# N60NE: 1978 Beech A36 - Status: Valid registration - Airframe: [Beech A36](https://openairdocs.org/model/beech-a36) (registry code 1151604, 6 seats) - Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032) - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15) (Textron Aviation Inc.), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (Continental Aerospace Technologies, Inc.) (OpenAirDocs) - Serial number: E-1209 - Year built: 1978 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, utility - Airworthiness date: January 13, 1978 - Certificate issued: September 25, 2014 - Expires: September 30, 2027 - Mode S code: A7C617 - Registered owner: [Cub Crafters Resale LLC](https://openairdocs.org/faa-owner/CUB%20CRAFTERS%20RESALE%20LLC) - Location: [Yakima, WA](https://openairdocs.org/faa-place/WA/Yakima) - Owner type: LLC - Owner's area on the map: 46.5300° N, 120.9410° W: Placed by OpenAirDocs at the center of ZIP code 98903, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=60NE - Page: https://openairdocs.org/aircraft/N60NE 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. The registry lists only the engine series, so ADs for every Continental IO-520 model are included. ## ADs that may apply (OpenAirDocs): 86 in force ### Matched by airframe (Beech A36) - [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 2010-13-10](https://openairdocs.org/ad/2010-13-10): Propeller governors · American Champion 7GCAA, DA 40, A36 and 1 more. Effective Aug 5, 2010 - [AD 2009-25-01](https://openairdocs.org/ad/2009-25-01): Shoulder harnessess · Textron 58, 58A, 58P and 12 more. Effective Jan 8, 2010 - [AD 2008-13-17](https://openairdocs.org/ad/2008-13-17): Circuit breaker toggle switches · Textron 58, 58P, 58TC and 14 more. Effective Aug 6, 2008 - [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 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 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 2005-01-19](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 2001-11-03](https://openairdocs.org/ad/2001-11-03): Blower Motor Circuit · Textron 1900D, 58, 58A and 5 more. Effective Jul 20, 2001 - [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 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 2000-24-04](https://openairdocs.org/ad/2000-24-04): Rudder Control Cables · Textron 58, A36 and B36TC. Effective Jan 5, 2001 - [AD 2000-20-14](https://openairdocs.org/ad/2000-20-14): Firewall Sealant · Textron A36 and B36TC. Effective Nov 28, 2000 - [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [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 99-09-15](https://openairdocs.org/ad/99-09-15): Flight Control Mechanism · Textron 1900D, 58, 58A and 5 more. Effective May 18, 1999 - [AD 98-14-03](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 95-04-03](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 93-03-02](https://openairdocs.org/ad/93-03-02): Loran Receiver System · Textron 58, A36, B36TC and 1 more. Effective Mar 12, 1993 - [AD 92-18-11](https://openairdocs.org/ad/92-18-11): Landing Gear Circuit · Textron A36 and B36TC. Effective Oct 18, 1992 - [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 91-20-08](https://openairdocs.org/ad/91-20-08): Fresh Air Blower Housing · Textron A36, A36TC, B36TC and 3 more. Effective Oct 31, 1991 - [AD 88-21-02](https://openairdocs.org/ad/88-21-02): Seat Tracks · Textron 58, 58A, 58P and 13 more. Effective Oct 31, 1988 - [AD 88-20-01](https://openairdocs.org/ad/88-20-01): Firewall Material · Textron A36, B36TC and F33A. Effective Oct 19, 1988 - [AD 87-18-06 R1](https://openairdocs.org/ad/87-18-06-R1): Seat Recline Actuator Handle · Textron 58, 58A, 58P and 9 more. Effective Feb 5, 1988 