# Swearingen SA-226T - Type: Aircraft model (FAA registry) - Registry code: 8780122 - Manufacturer (registry): SWEARINGEN - Model: SA-226T - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 8 - Weight class: Up to 12,499 lb - Cruise speed: 180 mph - Certification: Type certificated - Data sheet: [TCDS A5SW](https://openairdocs.org/tcds/A5SW) (OpenAirDocs) - Holder: Ontic Engineering and Manufacturing Inc. - Registered aircraft: 21 - Page: https://openairdocs.org/model/swearingen-sa-226t 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 2026-21-13](https://openairdocs.org/ad/2026-21-13): Elevator Tab Control System · Ontic Engineering and Manufacturing SA226-T, SA226-AT, SA226-T(B) and 8 more. Effective Dec 1, 2026 - [AD 2017-07-01](https://openairdocs.org/ad/2017-07-01): Propellers/Propulsors · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective May 5, 2017 - [AD 2016-25-12](https://openairdocs.org/ad/2016-25-12): Horizontal Stabilizer Structure · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Jan 12, 2017 - [AD 2016-15-02](https://openairdocs.org/ad/2016-15-02): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Aug 26, 2016 - [AD 2016-10-01](https://openairdocs.org/ad/2016-10-01): Elevator Control System · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Jun 15, 2016 - [AD 2015-19-10](https://openairdocs.org/ad/2015-19-10): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Nov 3, 2015 - [AD 2015-13-10](https://openairdocs.org/ad/2015-13-10): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 1 more. Effective Jul 21, 2015 - [AD 2014-09-02](https://openairdocs.org/ad/2014-09-02): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Jun 5, 2014 - [AD 2014-06-01](https://openairdocs.org/ad/2014-06-01): Fuselage Main, Bulkhead · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Apr 25, 2014 - [AD 2012-18-01](https://openairdocs.org/ad/2012-18-01): Wing, Fuselage Attach Fitting · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Sep 21, 2012 - [AD 2011-02-04](https://openairdocs.org/ad/2011-02-04): Flight Compartment Windows · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Jan 24, 2011 - [AD 2009-11-06](https://openairdocs.org/ad/2009-11-06): Hydraulic tube assemblies · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Jul 2, 2009 - [AD 2007-16-03](https://openairdocs.org/ad/2007-16-03): Pitch trim actuators · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 8 more. Effective Sep 7, 2007 - [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 2005-06-13](https://openairdocs.org/ad/2005-06-13): Wing spar center web cutout · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 2, 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 2003-19-10](https://openairdocs.org/ad/2003-19-10): Fuel boost pump · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 8 more. Effective Nov 7, 2003 - [AD 2002-08-02](https://openairdocs.org/ad/2002-08-02): Brake Shuttle Valves · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jun 6, 2002 - [AD 2002-08-01](https://openairdocs.org/ad/2002-08-01): Brake Master Cylinders · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jun 6, 2002 - [AD 2002-01-16](https://openairdocs.org/ad/2002-01-16): Dual Engine Flameout · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Mar 11, 2002 - [AD 2000-17-01](https://openairdocs.org/ad/2000-17-01): Brake System · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Oct 6, 2000 - [AD 2000-17-11](https://openairdocs.org/ad/2000-17-11): Main Landing Gear (MLG) Assemblies · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Sep 22, 2000 - [AD 2000-06-04](https://openairdocs.org/ad/2000-06-04): Pneumatic Deicing Boots · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 8 more. Effective May 5, 2000 - [AD 99-21-05](https://openairdocs.org/ad/99-21-05): Landing Gear Actuator Rod Ends · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 1 more. Effective Nov 16, 1999 - [AD 98-04-05](https://openairdocs.org/ad/98-04-05): Wing Trailing Edge Ribs · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 1 more. Effective Mar 10, 1998 - [AD 97-11-13](https://openairdocs.org/ad/97-11-13): Generator Fault Transformer Wiring · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jul 11, 1997 - [AD 97-10-13](https://openairdocs.org/ad/97-10-13): Elevator Torque Tube Arm · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Jul 8, 1997 - [AD 97-01-12](https://openairdocs.org/ad/97-01-12): Ground Proximity Warning System · Airtell International Ground Proximity Warning System, Mystere-Falcon 200, EMB-110P1 and 20 more. Effective Feb 25, 1997 - [AD 96-20-08](https://openairdocs.org/ad/96-20-08): Replace Side Cockpit Window · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Nov 14, 1996 - [AD 96-19-05](https://openairdocs.org/ad/96-19-05): Main Landing Gear or Nose Landing Gear Assemblies or Yokes · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Oct 1, 1996 - [AD 96-09-16](https://openairdocs.org/ad/96-09-16): Airplane Flight Manual (AFM) - Icing · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Jun 11, 1996 - [AD 95-17-09 R1](https://openairdocs.org/ad/95-17-09-R1): Essential Bus Current Limiters · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 13, 1996 - [AD 94-07-10 R1](https://openairdocs.org/ad/94-07-10-R1): Upper Wing Skin Inspection · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 25, 1996 - [AD 96-03-03](https://openairdocs.org/ad/96-03-03): Power Control Cable Safety Wire Nuts · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 15, 1996 - [AD 95-25-07](https://openairdocs.org/ad/95-25-07): Main Landing Gear Actuator Tangs & Hardware · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 1 more. Effective Jan 17, 1996 - [AD 95-24-11](https://openairdocs.org/ad/95-24-11): Foreign Object Damage Barriers In Floorboards · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Jan 3, 1996 - [AD 95-17-07](https://openairdocs.org/ad/95-17-07): Main Landing Gear Doors · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 1 more. Effective Aug 28, 1995 - [AD 93-15-01](https://openairdocs.org/ad/93-15-01): Horizontal Stabilizer Pivot Fitting Fasteners · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Sep 16, 1993 - [AD 93-07-12](https://openairdocs.org/ad/93-07-12): Horizontal Stabilizer Rear Spar Inspection · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective May 28, 1993 - [AD 92-19-08](https://openairdocs.org/ad/92-19-08): Rudder Pedal Link Attachment · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Oct 16, 1992 - [AD 92-18-07](https://openairdocs.org/ad/92-18-07): Power Lever Detent Arms · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Oct 2, 1992 - [AD 90-24-03](https://openairdocs.org/ad/90-24-03): Rudder Trim Link Assemblies · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 10 more. Effective Jan 25, 1991 - [AD 85-22-06 R1](https://openairdocs.org/ad/85-22-06-R1): Stall Avoidance