# Saab-Fairchild 340A - Type: Aircraft model (FAA registry) - Registry code: 7850100 - Manufacturer (registry): SAAB-FAIRCHILD - Model: 340A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 37 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (OpenAirDocs) - Holder: Saab AB - Registered aircraft: 8 - Page: https://openairdocs.org/model/saab-fairchild-340a 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 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2025-02-15](https://openairdocs.org/ad/2025-02-15): Time Limits/Maintenance Checks · Saab 340A (SAAB SF340A) and SAAB 340B. Effective Mar 19, 2025 - [AD 2023-17-02](https://openairdocs.org/ad/2023-17-02): Flight controls · Saab AB Support and Services 340A (SAAB SF340A) and SAAB 340B. Effective Oct 19, 2023 - [AD 2023-09-10](https://openairdocs.org/ad/2023-09-10): Electrical Power · Saab AB Support and Services 340A (SAAB SF340A) and SAAB 340B. Effective May 31, 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 2022-14-09](https://openairdocs.org/ad/2022-14-09): Landing gear · Saab AB Support and Services SAAB 340B and 340A (SAAB SF340A). Effective Aug 18, 2022 - [AD 2020-25-02](https://openairdocs.org/ad/2020-25-02): Landing Gear · Saab AB, Saab Aeronautics SAAB 2000, 340A (SAAB SF340A) and SAAB 340B. Effective Jan 21, 2021 - [AD 2018-18-17](https://openairdocs.org/ad/2018-18-17): Ice and Rain Protection · Saab AB, Saab Aeronautics 340A (SAAB SF340A) and SAAB 340B. Effective Oct 18, 2018 - [AD 2017-17-14](https://openairdocs.org/ad/2017-17-14): Lights · Saab AB, Saab Aeronautics 340A (SAAB SF340A). Effective Oct 2, 2017 - [AD 2016-22-15](https://openairdocs.org/ad/2016-22-15): Flight controls. · Saab AB, Saab Aeronautics 340A (SAAB SF340A) and SAAB 340B. Effective Dec 9, 2016 - [AD 2014-01-03](https://openairdocs.org/ad/2014-01-03): Air Conditioning · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B with STC SA7971SW. Effective Apr 3, 2014 - [AD 2012-13-01](https://openairdocs.org/ad/2012-13-01): Flight Controls · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Aug 2, 2012 - [AD 2011-27-05](https://openairdocs.org/ad/2011-27-05): Landing gear · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Feb 7, 2012 - [AD 2011-09-02](https://openairdocs.org/ad/2011-09-02): Fuselage · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B with STC SA984GL-D or 2 others. Effective May 25, 2011 - [AD 2009-23-07](https://openairdocs.org/ad/2009-23-07): Hydraulic power · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Dec 14, 2009 - [AD 2008-09-06 R1](https://openairdocs.org/ad/2008-09-06-R1): Fuel · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Nov 23, 2009 - [AD 2009-17-02](https://openairdocs.org/ad/2009-17-02): Fuel · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Sep 22, 2009 - [AD 2009-10-13](https://openairdocs.org/ad/2009-10-13): Powerplant · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Jun 24, 2009 - [AD 2008-26-08](https://openairdocs.org/ad/2008-26-08): Landing gear emergency extension valves · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Jan 28, 2009 - [AD 2008-08-07](https://openairdocs.org/ad/2008-08-07): Axle adaptor · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective May 19, 2008 - [AD 2008-07-03](https://openairdocs.org/ad/2008-07-03): Fuel tank system · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Apr 30, 2008 - [AD 2008-04-07](https://openairdocs.org/ad/2008-04-07): Fuel tank system · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 28, 2008 - [AD 2008-06-11](https://openairdocs.org/ad/2008-06-11): Icing conditions · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 27, 2008 - [AD 2008-03-18](https://openairdocs.org/ad/2008-03-18): Fuel tank system · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 17, 2008 - [AD 2008-03-17](https://openairdocs.org/ad/2008-03-17): Fuel tank systems · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 17, 2008 - [AD 2007-02-16](https://openairdocs.org/ad/2007-02-16): Direct current (DC) starter generator · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 1, 2007 - [AD 2006-18-12](https://openairdocs.org/ad/2006-18-12): Hot detection system of the tail pipe