIM TAB WAS REPLACED DUE TO CORROSION, WHEN PART WAS INSTALLED IT WAS NOT NOTICED THAT THE RIVETS ALONG THE LEADING EDGE AND AROUND THE PITCH HORN WERE NOT INS - [SDR 2002FA0000450](https://openairdocs.org/sdr/2002FA0000450), Apr 5, 2002: HINGE. CORRODED. THE CENTER RUDDER HINGE ASSEMBLY WAS REMOVED FROM THE AIRCRAFT FOR REPLACEMENT DUE TO VISIBLE CORROSION NEAR THE EDGE OF THE LOWER RIGHT HAND BOLT HOLE ON THE T - [SDR 2002FA0000166](https://openairdocs.org/sdr/2002FA0000166), Jan 9, 2002: DRAG BRACE. CRACKED. DURING SCHEDULED LANDING GEAR TIME CHANGE, THE DRAG BRACE SUPPORTS WERE CLEANED AND INSPECTED. THE RIGHT DRAG BRACE SUPPORT APPEARED TO BE CRACKED. A DYE-PENETR - [SDR 040521239A](https://openairdocs.org/sdr/040521239A), Dec 4, 2001: SUPPORT. CRACKED. LEFT HAND MAIN LANDING GEAR DRAG LEG SUPPORT FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SERVICE BASED ON RE - [SDR 040521239](https://openairdocs.org/sdr/040521239), Dec 4, 2001: SUPPORT. CRACKED. LEFT HAND AND RIGHT HAND MAIN LANDING GEAR DRAG LEG SUPPORTS FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SER - [SDR WD42001F00000](https://openairdocs.org/sdr/WD42001F00000), Nov 1, 2001: VALVE. MISMANUFACTURED. NEW REPLACEMENT PARTS FOR THE ANTI-SIPHON VALVE ASSEMBLY ARE BEING MFG INCORRECTLY. PROBLEM IS THE FLAPPER ASSEMBLY GASKET AND BACKUP PLATE WERE TRIMMED INCORRE - [SDR B3OR200000005](https://openairdocs.org/sdr/B3OR200000005), Nov 2, 2000: TUBE. CRACKED. PILOTS COMPLETED PRE-TAKEOFF ENGINE RUNS AND RETURNED ENGINES TO IDLE. WHEN POWER LEVERS WERE ADVANCED FOR TAXI TO ACTIVE, NR 1 ENGINE DID NOT RESPOND TO INPUT. - [SDR 20001120SH023](https://openairdocs.org/sdr/20001120SH023), Jun 7, 2000: DRAG BRACE. MISOVERHAULED. MAIN GEAR ASSEMBLY RECEIVED IN OVERHAULED CONDITION. DURING INSTALLATION PROCESS, NOTED AND VERIFIED THE DRAG LINK ATTACHMENT LUG SLEEVE WAS APPROXIMATELY .010 - [SDR 99ZZZX2657](https://openairdocs.org/sdr/99ZZZX2657), Jul 1, 1999: TUBE ASSY. CRACKED. PRE-TAKEOFF ENGINE RUNS COMPLETED, PILOTS TAXIED OUT ONTO ACTIVE, APPLIED TAKEOFF POWER, NR 1 ENGINE NO RESPONSE. RETURNED TO LINE, AND SHUT DOWN. MAINTENANCE I - [SDR 98ZZZX530](https://openairdocs.org/sdr/98ZZZX530), Jan 20, 1998: BOLT KIT. WRONG PARTS. THE BOLT KIT LISTED IS FOR THE UPPER AND LOWER AFT WING ATTACH FITTINGS FOR A BEECH SERIES 200, UPON RECEIVING 4 OF THESE KITS, NOTICED THE WASHERS INCLUDED IN - [SDR 98ZZZX531](https://openairdocs.org/sdr/98ZZZX531), Jan 19, 1998: BOLT KIT. WRONG PARTS. THE BOLT KIT LISTED IS FOR THE UPPER FORWARD WING BOLTS FOR A BEECH 200. UPON RECEIVING 2 EACH KITS, NOTED THE WASHERS INCLUDED WERE NOT PROPERLY RADIUSED ON TH - [SDR 98ZZZX538](https://openairdocs.org/sdr/98ZZZX538), Jan 18, 1998: BARREL NUT. WRONG PART. KIT 101-4024-1S CONTAINS THE FORWARD LOWER WING BOLT, PL WASHER AND BARREL NUT FOR INSTALLATION ON BEECH 200 SERIES ARICRAFT. THE BARREL NUT ASSY PN 80691CF-161 All 52: https://openairdocs.org/model/beech-a200-c-12c/reports.md ## STCs that may be installed (OpenAirDocs) (210, 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 SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International 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 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 SA03930NY](https://openairdocs.org/stc/SA03930NY): Installation of King Air Belly Payload Mount. Icarus Aero Inc - [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 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 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 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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. 