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [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 79-01-01](https://openairdocs.org/ad/79-01-01): Screws in Control System · Textron 100, 200, 35-B33 and 34 more. Effective Jan 8, 1979 - [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 76-22-02](https://openairdocs.org/ad/76-22-02): 'Y' Type Shoulder Harness · Textron 200, 58, 58A and 14 more. Effective Jun 2, 1977 - [AD 75-12-10](https://openairdocs.org/ad/75-12-10): Autopilots · M7 Aerospace 60, 95-C55, 95-C55A and 17 more. Effective Jun 11, 1975 - [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 74-24-03](https://openairdocs.org/ad/74-24-03): Strobe Light System · Textron 100, 200, 58 and 16 more. Effective Nov 22, 1974 - [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 74-03-02](https://openairdocs.org/ad/74-03-02): Landing Gear Shock Strut Piston · Textron 58, 58A, 95-B55 and 6 more. Effective Feb 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 73-14-03](https://openairdocs.org/ad/73-14-03): Landing Gear Shock Strut Piston · Textron 58, 58A, 95-B55 and 7 more. Effective Jul 6, 1973 - [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 ### Matched by engine (Continental IO-520 series) - [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023 - [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023 - [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023 - [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022 - [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016 - [AD 2014-05-29](https://openairdocs.org/ad/2014-05-29): SAP replacement parts manufacturer approval (PMA) investment cast cylinder assemblies · Continental Motors TSIO-520-A, TSIO-520-AE, TSIO-520-AF and 55 more. Effective Apr 25, 2014 - [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012 - [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010 - [AD 2009-19-07](https://openairdocs.org/ad/2009-19-07): EQ3 cylinders · Continental Motors IO-470-C, IO-470-D, IO-470-E and 72 more. Effective Oct 7, 2009 - [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007 - [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004 - [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000 - [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999 - [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998 - [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998 - [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995 - [AD 95-03-14](https://openairdocs.org/ad/95-03-14): Engine Mount Brackets · Continental Motors IO-346-A, IO-346-B, IO-520-C and 2 more. Effective Mar 13, 1995 - [AD 93-16-15](https://openairdocs.org/ad/93-16-15): Fuel Pump Drive Shaft · Continental Motors IO-520-B, IO-520-BA, IO-520-BB and 27 more. Effective Dec 14, 1993 - [AD 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993 - [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993 - [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991 - [AD 88-17-03](https://openairdocs.org/ad/88-17-03): Starter Adapter Shaftgear Assembly · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Aug 10, 1988 - [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988 - [AD 86-13-04 R3](https://openairdocs.org/ad/86-13-04-R3): Cylinder Assemblies · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 44 more. Effective Feb 24, 1988 - [AD 87-14-02](https://openairdocs.org/ad/87-14-02): Starter Adapter Shaftgear · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Oct 5, 1987 - [AD 81-24-06](https://openairdocs.org/ad/81-24-06): Engine Driven Fuel Pumps · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 51 more. Effective Nov 23, 1981 - [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981 - [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980 - [AD 