harness of the engine nacelles · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Oct 13, 2006 - [AD 2006-10-05](https://openairdocs.org/ad/2006-10-05): Shock strut of the main landing gear (MLG) · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jun 16, 2006 - [AD 2005-23-11](https://openairdocs.org/ad/2005-23-11): Compressor impeller assemblies · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 5 more. Effective Dec 14, 2005 - [AD 2005-10-09](https://openairdocs.org/ad/2005-10-09): Windshield wiper assembly · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jun 21, 2005 - [AD 2005-08-11](https://openairdocs.org/ad/2005-08-11): Hydraulic hoses · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective May 24, 2005 - [AD 2005-04-04](https://openairdocs.org/ad/2005-04-04): Engine Vibration Isolators (Mounts) · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Mar 23, 2005 - [AD 2004-24-06](https://openairdocs.org/ad/2004-24-06): Actuator bracket attachment bolt (RABAB) · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jan 4, 2005 - [AD 2004-22-14](https://openairdocs.org/ad/2004-22-14): Elevator and aileron trim-tab fittings · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Dec 10, 2004 - [AD 2004-15-10](https://openairdocs.org/ad/2004-15-10): Wire Harness of Left-Hand Electronic Flight Instrumentation System (LH EFIS) · Saab AB, Saab Aerosystems 340A (SAAB SF340A). Effective Aug 31, 2004 - [AD 2004-11-02](https://openairdocs.org/ad/2004-11-02): Outer flange of the nacelle frame · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jul 7, 2004 - [AD 2004-09-35](https://openairdocs.org/ad/2004-09-35): Two direct current (DC) over-voltage/feeder-fault test switches · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jun 15, 2004 - [AD 2004-09-08](https://openairdocs.org/ad/2004-09-08): Signal Conditioner Wiring Harness Behind Refueling Panel · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jun 4, 2004 - [AD 2004-07-23](https://openairdocs.org/ad/2004-07-23): Assistor springs and bearings · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective May 11, 2004 - [AD 2003-06-05](https://openairdocs.org/ad/2003-06-05): Air recirculaton fans · Saab AB, Saab Aerosystems 340A (SAAB SF340A). Effective Apr 30, 2003 - [AD 2002-26-19](https://openairdocs.org/ad/2002-26-19): Main Pitot Static Tube · Saab AB, Saab Aerosystems SAAB 2000, SAAB 340B and 340A (SAAB SF340A). Effective Feb 10, 2003 - [AD 2001-23-12 R1](https://openairdocs.org/ad/2001-23-12-R1): Aluminum Skin of Airplane · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Dec 31, 2001 - [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001 - [AD 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001 - [AD 2001-06-14](https://openairdocs.org/ad/2001-06-14): Nose Wheel Steering · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective May 7, 2001 - [AD 2000-23-19](https://openairdocs.org/ad/2000-23-19): Bushings in the Flap Fittings · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jan 2, 2001 - [AD 2000-23-15](https://openairdocs.org/ad/2000-23-15): Illuminated Panel Connector · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Dec 27, 2000 - [AD 2000-14-03](https://openairdocs.org/ad/2000-14-03): Smoke Detectors · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Aug 17, 2000 - [AD 2000-12-14](https://openairdocs.org/ad/2000-12-14): Cabin Compartment Ceiling · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jul 24, 2000 - [AD 2000-12-07](https://openairdocs.org/ad/2000-12-07): Main Landing Gear · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jul 20, 2000 Historical (superseded or no longer in force): - [AD 2017-21-05](https://openairdocs.org/ad/2017-21-05) (historical): Time Limits/ Maintenance Checks · Saab AB, Saab Aeronautics 340A (SAAB SF340A) and SAAB 340B. Effective Nov 27, 2017 - [AD 2016-13-06](https://openairdocs.org/ad/2016-13-06) (historical): Ice and Rain Protection · Saab AB, Saab Aeronautics 340A (SAAB SF340A) and SAAB 340B. Effective Aug 1, 2016 - [AD 2012-24-06](https://openairdocs.org/ad/2012-24-06) (historical): Flight Controls · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Jan 14, 2013 - [AD 