System (SAS) · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Oct 19, 1990 - [AD 90-03-19 R1](https://openairdocs.org/ad/90-03-19-R1): Electrical System · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Aug 15, 1990 - [AD 90-05-06 R1](https://openairdocs.org/ad/90-05-06-R1): Main Landing Gear Doors · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Aug 13, 1990 - [AD 87-13-11](https://openairdocs.org/ad/87-13-11): Landing Gear Selector · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 3 more. Effective Aug 10, 1987 - [AD 87-02-02](https://openairdocs.org/ad/87-02-02): Primary Control Cables · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jan 27, 1987 - [AD 86-10-08](https://openairdocs.org/ad/86-10-08): Elevator Gust Lock System · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective May 28, 1986 - [AD 85-04-01 R1](https://openairdocs.org/ad/85-04-01-R1): Hydraulic And Oxygen Line Inspection · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 1 more. Effective Oct 28, 1985 - [AD 83-15-09](https://openairdocs.org/ad/83-15-09): Nose Wheel Steering System Modification · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 4 more. Effective Sep 8, 1983 Historical (superseded or no longer in force): - [AD 2011-17-07](https://openairdocs.org/ad/2011-17-07) (historical): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 1 more. Effective Sep 1, 2011 - [AD 2008-12-16](https://openairdocs.org/ad/2008-12-16) (historical): Left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jul 23, 2008 - [AD 2001-20-14](https://openairdocs.org/ad/2001-20-14) (historical): Brake Shuttle Valves · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 4 more. Effective Nov 21, 2001 - [AD 2000-03-17](https://openairdocs.org/ad/2000-03-17) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Apr 10, 2000 - [AD 98-19-15 R1](https://openairdocs.org/ad/98-19-15-R1) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 3, 2000 - [AD 99-06-02](https://openairdocs.org/ad/99-06-02) (historical): Wing Spar Center Web · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Apr 16, 1999 - [AD 98-19-15](https://openairdocs.org/ad/98-19-15) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Sep 25, 1998 - [AD 97-23-01](https://openairdocs.org/ad/97-23-01) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Dec 1, 1997 - [AD 97-02-02](https://openairdocs.org/ad/97-02-02) (historical): Control Column Pitch Bearing Attaching Nuts · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 9 more. Effective Feb 6, 1997 - [AD 93-15-02 R2](https://openairdocs.org/ad/93-15-02-R2) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Jul 25, 1996 - [AD 94-07-10](https://openairdocs.org/ad/94-07-10) (historical): Upper Wing Skin Inspection · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 27, 1994 - [AD 92-01-02](https://openairdocs.org/ad/92-01-02) (historical): Parking Brake System · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jan 16, 1992 - [AD 86-24-11](https://openairdocs.org/ad/86-24-11) (historical): POH/AFM Appendix - Icing · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 1 more. Effective Dec 15, 1986 - [AD 74-24-02 R1](https://openairdocs.org/ad/74-24-02-R1) (historical): Horizontal Stabilizer Rear Spar · M7 Aerospace LP SA226-AT, SA226-T and SA226-TC. Effective Mar 8, 1976 - [AD 74-24-02](https://openairdocs.org/ad/74-24-02) (historical): Horizontal Stabilizer Rear Spar · M7 Aerospace LP SA226-AT, SA226-T and SA226-TC. Effective Mar 8, 1976 All 74: https://openairdocs.org/model/swearingen-sa-226t/ads.md ## Information bulletins (advisory) (15) - [SAIB 2026-15](https://openairdocs.org/saib/2026-15): Forward Pressure Bulkhead. Issued Sep 9, 2026 - [SAIB 2026-14](https://openairdocs.org/saib/2026-14): Rudder Control System, Brake. Issued Aug 25, 2026 - [SAIB CE-18-11](https://openairdocs.org/saib/CE-18-11): Flight Controls, Elevator Control System. Issued Feb 9, 2018 - [SAIB CE-17-04](https://openairdocs.org/saib/CE-17-04): Landing Gear, Main Landing Gear. Issued Dec 16, 2016 - [SAIB CE-16-06](https://openairdocs.org/saib/CE-16-06): Flight Controls, Rudder Control System. Issued Nov 20, 2015 - [SAIB CE-16-04](https://openairdocs.org/saib/CE-16-04): Engine Controls, Power Lever. Issued Nov 2, 2015 - [SAIB CE-15-09](https://openairdocs.org/saib/CE-15-09): Windows; Flight Compartment Windows. Issued Feb 24, 2015 - [SAIB CE-15-05R1](https://openairdocs.org/saib/CE-15-05R1): Flight Controls, Aileron Control System. Issued Nov 26, 2014 - [SAIB CE-15-05](https://openairdocs.org/saib/CE-15-05) (historical): Flight Controls, Aileron Control System. Issued Nov 25, 2014 - [SAIB CE-13-42](https://openairdocs.org/saib/CE-13-42): Wings, Ailerons. Issued Aug 1, 2013 - [SAIB CE-13-41](https://openairdocs.org/saib/CE-13-41): Landing Gear, Landing Gear Actuator. Issued Jul 23, 2013 - [SAIB CE-13-10](https://openairdocs.org/saib/CE-13-10): Windshield/Door Rain/Ice Removal. Issued Dec 21, 2012 - [SAIB CE-12-08](https://openairdocs.org/saib/CE-12-08): Flight Controls, Elevator Control System. Issued Nov 8, 2011 - [SAIB CE-11-32](https://openairdocs.org/saib/CE-11-32): Engine Mount Section. Issued May 11, 2011 - [SAIB CE-11-26](https://openairdocs.org/saib/CE-11-26): Wings: Wing Skin. Issued Mar 30, 2011 ## Registered aircraft (21) - [N101MC](https://openairdocs.org/aircraft/N101MC): [Marc Inc](https://openairdocs.org/faa-owner/MARC%20INC), [Bolton, MS](https://openairdocs.org/faa-place/MS/Bolton), built 1973, S/N T234 - [N226XX](https://openairdocs.org/aircraft/N226XX): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1974, S/N T245 - [N25677](https://openairdocs.org/aircraft/N25677): [Hometown LLC](https://openairdocs.org/faa-owner/HOMETOWN%20LLC), [Cleburne, TX](https://openairdocs.org/faa-place/TX/Cleburne), S/N T-254 - [N279M](https://openairdocs.org/aircraft/N279M): [L And L Investment LLC](https://openairdocs.org/faa-owner/L%20AND%20L%20INVESTMENT%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N T279 - [N303MA](https://openairdocs.org/aircraft/N303MA): [Hutchison Aviation LLC](https://openairdocs.org/faa-owner/HUTCHISON%20AVIATION%20LLC), [Alpharetta, GA](https://openairdocs.org/faa-place/GA/Alpharetta), S/N T278 - [N307PA](https://openairdocs.org/aircraft/N307PA): [Tgf Aviation LLC](https://openairdocs.org/faa-owner/TGF%20AVIATION%20LLC), [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette), S/N T307 - [N360LG](https://openairdocs.org/aircraft/N360LG): [N360lg LLC](https://openairdocs.org/faa-owner/N360LG%20LLC), [Helena, MT](https://openairdocs.org/faa-place/MT/Helena), built 1979, S/N T322 - [N377YB](https://openairdocs.org/aircraft/N377YB): [Moses International Inc](https://openairdocs.org/faa-owner/MOSES%20INTERNATIONAL%20INC), [Bellevue, MI](https://openairdocs.org/faa-place/MI/Bellevue), built 1978, S/N T-289 - [N400RT](https://openairdocs.org/aircraft/N400RT): [Wagner Air