80-01-04](https://openairdocs.org/ad/80-01-04): Cylinder Holddown Flange Assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 44 more. Effective Jan 25, 1980 - [AD 79-05-09](https://openairdocs.org/ad/79-05-09): Oil Pump Assembly Or Oil Pressure Relief Valve Screw And/Or Plunger · Teledyne Continental Motors 6-285-CA, GTSIO-520-C, GTSIO-520-D and 60 more. Effective Mar 12, 1979 - [AD 77-05-04](https://openairdocs.org/ad/77-05-04): Crankshaft · Continental Motors IO-470-L, IO-520-D, IO-520-F and 6 more. Effective Mar 11, 1977 - [AD 70-14-07](https://openairdocs.org/ad/70-14-07): Fuel Injection Pump · Continental Motors IO-360-A, IO-360-C, IO-360-D and 25 more. Effective Nov 22, 1974 - [AD 72-24-03](https://openairdocs.org/ad/72-24-03): Oil Filter Adapter · Continental Motors IO-360-A, IO-520-B, IO-520-C and 3 more. Effective Nov 15, 1972 - [AD 98-01-08](https://openairdocs.org/ad/98-01-08): Exhaust Roller Rocker Arm · Roller rocker arm P/N PE 92I intake and PE92E exhaust (Performance Engineering STC SE8594SW) - [AD 77-13-22](https://openairdocs.org/ad/77-13-22): Crankcase Cracks · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 22 more ### 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 - [AD 2000-26-16](https://openairdocs.org/ad/2000-26-16) (historical): Right Hand Fuselage Panel Assembly · Raytheon 58 Model or Series (all), A36 and B36TC. Effective Feb 16, 2001 - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 - [AD 91-18-19](https://openairdocs.org/ad/91-18-19) (historical): Pilot Shoulder Harnesses · Hawker Beechcraft 58 Model or Series (all), 58A, 58P and 11 more. Effective Oct 21, 1991 - [AD 72-22-01](https://openairdocs.org/ad/72-22-01) (historical): Landing Gear Uplock Rollers · Raytheon 35-33, 35-A33, 35-B33 and 49 more. Effective Oct 25, 1972 - [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023 - [AD 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Mar 29, 2022 - [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more - [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more - [AD 2009-16-03](https://openairdocs.org/ad/2009-16-03) (historical): Cylinder assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 55 more. Effective Sep 9, 2009 - [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more - [AD 94-09-07](https://openairdocs.org/ad/94-09-07) (historical): Engine Mount Brackets · Teledyne Continental Motors IO-346-A, IO-346-B, IO-520-C and 2 more. Effective Jul 5, 1994 - [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more - [AD 87-23-08](https://openairdocs.org/ad/87-23-08) (historical): Crankshafts · Teledyne Continental Motors IO-520 Series (all) and TSIO-520 Series (all). Effective Nov 30, 1987 - [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more All 101: https://openairdocs.org/aircraft/N60NE/ads.md ## Information bulletins (advisory) (17 in force) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-15-22](https://openairdocs.org/saib/CE-15-22): Wing Leading Edge Hinge-Pin Corrosion. Issued Sep 15, 2015 - [SAIB CE-13-22](https://openairdocs.org/saib/CE-13-22): Electrical Power System Circuit Breaker Switch. Issued Mar 13, 2013 - [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 NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020 - [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT Alternator Drive Coupling. Issued Jun 20, 2018 - [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT Engine damage as a result of kickback. Issued May 10, 2017 - [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016 - [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013 - [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012 - [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009 - [SAIB