2008-09-06](https://openairdocs.org/ad/2008-09-06) (historical): Fuel tank system · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B. Effective Jun 2, 2008 - [AD 2004-12-03](https://openairdocs.org/ad/2004-12-03) (historical): Main Landing Gear's (MLG) Separation Bolt Harness · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A). Effective Jul 29, 2004 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 All 122: https://openairdocs.org/model/saab-fairchild-340a/ads.md ## Information bulletins (advisory) (1) - [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008 ## Registered aircraft (8) - [N27XJ](https://openairdocs.org/aircraft/N27XJ): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1985, S/N 340A-027 - [N342JC](https://openairdocs.org/aircraft/N342JC): [Aviation Investments Inc](https://openairdocs.org/faa-owner/AVIATION%20INVESTMENTS%20INC), [Redondo Beach, CA](https://openairdocs.org/faa-place/CA/Redondo%20Beach), S/N 340A-030 - [N631BC](https://openairdocs.org/aircraft/N631BC): [Ibc Airways Inc](https://openairdocs.org/faa-owner/IBC%20AIRWAYS%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), S/N 340A-061 - [N651BC](https://openairdocs.org/aircraft/N651BC): [Aviation Inventory Resources Inc](https://openairdocs.org/faa-owner/AVIATION%20INVENTORY%20RESOURCES%20INC), [Alvarado, TX](https://openairdocs.org/faa-place/TX/Alvarado), S/N 340A-076 - [N691BC](https://openairdocs.org/aircraft/N691BC): [Aviation Inventory Resources Inc](https://openairdocs.org/faa-owner/AVIATION%20INVENTORY%20RESOURCES%20INC), [Alvarado, TX](https://openairdocs.org/faa-place/TX/Alvarado), S/N 340A-041 - [N727DL](https://openairdocs.org/aircraft/N727DL): [Aircraft Guaranty Corp Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20GUARANTY%20CORP%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1985, S/N 340A036 - [N906RA](https://openairdocs.org/aircraft/N906RA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), S/N 340A-109 - [N907RA](https://openairdocs.org/aircraft/N907RA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1987, S/N 340A-111 ## NTSB investigations (5) 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 CHI02IA275](https://openairdocs.org/ntsb/CHI02IA275), Sep 4, 2002: Saab-Scania 340A (N110XJ), Detroit, MI, incident, no damage. Probable cause: A malfunctioning yaw damper. - [NTSB NYC02LA146](https://openairdocs.org/ntsb/NYC02LA146), Jul 21, 2002: Saab-Scania 340A (N110XJ), Charleston, WV, substantial damage. Probable cause: The vehicle driver's failure to maintain clearance of the airplane. - [NTSB MIA99LA026](https://openairdocs.org/ntsb/MIA99LA026), Nov 4, 1998: Saab-Scania 340A (N325PX), Memphis, TN, minor damage, 1 fatal. Probable cause: The ground crewmembers inadvertent walking into the path of a rotating propeller resulting in her being struck and fatally injured. - [NTSB MKC89IA012](https://openairdocs.org/ntsb/MKC89IA012), Oct 24, 1988: Saab-Scania 340A (N347AM), Springfield, MO, incident, minor damage - [NTSB MKC86IA018](https://openairdocs.org/ntsb/MKC86IA018), Oct 29, 1985: SAAB-Fairchild SF340A (N342AM), Lincoln, NE, incident, no damage ## FAA accident and incident reports (69, newest 50) 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 20210121002349I](https://openairdocs.org/incident/20210121002349I), Jan 21, 2021: Saab-Fairchild 340A (N907RA), Anchorage, AK, Minor damage. The crew was cleared for a visual approach to runway 7R. The aircraft was descending into Anchorage international airport on right base. The SIC noticed sparks… - [Incident 20040525008769I](https://openairdocs.org/incident/20040525008769I), May 25, 2004: Saab SF340A (N95CQ), Pittsburgh, PA. (-23) At 1750E, shuttle america flight 4556, a, SF34, aborted takeoff on runway 28R for unknown reasons. No assistance was required and the aircraft returned… - [Incident 20031216033949I](https://openairdocs.org/incident/20031216033949I), Dec 16, 2003: Saab SF340A (N340SZ), Akron, OH. (-23) Shuttlecraft #4555, an SF340A N340SZ, enroute from fort wayne, IN. To pittsburgh, PA. Reported a fire indication in the aft cargo hold 15 miles west of… - [Incident 20031210031449I](https://openairdocs.org/incident/20031210031449I), Dec 10, 2003: Saab SF340A (N43SZ), Pittsburgh, PA. (-23) Uhla flight #4571, N43SZ, while at cruise reported RH DC generator failed briefly then came back on. After diverting back to PIC, RH DC generator failed… - [Incident 20030815024119I](https://openairdocs.org/incident/20030815024119I), Aug 15, 2003: Saab SF340A (N79XJ), Minneapolis, MN. (-23) During climb out and at level flight, flaps began uncommanded movement causing the aircraft to experience pitch changes. Flap position potentiometer had… - [Incident 20030214005739I](https://openairdocs.org/incident/20030214005739I), Feb 14, 2003: Saab SF340A (N110XJ), Bloomington-Nor, IL. (-23) At approximately 2025 CST on February 14, 2003, while on a revenue flight from detroit, mi (dtw) to Bloomington, IL (bmi) and on the final approach to… - [Incident 20020929032419I](https://openairdocs.org/incident/20020929032419I), Sep 29, 2002: Saab SF340A (N106XJ), Charleston, WV, Minor damage. (-23) Crew received master caution due to hydraulic pressure low. Crew observed pressure approaching redline. Hydraulic level was normal. Qrh procedures were… - [Incident 20020925024929I](https://openairdocs.org/incident/20020925024929I), Sep 25, 2002: Cessna 340A (N104CQ), Pittsburgh, PA. (-23) During initial climb flight 4942 shut down the left engine due to a bleed air leak the aircraft landed at pit. Maintenance personnel replaced the bleed… - [Accident 20020721016169A](https://openairdocs.org/incident/20020721016169A), Jul 21, 2002: Saab 340A (N110XJ), Charleston, WV, No damage. (.19) On July 21, 2002, about 0930 eastern daylight time, a Saab 340A, N110XJ, operated by mesaba aviation inc. as northwest airlink flight 2742, was… - [Incident 20020416007909I](https://openairdocs.org/incident/20020416007909I), Apr 16, 2002: Cessna 340A (N43SZ), Bedford, MA, Minor damage. (-23) An us airways express (shuttle america uhla) N43SZ, SF-340-A aircraft contacted a taxiway fence while mechanics were repositioning the aircraft from the… - [Incident 20010406005969I](https://openairdocs.org/incident/20010406005969I), Apr 6, 2001: Cessna 340A (N95CQ), Pittsburgh, PA. (-23) On 4/6/01 at 8:45 am at Pittsburgh international airport chautauqua flight #4215 a saab-fairchild 340-A N95CQ aborted a takeoff on runway 28R. ATC… - [Incident 20001203030619I](https://openairdocs.org/incident/20001203030619I), Dec 3, 2000: Cessna 340A (N96CN), Fort Wayne, IN. (-23) Mechanic reported the following: I'm writing to you in regards to the chautaugua airlines saab 340-A a/c #N96CN that had an emergency landing on 12-4-00.… - [Incident 20001002038489I](https://openairdocs.org/incident/20001002038489I), Oct 2, 2000: Saab SF340A (N991XJ), Elmira, NY. (-23) On Monday, October 2, 2000 at 1207 local time, a Saab 340A aircraft, operated by mesaba aviation, inc d/b/a northwest airlink (mala), under 14 CFR part… - [Incident 20000727031939I](https://openairdocs.org/incident/20000727031939I), Jul 27, 2000: Cessna 340A (N79XJ), Fort Wayne, IN. (-23)Flight crew declared an emergency and landed at Fort Wayne, IN (kfwa) due to smoke in the cargo area. Aircraft landed without incident, cargo hold was… - [Incident 20000626034749I](https://openairdocs.org/incident/20000626034749I), Jun 26, 2000: Cessna 340A (N922MA), Memphis, TN, Minor damage. (-23)Responded to scene where company reported wing tip strike with jetway. Found aircraft at gate A-33, Memphis International Airport, with right wing tip… - [Incident 20000510018109I](https://openairdocs.org/incident/20000510018109I), May 10, 2000: Cessna 340A (N68XJ), Lincoln, NE. (-23)Mesaba airlines lfight 2792, SF-340, returned to Lincoln Municipal Airport, Lincoln, NE, due to a gear unsafe light. The iarcraft was ferreied to… - [Incident 20000225001319I](https://openairdocs.org/incident/20000225001319I), Feb 25, 2000: Cessna 340A (N922MA), Memphis, TN, Minor damage. (-23) While taxiing to gate, a baggage cart ws blown into the number 1 propellor, causing damage. Propellor was the only damage to the aircraft. Two minor… - [Incident 20000217003499I](https://openairdocs.org/incident/20000217003499I), Feb 17, 2000: Cessna 340A (N114XJ), Middletown, PA. On February 17, 2000, at 1214 hours (local time) a saab-340-B, N114XJ, registered