# N361BC: Beech 36 - Status: Valid registration - Airframe: [Beech 36](https://openairdocs.org/model/beech-36) (registry code 1151602, 6 seats) - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15) (Textron Aviation Inc.) (OpenAirDocs) - Serial number: E1331 - Type: Fixed wing single engine - Engine type: Reciprocating - Certificate issued: February 5, 2007 - Expires: January 31, 2030 - Mode S code: A4101F - Registered owner: [Gta Air Inc](https://openairdocs.org/faa-owner/GTA%20AIR%20INC) - Location: [Addison, TX](https://openairdocs.org/faa-place/TX/Addison) - Owner type: Corporation - Owner's area on the map: 32.9600° N, 96.8372° W: Placed by OpenAirDocs at the center of ZIP code 75001, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=361BC - Page: https://openairdocs.org/aircraft/N361BC From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 31 in force ### Matched by airframe (Beech 36) - [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024 - [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023 - [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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2019-23-10](https://openairdocs.org/ad/2019-23-10): Aileron Control System · Textron 35-C33, 35-C33A, 36 and 12 more. Effective Nov 22, 2019 - [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 2007-08-08](https://openairdocs.org/ad/2007-08-08): Uplock roller · Textron 35, 35-33, 35-A33 and 49 more. Effective May 25, 2007 - [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 2003-01-01](https://openairdocs.org/ad/2003-01-01): Right hand fuselage panel assembly · Textron 36, 58, 58A and 3 more. Effective Feb 27, 2003 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2001-23-10](https://openairdocs.org/ad/2001-23-10): Flap Flex Shaft Assemblies · Textron 35, 35-33, 35-A33 and 60 more. Effective Dec 13, 2001 - [AD 2001-08-08](https://openairdocs.org/ad/2001-08-08): V-band Exhaust Clamp · Modified Teledyne Continental engine equipped (STC SA5223NM or 2 others). Effective Jun 7, 2001 - [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998 - [AD 97-16-10](https://openairdocs.org/ad/97-16-10): Filters · Cessna 310R, T310R, 36 and 17 more. Effective Sep 18, 1997 - [AD 97-14-15](https://openairdocs.org/ad/97-14-15): Cabin Side Door And Utility Door Handle · Textron 36, 50, 56TC and 41 more. Effective Sep 2, 1997 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995 - [AD 95-04-03](https://openairdocs.org/ad/95-04-03): Wing Spar · Textron 35-33, 35-A33, 35-B33 and 23 more. Effective Apr 7, 1995 - [AD 93-24-03](https://openairdocs.org/ad/93-24-03): Rudder Forward Spar · Textron 35-33, 35-A33, 35-B33 and 13 more. Effective Jan 21, 1994 - [AD 91-17-01](https://openairdocs.org/ad/91-17-01): Elevator Trim Tab Actuators · Textron 35-33, 35-A33, 35-B33 and 40 more. Effective Nov 25, 1991 - [AD 89-05-02](https://openairdocs.org/ad/89-05-02): Elevator Control Fittings · Textron 35, 35-33, 35-A33 and 42 more. Effective Mar 24, 1989 - [AD 84-09-01](https://openairdocs.org/ad/84-09-01): Window Emergency Egress Provision · Textron 35, 36, 50 and 60 more. Effective May 25, 1984 - [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978 - [AD 75-05-02](https://openairdocs.org/ad/75-05-02): Engine Oil · Beryl D Shannon Aviation Specialties Engine Crankcase… (D'Shannon Products STC SA2653WE). Effective Feb 21, 1975 - [AD 74-12-02](https://openairdocs.org/ad/74-12-02): Aft Facing Seats · Textron 36, 58, 58A and 3 more. Effective Jun 5, 1974 - [AD 71-24-10](https://openairdocs.org/ad/71-24-10): Security of Control Wheel · Textron 35-C33, 35-C33A, 36 and 21 more. Effective Aug 1, 1973 - [AD 70-03-05](https://openairdocs.org/ad/70-03-05): Turning