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 SA00416BO](https://openairdocs.org/stc/SA00416BO): Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit. Outerlink Corporation - [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 SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC - [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 - [STC SA2698NM-S](https://openairdocs.org/stc/SA2698NM-S): Installation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan Propellers. Raisbeck Engineering Inc - [STC SA00829CH](https://openairdocs.org/stc/SA00829CH): Installation of Butterfield Industries Air/Oil Separator System, kit Part Number BI 6001-1. Raisbeck Engineering - [STC SA02215SE](https://openairdocs.org/stc/SA02215SE): Fabrication of Inspection Panel Kit BI 9501-001. Raisbeck Engineering Inc - [STC SA1783NM](https://openairdocs.org/stc/SA1783NM): Install Mark VI system. Raisbeck Engineering Inc - [STC SA2905NM](https://openairdocs.org/stc/SA2905NM): Installation of Butterfield Industries Flow Through Anti-Ice Kit Part Number BI 1001-1. Raisbeck Engineering Inc - [STC SA3366NM](https://openairdocs.org/stc/SA3366NM): Installation of the Ram Air Recovery System. Raisbeck Engineering Inc - [STC SA3591NM](https://openairdocs.org/stc/SA3591NM): Installation of lower aft fuselage strakes. Raisbeck Engineering Inc - [STC SA3683NM](https://openairdocs.org/stc/SA3683NM): Installation of exhaust stack fairings. Raisbeck Engineering Inc - [STC SA4362NM](https://openairdocs.org/stc/SA4362NM): Installation of Butterfield Industries Oil Residue Collection System Kit Part Number BI 1011-1. Raisbeck Engineering Inc - [STC SA01924WI](https://openairdocs.org/stc/SA01924WI): Installation of an External Pod and Retractable EO/IR Sensor Lift Mechanism. Avcon Industries 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 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 SA890GL](https://openairdocs.org/stc/SA890GL): Install PARKER HANNIFIN CORPORATION aircraft wheel and brake DIVISION conversion kit 199-110,. KAMAN Corporation Aircraft Wheel and Brake LLC - [STC SA00415WI](https://openairdocs.org/stc/SA00415WI): Installation of a baggage door. Avcon Industries Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC - [STC SA01340LA](https://openairdocs.org/stc/SA01340LA): Installation of Sandel Avionics Terrain Awareness and Warning System. Sandel Avionics Inc - [STC SA01965WI](https://openairdocs.org/stc/SA01965WI): Installation of Wing Tip Hard Point Provisions. Avcon Industries Inc - [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc - [STC SA04062NY](https://openairdocs.org/stc/SA04062NY): Installation of Garmin G600 Avionics System. airplus engineering GmbH All 210: https://openairdocs.org/model/beech-a200-c-12c/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech A200](https://openairdocs.org/model/beech-a200): 17 registered aircraft, registry code 1152921 - [Leigh Aerosystems A200](https://openairdocs.org/model/leigh-aerosystems-a200): 1 registered aircraft, registry code 06102D7 --- 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.