to wilmington trust company trustee, on approach to Harrisburg international… - [Incident 19990606013869I](https://openairdocs.org/incident/19990606013869I), Jun 6, 1999: Saab SF340A (N114XJ), Rochester, NY. On Sunday June 6, 1999 at 1158 local during approach to Rochester international airport, the pilot experienced a loss of hydraulic fluid and main accumulator… - [Incident 19990317039859I](https://openairdocs.org/incident/19990317039859I), Mar 17, 1999: Cessna 340A (N406BH), Columbus, GA. Following the abnormal landing (hydraulic pressure and fluid loss) on runway 05, the crew taxied clear on the active runway via taxi-way c. asked by the ground… - [Incident 19990314016509I](https://openairdocs.org/incident/19990314016509I), Mar 14, 1999: Saab SF340A (N338BE), Syracuse, NY. (-5) On March 14, 1999, at 1739EST, Saab 340, s/n 340A-034, N338BE, operated by business express inc. reported electrical "fumes" in the cockpit while on… - [Accident 19981103031149A](https://openairdocs.org/incident/19981103031149A), Nov 3, 1998: Saab SF340A (N325PX), Memphis, TN, No damage, 1 fatal. (-23) Shara may, a ground crew member, was performing engine start assistance to the flight crew. Upon receiving the disconnect signal from the pilot, she… - [Incident 19981025033949I](https://openairdocs.org/incident/19981025033949I), Oct 25, 1998: Saab SF340A (N327PX), Springfield, MO. After takeoff, right hand fire warning light came on. Complied with checklist and blew fire bottles and shut down engine. Removed and replaced right hand fire… - [Incident 19980526026249I](https://openairdocs.org/incident/19980526026249I), May 26, 1998: Saab SF340A (N325PX), Little Rock, AR. On may 26, 1998, a fairchild Saab 340A, N325PX, registered to mcc financial corp. was operating as flagship 5124 level at 15000 approximately 70 miles… - [Incident 19980126002329I](https://openairdocs.org/incident/19980126002329I), Jan 26, 1998: Cessna 340A (N406BH), Springfield, MO. Narrative: eighty miles east of Springfield, MO (sgf), during cruise at 16,000', engine #1 propeller gear box failed. Aircraft declared an emergency and began… - [Incident 19970816027299I](https://openairdocs.org/incident/19970816027299I), Aug 16, 1997: Saab SF340A (N340BE), Rochester, NY. Narrative: on August 16, 1997 at 0700 EDT, a Saab 340, N340BE, flight 4200, operated by business express, returned to the Rochester international airport in… - [Incident 19970707035919I](https://openairdocs.org/incident/19970707035919I), Jul 7, 1997: Saab SF340A (N110XJ), Indianapolis, IN. Narrative: on July 07, 1997, Saab SF-340A aircraft, N110XJ, enroute from evansville, IN (evv) to detroit, mi (dtw) and operated under mesaba airlines flt 3025,… - [Incident 19970513015849I](https://openairdocs.org/incident/19970513015849I), May 13, 1997: Saab SF340A (N98XJ), Detroit, MI, Minor damage. Narrative: investigation revealed that the #2 main wheel outbd bearing had failed. The wheel is being evaluated to determine the cause of the failure. The… - [Incident 19970319010639I](https://openairdocs.org/incident/19970319010639I), Mar 19, 1997: Saab SF340A (N95CQ), Pittsburgh, PA, Minor damage. Narrative: the pilot stated: when taxiing in to gate E-9 at Pittsburgh, he was taxiing the aircraft between parked DO-328 and a truck. He thought he was clear… - [Incident 19960731024749I](https://openairdocs.org/incident/19960731024749I), Jul 31, 1996: Saab SF340A (N340BE), Albany, NY. Narrative: while enroute from btv to lga at 16,000 cruise right engine low oil pressure light illuminated and gauge indicated same. PIC declared emergency and… - [Incident 19960719027669I](https://openairdocs.org/incident/19960719027669I), Jul 19, 1996: Saab SF340A (N110XJ), Fort Wayne, IN. Narrative: on July 19, 1996 at approximately 1615 EST, mesaba airlines flight 3338, an SE340 model aircraft experienced a hydraulic failure during landing… - [Incident 19960331009729I](https://openairdocs.org/incident/19960331009729I), Mar 31, 1996: Saab SF340A (N327PX), Springfield, MO. Narrative: northwest airlink flight 5120 departed sgf on 3/31/96, at 0700 LCL. The crew experienced a tailpipe hot light on the #1 engine. The crew shut down… - [Incident 