LLC](https://openairdocs.org/faa-owner/WAGNER%20AIR%20LLC), [Kendalia, TX](https://openairdocs.org/faa-place/TX/Kendalia), built 1979, S/N T-311 - [N46SA](https://openairdocs.org/aircraft/N46SA): [Hopland Steven](https://openairdocs.org/faa-owner/HOPLAND%20STEVEN), [Johnson City, TN](https://openairdocs.org/faa-place/TN/Johnson%20City), built 1973, S/N T231 - [N505GM](https://openairdocs.org/aircraft/N505GM): [Nc Hold 7 LLC](https://openairdocs.org/faa-owner/NC%20HOLD%207%20LLC), [Raleigh, NC](https://openairdocs.org/faa-place/NC/Raleigh), built 1977, S/N T286 - [N50MT](https://openairdocs.org/aircraft/N50MT): [Odaniel Trey](https://openairdocs.org/faa-owner/ODANIEL%20TREY), [Bennington, NE](https://openairdocs.org/faa-place/NE/Bennington), built 1979, S/N T308 - [N5441M](https://openairdocs.org/aircraft/N5441M): [Ca Aviation Inc](https://openairdocs.org/faa-owner/CA%20AVIATION%20INC), [Springfield, MO](https://openairdocs.org/faa-place/MO/Springfield), built 1977, S/N T-283 - [N616PS](https://openairdocs.org/aircraft/N616PS): [Dena'Ina Leasing Agency LLC](https://openairdocs.org/faa-owner/DENA'INA%20LEASING%20AGENCY%20LLC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1979, S/N T316 - [N699KM](https://openairdocs.org/aircraft/N699KM): [Merlin Cattle Co LLC](https://openairdocs.org/faa-owner/MERLIN%20CATTLE%20CO%20LLC), [El Paso, TX](https://openairdocs.org/faa-place/TX/El%20Paso), built 1975, S/N T256 - [N749L](https://openairdocs.org/aircraft/N749L): [Geco Inc](https://openairdocs.org/faa-owner/GECO%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N T306 - [N75MX](https://openairdocs.org/aircraft/N75MX): [National Test Pilot School](https://openairdocs.org/faa-owner/NATIONAL%20TEST%20PILOT%20SCHOOL), [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave), S/N T-218 - [N772SL](https://openairdocs.org/aircraft/N772SL): [Kc Aviation Holdings LLC](https://openairdocs.org/faa-owner/KC%20AVIATION%20HOLDINGS%20LLC), [Tonopah, NV](https://openairdocs.org/faa-place/NV/Tonopah), S/N T258 - [N800LD](https://openairdocs.org/aircraft/N800LD): [N800ld LLC](https://openairdocs.org/faa-owner/N800LD%20LLC), [Galveston, TX](https://openairdocs.org/faa-place/TX/Galveston), S/N T291 - [N9900](https://openairdocs.org/aircraft/N9900): [Marc Inc](https://openairdocs.org/faa-owner/MARC%20INC), [Bolton, MS](https://openairdocs.org/faa-place/MS/Bolton), built 1976, S/N T-266 - [N9NZ](https://openairdocs.org/aircraft/N9NZ): [Qe 2 Holdings LLC](https://openairdocs.org/faa-owner/QE%202%20HOLDINGS%20LLC), [Prescott Valley, AZ](https://openairdocs.org/faa-place/AZ/Prescott%20Valley), S/N T255 ## NTSB investigations (25) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN16WA179](https://openairdocs.org/ntsb/CEN16WA179), Apr 26, 2016: Swearingen SA 226T (N125WG), Andorra, Lleida, Spain, Spain, substantial damage - [NTSB CHI07LA108](https://openairdocs.org/ntsb/CHI07LA108), Apr 11, 2007: Swearingen SA-226T (N125WG), Wheeling, IL, substantial damage. Probable cause: Partial failure of the left engine propeller governor during the takeoff ground roll. Factors included that directional control was not possible by the pilot which subsequently led to a collision… - [NTSB SEA07LA145](https://openairdocs.org/ntsb/SEA07LA145), Apr 1, 2007: Swearingen SA-226T (N46SA), McCall, ID, substantial damage. Probable cause: The nosewheel steering system's uncommanded turn during the landing roll, making it impossible for the pilot to maintain directional control. Factors include a snow bank running parallel to the side… - [NTSB NYC05LA089](https://openairdocs.org/ntsb/NYC05LA089), May 31, 2005: Swearingen SA-226T (N22DW), Teterboro, NJ, substantial damage. Probable cause: The pilot's improper decision to depart with a known deficiency, which resulted in a loss of control during landing at the destination airport. A factor was the fuel control units' improper flight… - [NTSB DEN04LA112](https://openairdocs.org/ntsb/DEN04LA112), Jul 21, 2004: Swearingen SA-226T (N84GA), Rifle, CO, substantial damage. Probable cause: the pilot's failure to maintain aircraft control during the aborted takeoff resulting in the airplane departing the runway and striking a runway light and two taxiway signs. Factors contributing to… - [NTSB CHI04LA096](https://openairdocs.org/ntsb/CHI04LA096), Mar 31, 2004: Swearingen SA226-T (N636SP), Omaha, NE, substantial damage. Probable cause: The pilot failed to maintain directional control during takeoff. Contributing factors to the accident were the runway light and the soft terrain. - [NTSB ATL04LA078](https://openairdocs.org/ntsb/ATL04LA078), Feb 28, 2004: Swearingen SA-226T (N70FC), Collegedale, TN, substantial damage. Probable cause: The pilot's inability to maintain directional control due to the inadequate grounding of the nose wheel steering clutches, as a result of inadequate maintenance inspection by other maintenance… - [NTSB ANC03LA062](https://openairdocs.org/ntsb/ANC03LA062), Jun 28, 2003: Swearingen SA-226T (N512FS), Goodnews, AK, substantial damage. Probable cause: The flight crew's inadequate evaluation of the weather conditions, which resulted in their inadequate compensation for the wind conditions, and subsequent undershoot. A contributing factor in the… - [NTSB CHI01LA302](https://openairdocs.org/ntsb/CHI01LA302), Aug 28, 2001: Swearingen SA226-T (N104BR), West Chicago, IL, substantial damage. Probable cause: the checklist not followed and the directional control not maintained by the pilot. A contributing factor was the left propeller’s start locks being engaged. - [NTSB FTW98FA073](https://openairdocs.org/ntsb/FTW98FA073), Dec 20, 1997: Swearingen SA226-T (N950TT), Byers, CO, destroyed, 1 fatal. Probable cause: The pilot inadvertently stalling the airplane and his subsequent spatial disorientation which prevented him from maintaining airplane control. Factors were excessive workload on the pilot and the… - [NTSB NYC96LA026](https://openairdocs.org/ntsb/NYC96LA026), Nov 7, 1995: Fairchild Merlin Iiia (N636SP), Butler, PA, substantial damage. Probable cause: failure of the pilot to perform a missed approach, when the airplane was not properly aligned with the landing runway; and his failure to properly flare the airplane, which resulted in a hard landing. - [NTSB LAX95FA338](https://openairdocs.org/ntsb/LAX95FA338), Sep 18, 1995: Swearingen SA-226T (N693PG), Chino, CA, destroyed. Probable cause: The pilot's improper IFR procedure by not initiating a missed approach at the outer marker, by attempting to intercept the glideslope from above after passing the outer marker, and by allowing the… - [NTSB FTW93FA165](https://openairdocs.org/ntsb/FTW93FA165), May 26, 1993: Fairchild SA-226T (N241DT), Santa Fe, NM, destroyed, 4 fatal. Probable cause: THE PILOT'S POORLY PLANNED CIRCLING APPROACH, AND HIS FAILURE TO MAINTAIN AN ADEQUATE ALTITUDE. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE DARK NIGHT AND A LACK OF VISUAL REFERENCE. - [NTSB CHI92LA038](https://openairdocs.org/ntsb/CHI92LA038), Dec 3, 1991: Swearingen SA-226T (N14TP), Iowa, IA, substantial damage. Probable cause: THE PILOT'S FAILURE TO EXTEND THE LANDING GEAR WHICH RESULTED IN THE PROPELLER BLADES CONTACTING THE RUNWAY DURING THE LANDING. A FACTOR RELATED TO THE ACCIDENT WAS THE PILOT'S FAILURE TO FOLLOW A… - [NTSB BFO89LA013](https://openairdocs.org/ntsb/BFO89LA013), Nov 30, 1988: Swearingen SA-226T (N263CM), Washington, DC, substantial damage. Probable cause: PILOTS FAILURE TO MAINTAIN CONTROL OF THE AIRPLANE DURING A TOUCH AND GO LANDING. - [NTSB CHI88IA074](https://openairdocs.org/ntsb/CHI88IA074), Mar 7, 1988: Swearingen SA226T (N600TA), Chicago, IL, incident, no damage. Probable cause: THE TRACON SUPERVISOR FAILED TO COMPLY WITH THE ESTABLISHED VISUAL MINIMA CRITERIA AND HIS INCORRECT ISSUANCE OF A VISUAL APPROACH TO AN ARRIVING AIRCRAFT. - [NTSB CHI88FA041](https://openairdocs.org/ntsb/CHI88FA041), Jan 10, 1988: Fairchild SA226T (N800AW), Pontiac, MI, destroyed, 3 fatal - [NTSB FTW85LAMS2](https://openairdocs.org/ntsb/FTW85LAMS2), Sep 17, 1985: Swearingen SA-226T (N3RB), Missing, destroyed, 1 fatal - [NTSB MKC83IA102](https://openairdocs.org/ntsb/MKC83IA102), May 6, 1983: Fairchild Swearingen SA226T (N779M), Lincoln, NE, incident, minor damage - [NTSB DCA82AA012](https://openairdocs.org/ntsb/DCA82AA012), Jan 19, 1982: Swearingen SA226-T(B) (N336SA), Rockport, TX, destroyed, 3 fatal - [NTSB FTW81FA105](https://openairdocs.org/ntsb/FTW81FA105), Jun 10, 1981: Swearingen SA226T (N555AM), Cameron, LA, destroyed, 2 fatal - [NTSB MIA79FLD22](https://openairdocs.org/ntsb/MIA79FLD22), Dec 4, 1978: Swearingen SAT226 (N97AB), Ft Pierce, FL, substantial damage - [NTSB MIA77RA036](https://openairdocs.org/ntsb/MIA77RA036), Mar 3, 1977: Swearingen SA226T (N5329M), Nassau, Burkina Faso, destroyed, 1 fatal - [NTSB FTW77FA033](https://openairdocs.org/ntsb/FTW77FA033), Feb 3, 1977: Swearingen SA266T (N34SM), Beckmam, TX, destroyed, 2 fatal - [NTSB LAX77FUG30](https://openairdocs.org/ntsb/LAX77FUG30), Feb 2, 1977: Swearingen SA226T (N555AM), Riverside, CA, substantial damage ## FAA accident and incident reports (40) 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 20211110019299I](https://openairdocs.org/incident/20211110019299I), Nov 10, 2021: Swearingen SA-226T (N749L), Fort Lauderdale, FL, Minor damage. Swearingen SA-226T ?merlin? Iii aircraft registration N749L, serial number T306 exited runway 9 at November at Fort Lauderdale executive airport (fxe). The… - [Incident 20131210023659I](https://openairdocs.org/incident/20131210023659I), Dec 10, 2013: Swearingen SA-226T (N749L), Bakersfield, CA, Minor damage. During the take-off roll, the pilot encountered an uncommanded deviation of directional control which resulted in the aircraft departing the left side of the… - [Incident 20080526837189I](https://openairdocs.org/incident/20080526837189I), May 26, 2008: Swrngn SA226T (N154L), Everett, WA, No damage. (-23) Pilot taxied aircraft to taxiway A-2 on pae from parking and was cleared 16R for takeoff. Aircraft got to 20-30 knots and started drifting right of… - [Accident 20070411006579A](https://openairdocs.org/incident/20070411006579A), Apr 11, 2007: Swrngn SA226T (N125WG), Chicago/Wheeli, IL, Substantial damage. (-23) Weather at the time of the accident was low overcast and snow with winds 090@11G26. The takeoff roll on runway 16 was normal until at a speed of… - [Accident 20070331007099A](https://openairdocs.org/incident/20070331007099A), Mar 31, 2007: Swrngn SA226T (N46SA), Mc Call, ID, Minor damage. (-23) Aircraft landed on runway 16 at mccall, Idaho. Pilot lost control and aircraft went off west side of runway and hit a snow bank. - [Incident 20050908020159I](https://openairdocs.org/incident/20050908020159I), Sep 8, 2005: Swrngn SA226T (N772SL), Oxford, MS, Minor damage. (-23) During landing props contacted runway. Pilot did go around and found selector valve had been moved from normal position and gear had not extended. Pilot… - [Accident 20050531018769A](https://openairdocs.org/incident/20050531018769A), May 31, 2005: Swrngn SA226T (N22DW), Teterboro, NJ, Destroyed. (-23) On 05/31/2005 at 11:30E the pilot lost control of the aircraft on short final runway 01 at teb and crashed. The ARFF team responded. Police officer… - [Accident 20040721015859A](https://openairdocs.org/incident/20040721015859A), Jul 21, 2004: Swrngn SA226T (N84GA), Rifle, CO, Substantial damage. (-23) Airplane was departing from Rifle, CO to lafayette, LA. Flight crew continuous alcohol/water injection (cawi) for take-off. Flight crew indicated that… - [Incident 20040409011699I](https://openairdocs.org/incident/20040409011699I), Apr 9, 2004: Swrngn SA226T (N226SR), Telluride, CO. (-23) On April 9, 2004, merlin N226SR was on an IFR flight plan enroute from santa ana, CA. To Telluride, CO. During the flight the right generator went off… - [Accident 20040331005709A](https://openairdocs.org/incident/20040331005709A), Mar 31, 2004: Swrngn SA226T (N636SP), Omaha, NE, Substantial damage. (-23) Approximately 1705 CST on March 31, 2004, N636SP taxied to the approach end of runway 30 at Millard Airport for a VFR flight. Pilot stated he lined up… - [Accident 20040228013719A](https://openairdocs.org/incident/20040228013719A), Feb 28, 2004: Swrngn SA226T (N70FC), Collegedale, TN, Substantial damage. (-23) On February 28, 2004 at 15:40 eastern standard time, a swearingen, SA-226T, N70FC registered to william d. fisher enterprises LLC., operating as a 14 CFR… - [Accident 20030628037249A](https://openairdocs.org/incident/20030628037249A), Jun 28, 2003: Swrngn SA226T (N512FS), Goodnews, AK, Substantial damage. (-23) During approach to landing on runway 5 at Goodnews, AK the aircraft struck the beach adjacent to the approach end of the runway. The main landing gear… - [Incident 20030221003469I](https://openairdocs.org/incident/20030221003469I), Feb 21, 2003: Swrngn SA226T (N5441M), Baton Rouge, LA, Minor damage. (-23) About half way down the ILS 13 approach at Baton Rouge the aircraft struck a 65 foot guy-line. The pilot stated that all of his instruments appeared to… - [Incident 20020316015919I](https://openairdocs.org/incident/20020316015919I), Mar 16, 2002: Swrngn SA226T (N78CS), Camarillo, CA, Minor damage. (-23) Hard landing during windy conditions. Suspected damage to engine mounts, wing and fuselage. - [Incident 20011213035279I](https://openairdocs.org/incident/20011213035279I), Dec 13, 2001: Swrngn SA226T (N226SR), Telluride, CO, Minor damage. (-23) Pilot lost control of aircraft during landing rollout on snow covered runway at Telluride airport. Aircraft departed the end of the runway causing damage… - [Accident 20010828024709A](https://openairdocs.org/incident/20010828024709A), Aug 28, 2001: Swrngn SA226T (N104BR), Chicago/West Ch, IL, No damage. (.19) On August 28, 2001, at 1720 central daylight time, a swearingen SA-226T, N104BR, piloted by an airline transport