Type Takeoffs · Textron 35-33, 35-A33, 35-B33 and 16 more. Effective Jun 30, 1972 - [AD 72-11-02](https://openairdocs.org/ad/72-11-02): Engine Fuel Interruption · Textron 35, 35-33, 35-A33 and 48 more. Effective May 20, 1972 - [AD 70-12-02](https://openairdocs.org/ad/70-12-02): Seat Tracks · Textron 36 and A36. Effective Jun 9, 1970 ### Historical (superseded or no longer in force) - [AD 2019-21-08](https://openairdocs.org/ad/2019-21-08) (historical): Aileron Control System · Textron 35-C33, 35-C33A, 36 and 16 more. Effective Nov 22, 2019 ## Information bulletins (advisory) (5 in force) - [SAIB CE-15-22](https://openairdocs.org/saib/CE-15-22): Wing Leading Edge Hinge-Pin Corrosion. Issued Sep 15, 2015 - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 - [SAIB CE-12-18](https://openairdocs.org/saib/CE-12-18): Flight Controls: Elevator Control Cable Condition. Issued Feb 7, 2012 - [SAIB CE-11-21](https://openairdocs.org/saib/CE-11-21): Flight Controls: Trailing Edge Flaps; Flap Nose Rib Cracking. Issued Feb 16, 2011 - [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002 ## NTSB investigations None matched to N361BC. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20120406006119I](https://openairdocs.org/incident/20120406006119I), Apr 6, 2012: Beech 36 (N361BC), Tyler, TX, No damage. Gta air (gtx)602, a BE-36, suffered brake problem while landing at Tyler at 1925 central time on April 6 2012. The aircraft turned off the runway onto taxiway… - [Incident 20060414004809I](https://openairdocs.org/incident/20060414004809I), Apr 14, 2006: Beech 36BEECH (N361BC), Abilene, TX, Minor damage. (-23) On April 14, 2006, at approximately 2000 CDT, the pilot of N361BC, a Beechcraft BE-A36, failed to lower the landing gear and subsequently made a gear-up… ## Service difficulty reports (8) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR XGNA2012F00003](https://openairdocs.org/sdr/XGNA2012F00003), Oct 3, 2012: CIRCUIT BREAKER. INTERMITTENT. LANDING LIGHT CIRCUIT BREAKER INTERMITTENT. THIS CIRCUIT BREAKER WAS REPLACED BY AD2008-13-17 IAW SB24-3807. NEW SWITCH CALLED FOR IN THE AD/SB 34-24-3807 IS IN - [SDR XGN2012F00002](https://openairdocs.org/sdr/XGN2012F00002), Aug 9, 2012: ROD END. CRACKED. LT MAIN INBD GEAR DOOR ACTUATING LINK ASSY, PN 35-815227-4 INBD ROD END, PN 131553-4M CRACKED THRU THE THREADED SHANK OF THE ROD END. - [SDR XGN2012F00000](https://openairdocs.org/sdr/XGN2012F00000), Apr 6, 2012: O-RING. DAMAGED. LEFT BRAKE CALIPER LOWER O-RING EDGE WAS DAMAGED FROM DEBRIS AND THE CALIPER WOULD NOT HOLD FULL FLUID PRESSURE. - [SDR XGN2006F00026](https://openairdocs.org/sdr/XGN2006F00026), Apr 6, 2006: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2001F00001](https://openairdocs.org/sdr/XGN2001F00001), Aug 2, 2001: ROD BOLT. BROKEN. ROD BOLT BROKE ON NR 6 CYLINDER, WHILE AIRCRAFT WAS ON FINAL APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ENGINE WAS DESTROYED. - [SDR 97ZZZX3324](https://openairdocs.org/sdr/97ZZZX3324), Jul 8, 1997: PUMP. FAILED. VACUUM PUMP FAILED. BOTH FILTERS CHANGED. REASON FOR FAILURE, UNKNOWN AT THIS TIME. - [SDR 97ZZZX3095](https://openairdocs.org/sdr/97ZZZX3095), Jun 12, 1997: CYLINDER. CRACKED. INSPECTION FOUND NR 4 CYLINDER CRACKED. CRACK RUNS FROM EXHAUST. - [SDR 98ZZZX689](https://openairdocs.org/sdr/98ZZZX689), Jan 7, 1997: PUMP. FAILED. DEPARTED AIRPORT AND WITHIN 30 MINUTES VACUUM PUMP BROKE. RETURNED TO BASE. NO OTHER TROUBLE. ## STCs that may be installed (OpenAirDocs) (390, first 50) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Beech 36) - [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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA04505CH](https://openairdocs.org/stc/SA04505CH): Installation