19950131004019I](https://openairdocs.org/incident/19950131004019I), Jan 31, 1995: Saab SF340A (N922MA), Monroe, LA. Narrative: during a flight from jackson, Mississippi to Monroe Regional Airport the cargo smoke light illuminated approximately 25 miles from the airport. The… - [Incident 19941218045059I](https://openairdocs.org/incident/19941218045059I), Dec 18, 1994: Saab SF340A (N325PX), Cedar Rapids, IA. Right engine chip light came on. Diverted to cid. Chips small enough to be no problem. - [Incident 19940704033819I](https://openairdocs.org/incident/19940704033819I), Jul 4, 1994: Saab SF340A (N922MA), Gulfport, MS. Narrative: aircraft was on a base leg for a landing to runway 32 at gulf port, MS when the right engine quit. Crew declared an emergency and landed without… - [Incident 19940515016339I](https://openairdocs.org/incident/19940515016339I), May 15, 1994: Saab SF340A (N347AM), Memphis, TN, Minor damage. Left engine torque gauge off scale on approach. Secured engine. Left engine propeller gear box had a failure. - [Incident 19940512016349I](https://openairdocs.org/incident/19940512016349I), May 12, 1994: Saab SF340A (N402BH), Muscle Shoals, AL. Right engine fire warning light on during climb. Diverted to huntsville. Found a faulty sensor box. - [Incident 19940306007609I](https://openairdocs.org/incident/19940306007609I), Mar 6, 1994: Saab SF340A (N402BH), Paducah, KY. Unsafe gear light after departure. Returned. Left gear collapsed. Broken bolt in left main gear shockstrut. - [Incident 19940126051999I](https://openairdocs.org/incident/19940126051999I), Jan 26, 1994: Saab SF340A (N325PX), Minneapolis, MN. Left engine lost power on descent. Shut engine down. Landed safely. Stainless steel tube failed. Lost P3 pressure - [Incident 19920711028959I](https://openairdocs.org/incident/19920711028959I), Jul 11, 1992: Saab SF340A (N407BH), Memphis, TN. Hydraulic system failed while taxiing for departure. Brake failed. Aircraft departed taxiway. - [Incident 19920601029429I](https://openairdocs.org/incident/19920601029429I), Jun 1, 1992: Saab SF340A (N935MA), Shreveport, LA. Lost hydraulic power on approach. Used emergency procedures. Landed safely. - [Incident 19920413014219I](https://openairdocs.org/incident/19920413014219I), Apr 13, 1992: Saab SF340A (N340BE), Boston, MA. Hung start fire first try after starter generator replaced. Pulled fire handle,evacuated aircraft,replaced gcu ok. - [Incident 19920123006569I](https://openairdocs.org/incident/19920123006569I), Jan 23, 1992: Saab SF340A (N325PX), Lafayette, LA. Lost both EFIS tubes on climbout. Returned. Landed safely. - [Incident 19911105060869I](https://openairdocs.org/incident/19911105060869I), Nov 5, 1991: Saab SF340A (N407BH), Memphis, TN. Unable to get gear down safe light. Hand pumped gear down and landed without incident. - [Incident 19911013049329I](https://openairdocs.org/incident/19911013049329I), Oct 13, 1991: Saab SF340A (N326PX), Memphis, TN, Minor damage. During taxi pilot lost nose wheel steering. Brakes ineffective. Coasted into a van. Hydraulic pump had failed. - [Incident 19910711032299I](https://openairdocs.org/incident/19910711032299I), Jul 11, 1991: Saab SF340A (N741BA), Rochester, NY, Minor damage. Struck a parked aircraft while maneuvering to park. - [Incident 19910522032149I](https://openairdocs.org/incident/19910522032149I), May 22, 1991: Saab SF340A (N325PX), Memphis, TN. Passenger had severe ear problem on deplaning. Aircraft was operated unpressurized with precautions. - [Incident 19910515040539I](https://openairdocs.org/incident/19910515040539I), May 15, 1991: Saab SF340A (N346AM), Memphis, TN. Hydraulic quanity pressure went to 0. Returned to airport. Used emergency procedures. Replaced hydraulic fitting. - [Incident 19900621036909I](https://openairdocs.org/incident/19900621036909I), Jun 21, 1990: Saab SF340A (N325PX), Pensacola, FL. Engine oil pressure loss on left engine on climb. Returned. Shut left engine down on rollout. - [Incident 19900426020959I](https://openairdocs.org/incident/19900426020959I), Apr 26, 1990: Saab SF340A (N326PX), Memphis, TN. Left engine chip detector warning. Secured. Declared emergency. Returned and landed without incident. All 69: https://openairdocs.org/model/saab-fairchild-340a/incidents.md ## Service difficulty reports (369, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000832](https://openairdocs.org/sdr/2026FA0000832), Sep 13, 2026: CLAMP. BROKEN. AIRCRAFT DEPARTED KHND. A FEW MINUTES AFTER REACHING FL 190 AND SETTING CRUISE POWER, THE LEFT ENGINE BEGAN TO LOSE POWER. THE LEFT ENGINE MANIFOLD PRESSURE BEG - [SDR 2026FA0000504](https://openairdocs.org/sdr/2026FA0000504), Jun 10, 2026: WHEEL HALF. CRACKED. 