pilot, was substantially damaged during… - [Incident 20001214036549I](https://openairdocs.org/incident/20001214036549I), Dec 14, 2000: Swrngn SA226AT (N633ST), St Louis, MO, Minor damage. (-23) Rated pilot who was receiving recurrency training taxied off taxi way onto runway and stopped, powered up and released the brakes. The aircraft went… - [Incident 20001012031239I](https://openairdocs.org/incident/20001012031239I), Oct 12, 2000: Swrngn SA226T (N616PS), Hailey, ID. (-23)Pilot reported heavy concentration of moisture while holding at 10,000 both engines flamed out, pilot let airspeed to decrease to best glide angle and… - [Incident 19980913039099I](https://openairdocs.org/incident/19980913039099I), Sep 13, 1998: Swrngn SA226T (N9900), Las Vegas, NV, Minor damage. (-5)Aircraft slid off left side until coming to rest in ditch - after landing pilot stated the nose wheel turned rapidly to the left, the pilot could not… - [Accident 19971219039199A](https://openairdocs.org/incident/19971219039199A), Dec 19, 1997: Swrngn SA226T (N950TT), Byers, CO, Destroyed, 1 fatal. (Tty) pilot reported a stall and acft crashed. Pilot suffered fatal inj. Acft was destroyed. Byers, CO. (.4)the pilot departed front range airport (elevation… - [Incident 19971125044049I](https://openairdocs.org/incident/19971125044049I), Nov 25, 1997: Swrngn SA226T (N39MS), Jacksonville, AR. Narrative: on November 25, 1997, at 1922 local, swearingen, SA-226-T, N39MS, s/n T257, made an emergency landing at Little Rock Afb. The aircraft was piloted… - [Accident 19951107049209A](https://openairdocs.org/incident/19951107049209A), Nov 7, 1995: Swrngn SA226T (N636SP), Butler, PA, Substantial damage. (-16) [privacy data omitted] PIC failed to report this accident. This office received an anonymous phone call in reference to this accident ten days later… - [Accident 19950918029139A](https://openairdocs.org/incident/19950918029139A), Sep 18, 1995: Swrngn SA226T (N693PG), Chino, CA, Destroyed. Struck ground beyond airport during ILS approach. High sink rate. ATC failed give altimeter. Intercept inside faf. - [Incident 19950711023239I](https://openairdocs.org/incident/19950711023239I), Jul 11, 1995: Swrngn SA226T (N14TP), Iowa City, IA, Minor damage. Nose gear collapsed on takeoff roll. Bent nose and propellers. - [Incident 19940915036689I](https://openairdocs.org/incident/19940915036689I), Sep 15, 1994: Swrngn SA226T (N950TT), Midland, TX. Fire warning light. Secured engine. Diverted Midland. Loose clamp caused fire light to illiminate. - [Accident 19930525015099A](https://openairdocs.org/incident/19930525015099A), May 25, 1993: Swrngn SA226T (N241DT), Santa Fe, NM, Destroyed, 4 fatal. ILS approach 02 circle 15. Lined upon 20. Given option 20 or 15. Impacted hill 5MI west airport. No ground lights. - [Incident 19930505021769I](https://openairdocs.org/incident/19930505021769I), May 5, 1993: Swrngn SA226T (N103PA), Chicago, IL, Minor damage. Right gear started to collapse on touchdown. Made go around and landed at Lansing. Unable to substantiate malfunction - [Accident 19911203054879A](https://openairdocs.org/incident/19911203054879A), Dec 3, 1991: Swrngn SA226T (N14TP), Iowa City, IA, Substantial damage. On second approach the propellers impacted runway and a portion of one propeller blade penetrated the fuselage. - [Incident 19900325012439I](https://openairdocs.org/incident/19900325012439I), Mar 25, 1990: Swrngn SA226T (N263CM), Manassas, VA, Minor damage. Lost control on rollout. Aircraft veered right then slid into grass at end of runway. - [Incident 19881216068369I](https://openairdocs.org/incident/19881216068369I), Dec 16, 1988: Swrngn SA26T (N600TA), Buffalo, NY. Landed with left engine shut down and propeller feathered. Reason for engine failure not given. - [Incident 19881130056529I](https://openairdocs.org/incident/19881130056529I), Nov 30, 1988: Swrngn SA226T (N263CM), Washington, DC, Minor damage. Nose pitched up on rollout. Applied forward pressure and plane oscillated. Made go around and landed. Damaged prop. - [Accident 19880110069869A](https://openairdocs.org/incident/19880110069869A), Jan 10, 1988: Swrngn SA226T (N800AW), Pontiac, MI, Destroyed, 3 fatal. Appears CFI gave student engine out on takeoff by power lever to flite idle at or below VMC causing roll over. - [Accident 19850917045529A](https://openairdocs.org/incident/19850917045529A), Sep 17, 1985: Swrngn SA226T (N3RB), Gulf Of Mexico, LA, Destroyed. Reported unable to maintain altitude after one engine shut down. Reason unknown. Ditched in Gulf, presumed fatal. - [Incident 19830506040269I](https://openairdocs.org/incident/19830506040269I), May 6, 1983: Swrngn SA226T (N779M), Lincoln, NE, Minor damage. Unable to maintain directional control on rollout. Left runway. Brakes locked. Suspect parking brake valve. - [Accident 19820119070812A](https://openairdocs.org/incident/19820119070812A), Jan 19, 1982: Swrngn SA226TB (N336SA), Rockport, TX, Destroyed. Aircraft collided with N26660 while turning final for runway 14, one half mile north of runway threshold. - [Accident 19810610032439A](https://openairdocs.org/incident/19810610032439A), Jun 10, 1981: Swrngn SA226T (N555AM), Cameron, LA, Destroyed. Illegal drug flight . Made high speed verticle impact into a lake. Severe thunderstorms in area. - [Accident 19781204044809A](https://openairdocs.org/incident/19781204044809A), Dec 4, 1978: Swrngn SA226T (N97AB), Ft Pierce, FL, Substantial damage - [Incident 19780613045569I](https://openairdocs.org/incident/19780613045569I), Jun 13, 1978: Swrngn SA226TC (N22DW), Jamaica, NY. Pilot unable to get a gear safe indication except after manual gear extension. A wire to extension motor broken. - [Accident 19770303010899A](https://openairdocs.org/incident/19770303010899A), Mar 3, 1977: Swrngn SA226T (N5329M), Nassau Bahamas, Destroyed. Investigated under the jurisdiction of the goverment of the Bahamas - [Accident 19770203014509A](https://openairdocs.org/incident/19770203014509A), Feb 3, 1977: Swrngn SA226T (N34SM), Beckmam, TX, Destroyed. Clrd for ILS apch rwy 12R,nav rcvr tuned to freq for ILS apch rwy 3R. ## Service difficulty reports (34) As reported by operators and repair stations, by the model named in the report. - [SDR 2020F00435](https://openairdocs.org/sdr/2020F00435), Oct 9, 2020: CURRENT LIMITER. FAILED. AFTER TAKE OFF FROM ICT ON CLIMB OUT, PITCH TRIM CONTROL WAS INOPERABLE ON LEFT HAND SIDE (PILOTS SIDE) CONTROL YOKE. CREW USED PITCH TRIM FROM RIGHT SIDE (COPI - [SDR CA150910008](https://openairdocs.org/sdr/CA150910008), Sep 9, 2015: WINDSHIELD. CRACKED. (CAN) AT CRUISING ALTITUDE FL20 THE LT WINDSHIELD DEVELOPED SUDDEN SUBSTANTIAL CRACKING. PILOT SLOWED THE ACFT REDUCED PRESSURIZATION AND DESCENDED TO 10000 FT - [SDR CA150910007](https://openairdocs.org/sdr/CA150910007), Sep 7, 2015: WIRE. BROKEN. (CAN) ALL 3 GEAR LIGHTS FAILED TO ILLUMINATE ON GEAR DOWN SELECTION AND GEAR LIGHTS FAILED TO TEST WHEN TESTED IN FLIGHT. AFTER 2 GEAR CYCLES AND WHEN INDICATOR - [SDR 2015FA0000027](https://openairdocs.org/sdr/2015FA0000027), Jan 9, 2015: FITTING. CORRODED. CORROSION FOUND AT FITTINGS OTBD SIDES OF EACH INBD OF SPAR ATTACH BOLT HEADS. LEFT FITTING IS WORSE THAN RIGHT. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND - [SDR CA081020008](https://openairdocs.org/sdr/CA081020008), Oct 9, 2008: WINDSHIELD. CRACKED. (CAN) DURING CRUISE FLIGHT THE LT COCKPIT WINDSHIELD GLASS CRACKED WITH AN EXPLOSIVE BANG. THE CREW IMMEDIATELY DESCENDED AND REDUCED CABIN PRESSURE TO AVOID TH - [SDR CA080403005](https://openairdocs.org/sdr/CA080403005), Mar 31, 2008: WINDSHIELD. CRACKED. IN LEVEL CRUISE AT FLIGHT LEVEL 220 APPROXIMATELY 25 MINUTES AFTER DEPARTURE, THE LEFT HEATED WINDSHIELD SUDDENLY SHATTERED. ATC WAS ADVISED AND DESCENT REQUEST - [SDR 2007FA0000640](https://openairdocs.org/sdr/2007FA0000640), Jul 2, 2007: SOLENOID VALVE. FAILED. THE NOSE WHEEL STEERING WAS TESTED PRIOR TO FLIGHT, AD TESTED SATISFACTORY. AT AROUND 60 TO 70 KNOTS DURING THE TAKEOFF ROLL, THE AC STEERING FAILED IN A MANOR - [SDR O05R200400107](https://openairdocs.org/sdr/O05R200400107), Apr 5, 2004: BLADE. OUT OF TOLERANCE. 1 BLADE REJECTED FOR DIMENSIONS. - [SDR O05R200400106](https://openairdocs.org/sdr/O05R200400106), Apr 5, 2004: BLADE. OUT OF TOLERANCE. 1 BLADE REJECTED FOR DIMENSIONS. - [SDR O05R200400105](https://openairdocs.org/sdr/O05R200400105), Apr 5, 2004: BLADE. OUT OF TOLERANCE. 1 BLADE REJECTED FOR DIMENSIONS. - [SDR VH22003F00000](https://openairdocs.org/sdr/VH22003F00000), Mar 31, 2003: CONTROL BOX. FAILED. ON MARCH 15, 2003 FAS INSTALLED AUTO CONTINUOUS IGNITION SYSTEM IAW AD AND SB WHICH INSTALLED A NEW IGNITION CONTROL BOX LATEST VARIANT OF THIS UNIT. SYSTEM OPS - [SDR 2003FA0000049](https://openairdocs.org/sdr/2003FA0000049), Jan 8, 2003: VALVE. DEFECTIVE. AIRCRAFT ROLLED LT AFTER FLAPS WERE DEPLOYED FOR 30 SECONDS, INTERMITTENLY. FOUND LT LOCK OUT VALVE DEFECTIVE. VALVE WAS GROUND PRESSURE TESTED AND IT FAILED TH - [SDR AUS20021483](https://openairdocs.org/sdr/AUS20021483), Nov 18, 2002: STRUCTURE. DAMAGED. (AUS) PILOT COMPLAINED THAT THE NLG GREEN LIGHT WAS TAKING A LONG TIME TO ILLUMINATE. INVESTIGATION THEN FOUND EVIDENCE OF A HEAVY LANDING. INVESTIGATION FOUND - [SDR 2002FA0000854](https://openairdocs.org/sdr/2002FA0000854), Jul 8, 2002: VALVE. FAILED. OVERHAULED VALVE FAILED SHOP GROUND TEST. VALVE (SN 493A), FAILED ON FIRST LANDING, CAUSING AN UNCONTROLABLE SHIMMY IN STEERING OF AIRCRAFT, VIOLANT SHAKING. - [SDR GXPA00011](https://openairdocs.org/sdr/GXPA00011), May 24, 2000: ENGINE. MALFUNCTIONED. AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. RIGHT EGT FLUCTUATES EXCESSIVELY. AIRCRAFT LANDED BACK IN TOLEDO AND GROUNDED FOR CORRECTIVE ACTION. (X) - [SDR 20000512SH018](https://openairdocs.org/sdr/20000512SH018), Feb 2, 2000: YOKE. CRACKED. DURING ACCOMPLISHMENT OF AD 96-19-05, ULTRASONIC INSPECTION OF MAIN LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE INBOARD SIDE OF THE RIG - [SDR 20000512SH017](https://openairdocs.org/sdr/20000512SH017), Feb 2, 2000: YOKE. CRACKED. DURING ACCOMPLISHMENT OF AD 96-19-05, ULTRASONIC INSPECTION OF MAIN LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE INBOARD SIDE OF THE LT - [SDR 20000512SH016](https://openairdocs.org/sdr/20000512SH016), Feb 2, 2000: YOKE. CRACKED. DURING ACCOMPLISHMENT OF AD 96-19-05, ULTRASONIC INSPECTION OF MAIN LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE INBOARD SIDE OF THE RT - [SDR 20000512SH009](https://openairdocs.org/sdr/20000512SH009), Feb 2, 2000: YOKE. CRACKED. DURING ACCOMPLISHMENT OF AD 96-19-05 ULTRASONIC INSPECTION OF NOSE LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE INBD SIDE OF THE LT MLG - [SDR 20000512SH008](https://openairdocs.org/sdr/20000512SH008), Feb 2, 2000: YOKE. CRACKED. DURING ACCOMPLISHMENT OF AD 96-19-05 ULTRASONIC INSPECTION OF NOSE LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE RT SIDE OF THE NLG YOKE - [SDR 99ZZZX3079](https://openairdocs.org/sdr/99ZZZX3079), Aug 3, 1999: WIRE. CHAFED. WIRE ON OIL COOLER FIRE DETECTOR CHAFED TO ASPIRATOR ASSEMBLY CAUSING FALSE FIRE INDICATION. - [SDR CA990318040](https://openairdocs.org/sdr/CA990318040), Mar 5, 1999: BEARING. CRACKED. (CAN) LEFT FLAP ACTUATOR CENTER WALKING BEAM BEARING OUTER RACE CRACKED. - [SDR CA980610013](https://openairdocs.org/sdr/CA980610013), Jun 2, 1998: LINE. CHAFED. (CAN) DURING INSPECTION OF BOTTOM IGNITOR, IT WAS NOTED THAT THE COOLING AIR HOSE TO IGNITOR HOUSING WAS RUBBING AGAINST REAR TURBINE BEARING OIL LINE. OIL LINE - [SDR 98ZZZX2123](https://openairdocs.org/sdr/98ZZZX2123), May 14, 1998: HUB. FAILED. DURING LANDING, RIGHT INBOARD MAIN DEPARTED AIRCRAFT, OUTBOARD TIRE THEN FAILED. INVESTIGATION REVEALED ONE EACH STUD ON HUB MISSING ONE EACH. STUD BROKEN PREVI - [SDR 97ZZZX5084](https://openairdocs.org/sdr/97ZZZX5084), Nov 24, 1997: BATTERY. DEFECTIVE. BATTERY SUPPORT SLEEVE ON THE OUTSIDE OF BATTERY SLIDES DOWN 2 INCHES IN-FLIGHT OR DURING LANDING ABOUT 2 INCHES. CONCORDE FAX SAID TO PUSH SLEEVE UP AND PUT TA - [SDR 97ZZZX4458](https://openairdocs.org/sdr/97ZZZX4458), Sep 30, 1997: FUEL CONTROL. FAILED. FUEL CONTROL, INTERNAL FAILURE. FAILED TO RESPOND TO POWER LEVER MOVEMENT. - [SDR 97ZZZX3927](https://openairdocs.org/sdr/97ZZZX3927), Aug 14, 1997: MAIN SHAFT NUT. FAILED. TURBINE (MAINSHAFT) RETENTION NUT FAILED (CRACKED IN HALF) DURING OPERATION OF ENGINE ON THE GROUND. IT WAS OBSERVED THE PROPELLER WOULD NOT ROTATE FREELY AND T - [SDR 97ZZZX2632](https://openairdocs.org/sdr/97ZZZX2632), Apr 7, 1997: ROTOR. CRACKED. SECOND STAGE TURBINE ROTOR EXHIBITS RIVET HOLE CRACKS 0.020 INCH TO 0.050 INCH DEEP. DEFECT DISCOVERED 200 HOURS AFTER HOT SECTION INSPECTION AT UNSCHEDULED ENG - [SDR 97ZZZX2634](https://openairdocs.org/sdr/97ZZZX2634), Apr 4, 1997: BRAKE LINE. BROKEN. WHILE REMOVING BRAKE ASSY, NORMAL FLEXING OF OTBD BRAKE LINE CAUSED LINE TO BREAK OFF AT METAL FERRULE. FURTHER INVESTIGATION REVEALED LINE WAS SO BRITTLE, IT L - [SDR 97ZZZX842](https://openairdocs.org/sdr/97ZZZX842), Jan 31, 1997: SWITCH. OUT OF ADJUST. PILOT REPORTED LOSS OF NOSE WHEEL STEERING ON TAKEOFF ROLL. DIRECTIONAL CONTROL WAS LOST AND AIRCRAFT RAN OFF OF THE RUNWAY ONTO THE GRASS. AIRCRAFT WAS NOT DAM - [SDR CA961230009](https://openairdocs.org/sdr/CA961230009), Dec 2, 1996: HINGE. CRACKED. (CAN) CABIN DOOR FOUND WITH EXCESSIVE LATERAL MOVEMENT WHEN MOVED OPEN OR CLOSED. IT WAS ALSO NOTED THAT DOOR GUIDES WOULD CONTACT THE FUSELAGE FRAME WHEN CLOSI - [SDR 96ZZZX2114](https://openairdocs.org/sdr/96ZZZX2114), Apr 10, 1996: SEAL. MISINSTALLED. ATTEMPT TO REMOVE THE EMERGENCY EXIT FOR ACCESS FOR OTHER MAINTENANCE WAS UNSUCCESSFUL BY ONE PERSON. EXIT HAD TO BE PRIED FROM ACFT USING A SCREWDRIVER WHILE 2 - [SDR CA951030005](https://openairdocs.org/sdr/CA951030005), Oct 20, 1995: CHIP DETECTOR. FAILED. (CAN)SMOKE IN AIRCRAFT CABIN. REDUCTION OF OIL PRESSURE AND TORQUE