of Hartzell Propeller model HC-C3YF-1N/NM8410-4 or HC-C3YF-1N/NM8410K-4. Hartzell Propeller Inc - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International 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 SA12416IB](https://openairdocs.org/stc/SA12416IB): Installation of Main wheel, Nose wheel, brake assembly, axle, master cylinder and brake lines. BERINGER AERO - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA4103WE](https://openairdocs.org/stc/SA4103WE): Installation of a replacement flexible fuel cell in the wing of the Beech 33, 35, 36. aircraft. Aerosport Fuel Cells, LLC - [STC SA01152CH](https://openairdocs.org/stc/SA01152CH): Installation of stainless steel passenger step, P/N 002-430076-23, with South Seas Ventures, Inc. drawing as listed on AML No. SA01152CH, or later FAA approved revision. McFarlane Aviation LLC - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC - [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 SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA00423SE](https://openairdocs.org/stc/SA00423SE): Installation of stainless steel battery box. CheckSix AeroSolutions, LLC - [STC SA5902NM](https://openairdocs.org/stc/SA5902NM): Installation of locking fuel cap assembly. CheckSix AeroSolutions, LLC - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA2754CE](https://openairdocs.org/stc/SA2754CE): Installation of a flap actuated landing gear warning system. Walter Timothy Miller - [STC SA02024WI](https://openairdocs.org/stc/SA02024WI): Installation of the Aft Auxiliary Heating System (AAHS). Peregrine - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC - [STC SA04537CH](https://openairdocs.org/stc/SA04537CH): Installation of wingtip position/anti-collision light support bracket. Gallagher Aviation LLC - [STC SA01561CH](https://openairdocs.org/stc/SA01561CH): Installation of Hartzell Model PHC-(C, L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines. D'Shannon Products Ltd - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp - [STC SA02535CH](https://openairdocs.org/stc/SA02535CH): Installation of M-T Propeller, Inc model MTV-9-D/205-58 or MTV-9-D/210-58 propeller. McFarlane Aviation LLC - [STC SA01422AT-D](https://openairdocs.org/stc/SA01422AT-D): Installation of Lower Cabin Door Stiffener. Summit Aviation Inc - [STC SA02314AT-D](https://openairdocs.org/stc/SA02314AT-D): Installation of a stainless steel exhaust system. Summit Aviation Inc - [STC SA10145SC-D](https://openairdocs.org/stc/SA10145SC-D): Installation of a Teledyne Continental Motors Model IO-550-R engine. Summit Aviation Inc - [STC SA00638WI](https://openairdocs.org/stc/SA00638WI): Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. Aero-Mach Wilco LLC - [STC SA11GL](https://openairdocs.org/stc/SA11GL): Installation of Cleveland 6.00-6wheels and brakes conversion kit 199-49. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA01904WI](https://openairdocs.org/stc/SA01904WI): Installation of LED Position and Recognition Lights. Whelen Aerospace Technologies - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). 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 SA00469NY](https://openairdocs.org/stc/SA00469NY): Installation of Main Landing Gear Auxiliary Landing Lights. Gallagher Aviation LLC - [STC SA00901NY](https://openairdocs.org/stc/SA00901NY): Installation of a wing tip recognition lights. Gallagher Aviation LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc All 390: https://openairdocs.org/aircraft/N361BC/stcs.md ## Related - Other Beech 36 aircraft: https://openairdocs.org/model/beech-36/aircraft.md --- 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.