NE-10-07](https://openairdocs.org/saib/NE-10-07): Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.. Issued Nov 2, 2009 - [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009 - [SAIB NE-07-09R1](https://openairdocs.org/saib/NE-07-09R1): Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum Head. Issued Mar 21, 2007 - [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002 ## NTSB investigations None matched to N60NE. ## FAA accident and incident reports None matched to N60NE. ## Reports on N60NE not matched to an aircraft (3) They name N60NE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19990413020279I](https://openairdocs.org/incident/19990413020279I), Apr 13, 1999: Swrngn SA227AC (N60NE), Billings, MT. On 4/13/99, big sky airlines, inc., flight #1136, departed Billings, Montana. The fairchild SA-227-AC, N425MA, experienced a gear retraction failure. The right… - [Incident 19981112033719I](https://openairdocs.org/incident/19981112033719I), Nov 12, 1998: Swrngn SA227AC (N60NE), Billings, MT. On 11/12/98 big sky airlines, inc., flight number 1205, aircraft N60NE, experienced loss of nose wheel steering during take-off. The crew aborted take-off and… - [Incident 19980130003679I](https://openairdocs.org/incident/19980130003679I), Jan 30, 1998: Frchld SA227CC (N60NE), Missoula, MT, Minor damage. Narrative: on February 11, 1998, at approximately 1615 MST, a big sky airlines SA-227, flight 1204, being operated as a domestic airline under FAR part 121,… ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N60NE not matched to an aircraft (64, newest 50) They name N60NE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2005FA0000067](https://openairdocs.org/sdr/2005FA0000067), Jan 6, 2005: WARNING SYSTEM. MALFUNCTIONED. MRR-M05-3, CREW OBSERVED THE CABIN DOOR LIGHT CAME ON DURING CRUISE. CREW VERIFIED HANDLE WAS IN THE FULL CLOSED POSITION. THE LIGHT WENT OUT WHEN CABIN DIFFERE - [SDR 2005FA0000066](https://openairdocs.org/sdr/2005FA0000066), Jan 5, 2005: WARNING SYSTEM. MALFUNCTIONED. CREW OBSERVED THE CABIN DOOR LIGHT CAME ON DURING CRUISE. CREW VERIFIED HANDLE WAS IN THE FULL CLOSED POSITION. THE LIGHT WENT OUT DURING DESCENT, AND WAS ON FO - [SDR 2005FA0000051](https://openairdocs.org/sdr/2005FA0000051), Dec 26, 2004: INDICATOR. MALFUNCTIONED. NOTE: WRITTEN UP BY CREW AS DG PRECESSING. VERIFIED WITH MAINTENANCE THAT THE ATTITUDE INDICATOR WAS PRECESSING. BAD ATTITUDE INDICATOR. REMOVED AND REPLACED FO - [SDR 2005FA0000062](https://openairdocs.org/sdr/2005FA0000062), Dec 22, 2004: HANDLE. OUT OF RIG. CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT, CREW DESCENDED AND DEPRESSURIZED, AND THE LIGHT WENT OUT. CREW LANDED AT CLOSEST AIRPORT. FOUND CARGO DOOR HANDLE NO - [SDR 2005FA0000323](https://openairdocs.org/sdr/2005FA0000323), Sep 27, 2004: CLAMP. LOOSE. AFTER TAKEOFF, AT ABOUT 400 FT, NR 2 ENG FIRE WARNING LIGHT CAME ON. ENG PARAMETERS CHECKED NORMAL. CREW FOLLOWED EMERGENCY PROCEDURES, RETURNED TO FIELD. AFTER - [SDR 2005FA0000052](https://openairdocs.org/sdr/2005FA0000052), May 15, 2004: VANE. FAILED. MRR-M04-10, AIRCRAFT FILLED WITH SMOKE DURING LANDING. CREW TAXIED IN WITH NO FURTHER INCIDENT. SUSPECT ACM COOLING TURBINE FAILURE. INITIALLY DEFERRED THE NR 1 - [SDR 2004F00205](https://openairdocs.org/sdr/2004F00205), Nov 20, 2003: DOOR. STIFF. FLT 2587 - HLN - THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB AT 10,000 FT, CREW RETURNED TO STATION. SUSPECT DOOR CLOSING PROCEDURES WITH FULL BAGGAGE ARE - [SDR 2003F00118](https://openairdocs.org/sdr/2003F00118), Nov 25, 2002: ODOR. DETECTED. GGW - FLT 2568 - CREW REPORTED STRONG FOREIGN ODOR IN COCKPIT. RAN AIRCRAFT ON GROUND FOR APPROXIMATELY 30 MINUTES. UNABLE TO SMELL OR FEEL ANY HEAT. COULD NOT - [SDR 2002F00850](https://openairdocs.org/sdr/2002F00850), Mar 31, 2002: ACM. FAILED. FLT 2591 - GEG - DURING DESCENT, CO-PILOT NOTICED THE CABIN TEMP DIDN'T RESPOND TO TEMP CONTROLLER IN AUTO OR MANUAL MODE. THE CABIN TEMP KEPT ON RISING, AND PE - [SDR BSA2001F00000](https://openairdocs.org/sdr/BSA2001F00000), Jun 3, 2001: HYDRAULIC LINE. CHAFED. HYDRAULIC PRESSURE LOW LIGHT CAME ON DURING CLIMBOUT APPROX 25 MILES OUT. CREW SELECTED GEAR DOWN. ALL HYDRAULIC PRESSURE WAS LOST SHORTLY AFTER THAT. CREW COMP - [SDR MALA975455](https://openairdocs.org/sdr/MALA975455), Jun 6, 1997: COOLING TURBINE. FAILED. FLT 3235 - DURING APPROACH TO MSP, THE RIGHT BLEED WEMAC BLEW WARM AIR. AFTER LANDING THE WEMAC BEGAN EMITTING SMOKE. TAXIED WITH RIGHT BLEEDS OFF. MAINTENANCE - [SDR MALA975411](https://openairdocs.org/sdr/MALA975411), May 14, 1997: AIR DISTRIBUTION. ODOR. FLT 3211 - CREW NOTICED SMOKE IN CABIN DURING LANDING INTO PIR. MAINTENANCE PERFORMED TEST FLIGHT. NO DEFECTS FOUND. TEST FLIGHT SATISFACTORY. RETURNED TO SERVI - [SDR MALA975403](https://openairdocs.org/sdr/MALA975403), May 11, 1997: STRUT. REQ'D SERVICE. AFTER TAKEOFF THE NOSE GEAR RED INTRANSIT LIGHT WOULD NOT EXTINGUISH UPON GEAR RETRACTION. MAINTENANCE SERVICED NOSE LANDING GEAR STRUT. COMPLETED GEAR SWINGS. - [SDR MALA975352](https://openairdocs.org/sdr/MALA975352), Mar 20, 1997: DOUBLER. WORN. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FUOND THE LEFT FLAP WALKING BEAM ROLLER DOUBLER WORN BEYOND LIMITS. THE ROLLER DOUBLER P/N 27-31141-001 WAS RE - [SDR MALA975349](https://openairdocs.org/sdr/MALA975349), Mar 17, 1997: FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN LEFT SIDE OF LOWER CONSTANT SECTION RELIEF RADIUS AT FUSELAGE FRAME STATION 174. COM - [SDR MALA965255](https://openairdocs.org/sdr/MALA965255), Dec 21, 1996: DOOR MECH. OUT OF ADJUST. FLT 3016 - ON CLIMB-OUT FROM DTW, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. THE LIGHT EXTINGUISHED ON TOUCHDOWN. MAINTENANCE ADJU - [SDR MALA965221](https://openairdocs.org/sdr/MALA965221), Nov 27, 1996: DOOR SWITCH. OUT OF ADJUST. FLT 3192 - CLIMBING THROUGH 11,000 FEET, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE CREW PERFORMED QRH PROCEDURES AND THE CABIN WAS DEPRESSURIZED. THE AIRCR - [SDR MALA965060](https://openairdocs.org/sdr/MALA965060), Jun 30, 1996: AIR DISTR. SMOKE. FLT 3324 - AFTER LANDING IN LNK, THE CREW NOTED SMOKE COMING OUT OF THE LEFT GASPER VENT. THE SYSTEM WAS DEFERRED PER MEL 21-96. (M) - [SDR MALA964997](https://openairdocs.org/sdr/MALA964997), May 15, 1996: ACTUATOR. MALFUNCTIONED. FLT NR 3301 - ON CLIMB-OUT FROM DTW, THE NOSE GEAR CONTINUED TO CYCLE IN THE WHEEL WELL AFTER GEAR RETRACTION. THE RECYCLED THE GEAR, AND THE PROBLEM REMAINED. - [SDR MALA964993](https://openairdocs.org/sdr/MALA964993), May 15, 1996: DOOR. BENT. FLT 3060 - THE NOSE GEAR BEGAN TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND THE LOWER FORWARD CORNER OF THE NLG DOOR BENT OUT - [SDR MALA964960](https://openairdocs.org/sdr/MALA964960), Apr 17, 1996: ANGLE. WORN. DURING AN INSPECTION INS MSP, MAINTENANCE PERSONNEL AT FS 107 CAPTAINS SIDE INBOARD SEAT TRACK, BOX BEAM INBOARD SUPPORT ANGLE P/N 27-25008-005 WORN. REMOVED AN - [SDR MALA964959](https://openairdocs.org/sdr/MALA964959), Apr 17, 1996: SKIN. CRACKED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND ELEVATOR P/N 27-44001-161 TO HAVE INBOARD MOST LEADING EDGE SKIN PANEL CRACKED FROM SKIN EDGE TO RIVET - [SDR MALA964958](https://openairdocs.org/sdr/MALA964958), Apr 17, 1996: COVER PANEL. CRACKED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RIGHT WING EXTENSION AT TOP SKIN COVER PANEL, ONE SCREW HOLE CRACKED AND OTHERS WORN ELONGATED. LOC - [SDR MALA964957](https://openairdocs.org/sdr/MALA964957), Apr 17, 1996: STRUCTURE. CRACKED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND .300 CRACK IN CENTER SUB FLOOR STRUCTURE LIGHTING HOLE FLANGE JUST FORWARD OF FS 491.00. STOP DRILLED C - [SDR MALA964956](https://openairdocs.org/sdr/MALA964956), Apr 17, 1996: FRAME. DAMAGED. DURING AND INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND LOWER BELT FRAME AT FS 493.247 SLIGHTLY OIL CANNED HORIZONTALLY JUST ABOVE STRINGER PASS THROUGH AT FU - [SDR MALA964955](https://openairdocs.org/sdr/MALA964955), Apr 17, 1996: ANGLE. BROKEN RIVET. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED LOWER RIGHT OUTBOARD WING TO NACELLE TRANSIT ANGLE HAS A RIVET HEAD BROKEN HALF OFF AND A .125 INCH CRA - [SDR MALA964966](https://openairdocs.org/sdr/MALA964966), Apr 14, 1996: SKIN. DENTED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL COMPLETED REPAIR TO THE LEFT LOWER WING SKIN JUST FORWARD OF WING PANEL NR 663 DUE TO THREE SMALL DENTS BELOW - [SDR MALA964963](https://openairdocs.org/sdr/MALA964963), Apr 13, 1996: SKIN. DAMAGED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE PASSENGER DOOR SKIN AT FORWARD AND AFT HINGE CUT OUT CHAFFED AND DAMAGED. COMPLETED REPAIR BY REMOV - [SDR MALA964962](https://openairdocs.org/sdr/MALA964962), Apr 13, 1996: DOUBLER. WORN. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL REPAIRED WEAR TO RIGHT FLAP WALKING BEAM ROLLER DOUBLER BY REPLACING WITH A NEW DOUBLER P/N 27-31141 AND INST - [SDR MALA964961](https://openairdocs.org/sdr/MALA964961), Apr 13, 1996: RIB. CHAFED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB C - [SDR 96ZZZM928](https://openairdocs.org/sdr/96ZZZM928), Apr 13, 1996: HINGE ARM. DAMAGED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB C - [SDR 96ZZZM927](https://openairdocs.org/sdr/96ZZZM927), Apr 13, 1996: RIB. CRACKED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CR - [SDR 96ZZZM876](https://openairdocs.org/sdr/96ZZZM876), Apr 13, 1996: HINGE ARM. BENT. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CR - [SDR 96ZZZM875](https://openairdocs.org/sdr/96ZZZM875), Apr 13, 1996: RIB. CHAFED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INCH BY .500 INCH, OUTBOARD NOSE END RIB CR - [SDR MALA964965](https://openairdocs.org/sdr/MALA964965), Apr 11, 1996: SKIN. DENTED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND DENT DAMAGE TO LOWER FUSELAGE SKIN JUST AFT OF FS 493.247 AND ON BOTH LEFT AND RIGHT SIDE OF BL 0. COMB - [SDR MALA964964](https://openairdocs.org/sdr/MALA964964), Apr 11, 1996: SKIN. DAMAGED. DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED AFT CARGO DOOR SKIN AT FORWARD AND AFT HINGE CUT OUTS, SKIN CHAFED ADN DAMAGED. COMPLETED REPAIRS BY RE - [SDR MALA964928](https://openairdocs.org/sdr/MALA964928), Mar 22, 1996: UPLOCK SWITCH. FAILED. FLT NR 3353 - AFTER DEPARTURE FROM DTW, THE CREW NOTED THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT RETURNED TO DTW AN - [SDR MALA964899](https://openairdocs.org/sdr/MALA964899), Mar 6, 1996: RETRACT MECH. LACK OF LUBE. FLT NR 3271 - ON CLIMB-OUT FROM STC, THE NOSE GEAR BEGAN TO CYCLE AFTER THE GEAR WAS RETRACTED. THE CREW CYCLED THE GEAR UNTIL THE INTRANSIT LIGHT REMAINED EXTI - [SDR MALA964888](https://openairdocs.org/sdr/MALA964888), Feb 23, 1996: RETRACT MECH. MALFUNCTIONED. FLT NR 3370 - ON APPROACH TO DTW, THE NOSE GEAR INTRANSIT LIGHT WAS SLOW TO EXTINGUISH. THE PILOT ALSO REPORTED THAT, WHEN GEAR DID COME DOWN, IT CAME DOWN HARD - [SDR MALA964874](https://openairdocs.org/sdr/MALA964874), Feb 16, 1996: RETRACT MECH. MALFUNCTIONED. FLT NR 3345 - EN ROUTE FROM DTW TO CRW, THE NOSE GEAR INTRANSIT LIGHT ILLUMINATED AND THE NOSE GEAR BEGAN TO CYCLE IN THE GEAR WELL. THE CREW ELECTED TO RETURN - [SDR MALA964871](https://openairdocs.org/sdr/MALA964871), Feb 16, 1996: UPLOCK HOOK. WORN. FLT NR 3395 - EN ROUTE TO