RESULTING IN SHUT DOWN OF ENGINE. FOUND CHIP DETECTOR BROKEN AND THREADS STILL IN ENGINE NOSE - [SDR 95ZZZX3584](https://openairdocs.org/sdr/95ZZZX3584), Jun 22, 1995: FUSELAGE. SKIN DAMAGE. AFTER AIRCRAFT WAS STRIPPED IN PREPARATION FOR PAINT, A LARGE AMOUNT OF PLASTIC FILLER WAS DISCOVERED ON THE FUSELAGE IN LINE WITH THE PROPELLER ROTATIONAL PLAN ## STCs that may be installed (OpenAirDocs) (114, 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 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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International 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 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 SA8808SW](https://openairdocs.org/stc/SA8808SW): Installation of a TCAS 791 (TCAS I) system. Acron Aviation Inc - [STC SA04627CH](https://openairdocs.org/stc/SA04627CH): Installation of Luma Technologies LT-4048 Series LED Display Panel. Luma Technologies 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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin 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 SA4872SW](https://openairdocs.org/stc/SA4872SW): Installation of two Garrett AiResearch Model TPE 331-1OUA-501G or TPE 331-1OUA-511G engines. Worldwide Aviation LLC - [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 SA09170AC](https://openairdocs.org/stc/SA09170AC): Installation of Concorde RG390ES sealed lead-acid batteries. Ontic Engineering and Manufacturing Inc - [STC SA09463AC](https://openairdocs.org/stc/SA09463AC): Installation of Concorde FASRG91STC sealed lead-acid batteries. Ontic Engineering and Manufacturing Inc - [STC SA4618SW](https://openairdocs.org/stc/SA4618SW): Installation of the Zee Systems R-12/R-134a Air Conditioning Systems. Ontic Engineering and Manufacturing Inc - [STC SA4725SW](https://openairdocs.org/stc/SA4725SW): Installation of Conrac stall warning and stall avoidance system. Ontic Engineering and Manufacturing Inc - [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 ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc - [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA04143NY](https://openairdocs.org/stc/SA04143NY): Installation of MT-Propeller Entwicklung GmbH propellers and spinners. MT- Propeller Entwicklung GmbH - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA1709GL](https://openairdocs.org/stc/SA1709GL): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS - [STC ST00276WI](https://openairdocs.org/stc/ST00276WI): Installation of Kedeg Company 21BC11e Coaleser Assemly. Purolator Facet, Inc - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA1541GL](https://openairdocs.org/stc/SA1541GL): Install Egan Aviation air ambulance stretcher P/N 125 using installation kit P/N 801. Paul/ Lanna Egan LLC - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA961NW](https://openairdocs.org/stc/SA961NW): Installation of forward facing white lights (100 watt), clear plastic wing tip covers, and associated systems. Knots 2U Ltd - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA04182AT](https://openairdocs.org/stc/SA04182AT): Installation of Pilot and Copilot Main Windshield. PPG Aerospace - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation - [STC SA02717NY PAGE 2](https://openairdocs.org/stc/SA02717NY%20PAGE%202): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA03893AT](https://openairdocs.org/stc/SA03893AT): Installation of MT-Propeller Model MTV-27-1-E-C-F-R(G)/CFRL250-103. MT-Propeller USA Inc - [STC SA03893AT`](https://openairdocs.org/stc/SA03893AT%60): Installation of MT-Propeller Model MTV-27-1-E-C-F-R(G)/CFRL250-103. MT-Propeller USA Inc - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc All 114: https://openairdocs.org/model/swearingen-sa-226t/stcs.md ## PMA parts (OpenAirDocs) (543, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [RFS60-438](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189651152120260722154552.0001): Spacer, Axle. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 60-438 · Jul 1, 2026 - [LM29749-20629](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119055499320260705233748.0001): Cone. Timken Corporation · PMA PQ4105CE · Replaces 214-01400, LM29749 · Jun 4, 2026 - [BAS-FAC-X200G](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103590946320251215171647.0001): Pressure Transducer. Benz Airborne Systems · PMA PQ0611SW · Replaces APTE-6KBS-1000-200G, 27-19153-1… · Dec 9, 2025 - [26-24076-005ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118027719720250604171547.0001): Faceplate. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 26-24076-005 · Apr 1, 2025 - [27-70102-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178682222220250604160107.0001): Plunger Assy, Lock. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-70102-001 · Mar 21, 2025 - [3651-00ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193188186120250115124157.0001): Valve Assy, Fuel Drain. ANB Aviation of CT, LLC · PMA PQ10055NE · Replaces 3651-0027-19484-001 · Dec 20, 2024 - [DS001-015-2ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152932335620250423205610.0001): O-Ring. ANB Aviation of CT, LLC · PMA PQ10055NE · Replaces DS001-015-227-31000-799 · Dec 20, 2024 - [DS001-015-2ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110053804520250115124158.0001): O-Ring. ANB Aviation of CT, LLC · PMA PQ10055NE · Replaces DS001-015-227-31000-799 · Dec 20, 2024 - [3651-00ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109404527420250423205609.0001): Valve Assy, Fuel Drain. ANB Aviation of CT, LLC · PMA PQ10055NE · Replaces 3651-0027-19484-001 · Dec 20, 2024 - [M23065-1470](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132956462920241113171047.0001): Fan Cover. Miraj Corporation · PMA PQ0870NE · Replaces 23065-1470 · Nov 8, 2024 - [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143160510320241022163145.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024 - [MDL-4048-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172939396220241206121238.0001): LT-4048 Series Integrated LED Display Panel (ILDP). Luma Technologies LLC · PMA PQ4012NM · Modification part · Sep 9, 2024 - [HEM27-90264-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100636187320250303205511.0001): Fork. Hemico Inc. · PMA PQ2145NE · Replaces 27-90264-005 · Jul 24, 2024 - [HEM27-90282-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100131157720250303205511.0001): Shaft. Hemico Inc. · PMA PQ2145NE · Replaces 27-90282-005 · Jul 24, 2024 - [SS1012-7ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148948392420240501205845.0001): Switch, Pressure. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces SS1012-7 · Apr 29, 2024 - [AC-5451021-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198170372420240514142827.0001): Small Bushing. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 5451021-1 27-51521-001 · Mar 25, 2024 - [27-84183-003ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194925461320240514142833.0001): Gasket. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-84183-003 27-84183-001 · Mar 25, 2024 - [AC27-52531-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184288942320240514142830.0001): Shaft. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-52531-001 · Mar 25, 2024 - [27-24115-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182401737520240514142833.0001): Slip Ring. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-24115-001 · Mar 25, 2024 - [27-52529-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172876082320240514142834.0001): Shaft. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-52529-001 27-52529-1 · Mar 25, 2024 - [27-55001-273ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160012463820240514142831.0001): Swivel Assembly. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-55001-273 · Mar 25, 2024 - [AC27-52529-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155533640320240514142830.0001): Shaft. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-52529-005 · Mar 25, 2024 - [27-19301-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149498140220240514142831.0001): Aspirator Seal. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-19301-001 · Mar 25, 2024 - [27-31191-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143832340220240514142832.0001): Pin Assy. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-31191-001 · Mar 25, 2024 - [27-82179-001ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142288982320240514142831.0001): Battery Switch Guard. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-82179-001 · Mar 25, 2024 - [AC-5451031-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137851671620240514142829.0001): Shaft. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 5451031-1 27-52531-001 · Mar 25, 2024 - [AC27-52535-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130837369820240514142831.0001): Large Bushing. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-52535-001 · Mar 25, 2024 - [AC-5451029-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120224438120240514142828.0001): Shaft. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 5451029-1 27-52529-005 · Mar 25, 2024 - [AC-5451035-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119224996320240514142829.0001): Large Bushing. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 5451035-1 27-52535-001 · Mar 25, 2024 - [26-63308-003ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110061985820240514142832.0001): Boost Pump Gasket. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 26-63308-003 26-63308-001 · Mar 25, 2024 - [AC-5451022-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107300966920240514142828.0001): Pin. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 5451022-1 27-51522-001 · Mar 25, 2024 - [27-31191-002ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103124773220240514142832.0001): Pin. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-31191-002 · Mar 25, 2024 - [27-55001-033ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101731216920240514142832.0001): Swivel. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-55001-033 · Mar 25, 2024 - [M06-200001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136215913020240223153730.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-200001 · Feb 15, 2024 - [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154818143220231108124805.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023 - [L8537831](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164866341620251223203907.0001): Oil Cooler Assy. Honeywell International Inc. · PMA PQ1222NM · Replaces 8537831 · Feb 23, 2023 - [L8537927](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109923243220251223203907.0001): Thermostatic Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 8537927 · Feb 23, 2023 - [L8537831](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157615061720241017144607.0001): Oil Cooler Assy. Honeywell International US LLC · PMA PQ1354NM · Replaces 8537831 · Feb 21, 2023 - [L8537927](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143442991420241017144607.0001): Thermostatic Control Valve. Honeywell International US LLC · PMA PQ1354NM · Replaces 8537927 · Feb 21, 2023 - [392908-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199592431420231227185350.0001): Regulator Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 392908-1-1 · Jan 7, 2023 - [320250-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191092133020231227185349.0001): Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 320250-6 · Jan 7, 2023 - [3213812-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178425193720231227185350.0001): Regulator Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3213812-6 · Jan 7, 2023 - [3213812-3-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146692666620231227185351.0001): Regulator Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3213812-3-1 · Jan 7, 2023 - [3167988-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127902280220231227185349.0001): Tee Blue. Honeywell International Inc. · PMA PQ1222NM · Replaces 3167988-2 · Jan 7, 2023 - [320250-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122630144820231227185349.0001): Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 320250-7 · Jan 7, 2023 - [129542-5-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102217310720231227185349.0001): Temperature Sensor. Honeywell International Inc. · PMA PQ1222NM · Replaces 129542-5-3 · Jan 7, 2023 - [979458-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101435071820231227185350.0001): Modulating Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 979458-5 · Jan 7, 2023 - [8000950](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136238737420221130202607.0001): Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces M7 Aerospace LLC27-62056-001… · Oct 21, 2022 - [27-71004-067ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190760586220230216155741.0001): Link Assembly. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-71004-035, 27-71004-067 · Sep 20, 2022 - [27-71004-059ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179825315920230216155738.0001): Link Assembly. ANB Aviation Parts LLC · PMA PQ1730CE · Replaces 27-71004-00327-71004-04327-71004-05927… · Sep 20, 2022 All of them: https://openairdocs.org/model/swearingen-sa-226t/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Swearingen SA226-T(B)](https://openairdocs.org/model/swearingen-sa226-t-b): 16 registered aircraft, registry code 8780406 - [Fairchild SA226-T(B)](https://openairdocs.org/model/fairchild-sa226-t-b): 3 registered aircraft, registry code 3377516 - [Fairchild SA226-T](https://openairdocs.org/model/fairchild-sa226-t): 1 registered aircraft, registry code 3377514 --- 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.