3-PIECE NOSE GEAR WHEEL ASSEMBLY CRACKS ON MIDDLE HUB ASSEMBLY #D30321. - [SDR 2026FA0000503](https://openairdocs.org/sdr/2026FA0000503), Jun 10, 2026: WHEEL. CRACKED. 3-PIECE NOSE GEAR WHEEL ASSEMBLY CRACKS ON MIDDLE HUB ASSEMBLY #D30321. - [SDR 2026FA0000327](https://openairdocs.org/sdr/2026FA0000327), May 7, 2026: ALTERNATOR. DESTROYED. ALTERNATOR INPUT SHAFT HAS BEEN DAMAGED DUE TO DETROYED DRIVE COUPLING. DRIVE COUPLING HUB NO LONGER ROUND AND WOODRUFF KEY SLOT NO LONGER VISIBLE AS THE HOLE I - [SDR 2025FA0000646](https://openairdocs.org/sdr/2025FA0000646), Sep 16, 2025: INTAKE DUCT. RUPTURED. R/H ENGINE MP WILL NOT GO OVER 32 INCHES ABOVE 15,000. PRESSURE TESTED THE RH ENGINE INTAKE SYSTEM AND FOUND THE REAR INTAKE PIPE TORN. - [SDR 2025FA0000002](https://openairdocs.org/sdr/2025FA0000002), Jan 3, 2025: ATTACH BRACKET. FAILED. THE ACFT LANDED WITH DOWN AND LOCKED INDICATIONS ON LEFT AND NOSE GEAR ONLY. THE RIGHT GEAR COLLAPSED ON LANDING CAUSING THE AIRCRAFT TO GO OFF THE RUNWAY INTO - [SDR 2022FA0000653](https://openairdocs.org/sdr/2022FA0000653), Aug 14, 2022: SHIMMY DAMPENER. FAULTED. NOSE SHIMMY ON TAKEOFF, ABORTED TAKEOFF TO VERIFY TIRE WAS NOT FLAT. REPORTED BY PILOT - [SDR 2022FA0000447](https://openairdocs.org/sdr/2022FA0000447), Aug 2, 2022: ELT. FALSE ACTIVATION. THE AIRCRAFT WAS SECURED AND PARKED ON THE KBOI NORTH RAMP FOR SEVERAL DAYS, WITHOUT MOVEMENT. THE ELT FALSELY ACTIVATED AROUND 0200 UTC ON 02AUG22, ALERTING TH - [SDR S1ZA202102000005](https://openairdocs.org/sdr/S1ZA202102000005), Mar 1, 2021: BULKHEAD. CRACKED. RIGHT MAIN FUEL TANK (TIP TANK) AFT BULKHEAD (PN: 0823400-109) CRACKED IN UPPER RADIUS. THIS BULK HEAD IS AN EXTENSION OF THE AFT WING SPARE IS THE ONLY ONE OF - [SDR 2021FA0000032](https://openairdocs.org/sdr/2021FA0000032), Feb 4, 2021: BELLCRANK. CRACKED. AFTER DISCOVERING FAILED RH MLG IDLER BELLCRANK, P/N 0841106-6, DECIDED TO PERFORM NDI INSPECTION OF LH MLG IDLER BELLCRANK P/N 0841106-5. MULTIPLE CRACK INITIA - [SDR 2021FA0000033](https://openairdocs.org/sdr/2021FA0000033), Feb 3, 2021: BELLCRANK. CRACKED. R/H INNER GEAR DOOR BELLCRANK IDLER HAD BROKEN IN TWO PIECES. CUSTOMER BOUGHT A NEW PART WITH HIM TO INSTALL. BREAKAGE LOOKED CLEAN WITH NO CORROSION AT THE BRE - [SDR 2021FA0000025](https://openairdocs.org/sdr/2021FA0000025), Jan 27, 2021: BELLCRANK. BROKEN. AFTER LANDING ON POSTFLIGHT WALK AROUND, DISCOVERED RT INBOARD GEAR DOOR OPEN. FOUND BELLCRANK ASSEMBLY IDLER RT, P/N 0841106-6 FAILED AT ARM THAT ATTACHES TO D - [SDR 2020FA0000525](https://openairdocs.org/sdr/2020FA0000525), Dec 7, 2020: PITOT TUBE. CRACKED. 24 MONTH 91.411 & 91.413 TEST WAS DUE ON AIRCRAFT. WE PERFORM A PITOT LEAK CHECK PRIOR TO PERFORMING THE STATIC SYSTEM TESTS TO ENSURE OUR TEST EQUIPMENT WILL F - [SDR 2020FA0000428](https://openairdocs.org/sdr/2020FA0000428), Sep 10, 2020: SWITCH. BROKEN. RIGHT GEAR DOWN LIGHT WOULD NOT ILLUMINATE ON LANDING. I LOOKED AT THE LANDING GEAR WHEN THE PLANE WAS TOWED IN TO MY SHOP. I FOUND THE LANDING GEAR MICRO SWITC - [SDR S1ZA2020081000004](https://openairdocs.org/sdr/S1ZA2020081000004), Aug 8, 2020: BELLCRANK. BROKEN. THE RIGHT MAIN GEAR IDLER BELL CRANK ASSY BROKE IN HALF. THE BREAK CAUSED THE INNER GEAR DOOR TO HANG FREE. THE POINT OF FAILURE HAD RUST IN THE CRACK. THE GEAR - [SDR S1ZA2019120500003](https://openairdocs.org/sdr/S1ZA2019120500003), Dec 5, 2019: CRANKCASE. CRACKED. CRACKED CRANK CASE. REMOVED ALL CYLINDERS DUE TO 4 BEING LOW COMPRESSION. 