CRW, THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR BEGAN TO CYCLE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE - [SDR MALA964837](https://openairdocs.org/sdr/MALA964837), Jan 22, 1996: POSITION SW. FAILED. FLT NR 3027 - ON CLIMB-OUT FROM GPS, THE NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. ALL OTHER INDICATIONS WERE NORMAL. THE LIGHT ALSO - [SDR MALA954738](https://openairdocs.org/sdr/MALA954738), Dec 8, 1995: POSITION SW. OUT OF ADJUST. FLT NR 3226 - AFTER DEPARTURE FROM MSP, THE NOSE GEAR CYCLED IN THE WHEEL WELL. THE CREW ELECTED TO RETURN TO MSP, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAI - [SDR MALA954674](https://openairdocs.org/sdr/MALA954674), Oct 20, 1995: RADAR SCREEN. FAILED. FLT NR 3018 - IN CRUISE FLIGHT, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR INDICATOR. SYSTEM OPE - [SDR MALA954656](https://openairdocs.org/sdr/MALA954656), Oct 6, 1995: STEER MANIFOLD. FAILED. FLT NR 3350 - DURING THE LANDING ROLL IN EVV, THE AIRCRAFT VEERED TO THE RIGHT BELOW 60 KTS PRIOR TO ENGAGING THE STEERING BUTTON. THE CREW APPLIED THE LEFT BRA - [SDR MALA954590](https://openairdocs.org/sdr/MALA954590), Aug 20, 1995: SKIN. DENTED. MSP - DURING A SCHEDULED INSPECTION, THE RIGHT LOWER WING SKIN WAS FOUND DENTED AT WS 197.00. REPAIRS WERE COMPLETED BY INSTALLING A SURFACE DOUBLER AW FAC SRM - [SDR MALA954556](https://openairdocs.org/sdr/MALA954556), Jul 29, 1995: INDICATOR. FAILED. FNT - FLT 3440 - DURING APPROACH, CREW DID NOT GET A GREEN 'GEAR DOWN AND LOCKED' INDICATION WHEN THE GEAR WAS SELECTED DOWN. AFTER A VISUAL INSPECTION BY ATC P - [SDR MALA954500](https://openairdocs.org/sdr/MALA954500), Jun 8, 1995: ANGLE. CRACKED. MSP - DURING SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE RT LOWER WING TO NACELLE TRANSIT ANGLE WAS CRACKED AT THE LEADING EDGE. MAINTENANCE RE - [SDR MALA954474](https://openairdocs.org/sdr/MALA954474), May 25, 1995: ANGLE. CRACKED. MSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LT INBOARD UPPER WING TO NACELLE ANGLE PN 27-335112 FORWARD END AT STA 115.00 CRACKED APPROXIMATELY 1 IN - [SDR MALA954473](https://openairdocs.org/sdr/MALA954473), May 25, 1995: ANGLE. CRACKED. MSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LEFT INBOARD LOWER WING TO NACELLE ANGLE PN 27-35112 FORWARD END, AT APPROXIMATE STA 115.00 CRACKED APPR All 64: https://openairdocs.org/aircraft/N60NE/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (577, 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 A36) - [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 SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. 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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc - [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 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. Lists 36 Series - [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 SA228CH](https://openairdocs.org/stc/SA228CH): Installation of Model TCAS 791 TCAS I. Acron Aviation Inc - [STC SA306CH](https://openairdocs.org/stc/SA306CH): Installation of a Sextant VSI TCAS display. 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 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 SA00639SE](https://openairdocs.org/stc/SA00639SE): Installation of Turbine Outlet Temperature Indicator. DV Aviation Inc - [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. Lists 36 Series - [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 All 577: https://openairdocs.org/aircraft/N60NE/stcs.md ## Related - Other Beech A36 aircraft: https://openairdocs.org/model/beech-a36/aircraft.md - The Continental IO-520 series engine: https://openairdocs.org/engine/continental-io-520-series.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.