2 OTHER CYLINDERS WERE RECENTLY REPLACED BY PERSONS UNKNOWN AT EXACT TIME UNKNOWN. I F - [SDR S1ZA2019120500391](https://openairdocs.org/sdr/S1ZA2019120500391), Dec 5, 2019: SPAR. USED. LEFT MAIN FUEL TANK (TIP TANK) AFT BULKHEAD (PN: 0823400-109) CRACKED IN UPPER RADIUS. THIS BULK HEAD IS AN EXTENSION OF THE AFT WING SPARE AND IS ONE OF ONLY 2 - [SDR CA180907011](https://openairdocs.org/sdr/CA180907011), Sep 7, 2018: CLAMP. CRACKED. (CAN) DURING ANNUAL INSPECTION AS WELL AS IN CONJUNCTION WITH AD 2000-01-16, THE V-BAND CLAMP THAT ATTACHES THE WASTEGATE EXHAUST ELBOW TO THE EXHAUST HEADER AS - [SDR 2017FA0000348](https://openairdocs.org/sdr/2017FA0000348), Apr 19, 2017: CYLINDER HEAD. CRACKED. CRACKS IN THE HEADS ABOVE THE INTAKE PORT IN BOTH CYLINDERS. FUEL STAINING ON THE EXTERIOR OF THE HEAD. THIS IS THE THIRD AND FOURTH CYLINDERS THAT HAVE BEEN RE - [SDR SQPA032020170001](https://openairdocs.org/sdr/SQPA032020170001), Mar 20, 2017: PROPELLER. DETACHED. LEFT PROPELLER DEPARTED AIRCRAFT DURING CLIMBOUT. NO PRIOR INDICATION OF PROBLEMS WERE REPORTED BY PILOT - [SDR 2017FA0000363](https://openairdocs.org/sdr/2017FA0000363), Mar 17, 2017: LIFTER. SPALLED. BOTTOM SURFACE OF LIFTERS SPALLING CAUSING DAMAGE TO CAMSHAFT AND METAL CONTAMINATION TO ENGINE. - [SDR 2017FA0000361](https://openairdocs.org/sdr/2017FA0000361), Mar 17, 2017: LIFTER. FAILED. BOTTOM SURFACE OF LIFTERS SPALLING CAUSING DAMAGE TO CAMSHAFT AND METAL CONTAMINATION TO ENGINE. - [SDR 2017FA0000356](https://openairdocs.org/sdr/2017FA0000356), Mar 17, 2017: LIFTER. SPALLED. BOTTOM SURFACE OF LIFTERS SPALLING CAUSING DAMAGE TO CAMSHAFT AND METAL CONTAMINATION TO ENGINE. - [SDR 2016F00096](https://openairdocs.org/sdr/2016F00096), Mar 8, 2016: BOLT. FAILED. LEFT MLG SCISSORS ASSY. THE AN310-5 NUT GALLED OFF THE END OA AN AN175-20 BOLT. RESULTING IN THE FAILURE OF THE LT MLG SCISSORS ASSEMBLY. - [SDR CA151209003](https://openairdocs.org/sdr/CA151209003), Nov 22, 2015: WINDOW. CRACKED. (CAN) PILOT HEARD THE SIDE WINDOW CRACK WHEN HE WAS CRUISING AT 13,000 FT. WITH THE ACFT PRESSURIZED. THE WINDOW CRACKED FROM THE LOWER FORWARD EDGE TO THE STOR - [SDR YWYR2015112400001](https://openairdocs.org/sdr/YWYR2015112400001), Nov 16, 2015: CYLINDER. CRACKED. WHILE PERFORMING VISUAL INSPECTION DURING ANNUAL INSPECTION, TECH NOTED STAINING BETWEEN CYLINDER FINS ON INTAKE SIDE OF CYLINDER NR 6 ON RT ENGINE. CYLINDER CO - [SDR 3PSR20151012005](https://openairdocs.org/sdr/3PSR20151012005), Oct 12, 2015: BLADE. CRACKED. DURING A BEARING INSPECTION OF BLADE, PN 660713275, SN SF340-132 5019, A 6" CRACK AROUND THE BLADE SHANK WAS NOTED. THIS CRACK WAS VERIFIED WITH A FLUORESCENT P - [SDR CA060609001](https://openairdocs.org/sdr/CA060609001), Mar 12, 2015: AXLE. LOOSE. (CAN) NR 4 MAIN WHEEL ASSEMBLY OBSERVED TO BE HOT TO THE TOUCH DURING ROUTINE MAINTENANCE. WHEN THE AIRCRAFT WAS JACKED TO INVESTIGATE THE CAUSE, THE WHEEL APPE - [SDR NI6R201503050024](https://openairdocs.org/sdr/NI6R201503050024), Mar 5, 2015: CRANKCASE. CRACKED. DURING INVESTIGATION OF LT ENGINE OIL LEAK, A CRACK WAS DISCOVERED IN THE ENGINE CASE OTBD SIDE RUNNING BETWEEN THE NR 2 & NR 4 CYLINDERS. - [SDR NI6R201502260023](https://openairdocs.org/sdr/NI6R201502260023), Feb 26, 2015: PIN. BROKEN. RT ENGINE NR 5 WRIST PIN, INTERNAL ALUMINUM PIECE BROKEN. - [SDR BIGR20140725001](https://openairdocs.org/sdr/BIGR20140725001), Jul 20, 2014: ALTERNATOR. FRACTURED. THE RT ENGINE LOCKED UP DURING FLIGHT GOING INTO FEATHER AND COULD NOT BE RESTARTED. MAINTENANCE FOUND THE ENGINE NEARLY LOCKED UP BUT COULD STILL BE TURNED WIT - [SDR ANCF2014FA0000376](https://openairdocs.org/sdr/ANCF2014FA0000376), Jun 9, 2014: RESISTOR. BURNED. DURING ANNUAL INSPECTION, FOUND HEATER BLOWER LOW SPEED RESISTOR, BURNED. ATTACHED WIRE INSULATION WAS BURNED BACK ABOUT TWO INCHES . FOUND HEAT DAMAGE TO MOUNT - [SDR 2014FA0000361](https://openairdocs.org/sdr/2014FA0000361), Jun 4, 2014: POINTS. BROKEN. OWNER PERFORMED MAGNETO CHECK ON LT ENGINE AND FOUND MAGNETO INOPERABLE, UPON REMOVAL OF MAGNETO AND INSPECTION OF MAGNETO FOUND THE POINTS CONTACT BROKEN. - [SDR CA140630025](https://openairdocs.org/sdr/CA140630025), May 5, 2014: LINE. CHAFED. (CAN) WHILE REMOVING THE ENGINE FROM THE AIRFRAME, THE OIL LINE BETWEEN THE WASTEGATE CONTROLLER AND ABSOLUTE PRESSURE CONTROLLER WAS FOUND TO BE CHAFING AGAINS - [SDR CA140630024](https://openairdocs.org/sdr/CA140630024), May 3, 2014: CYLINDER HEAD. SEPARATED. (CAN) THE NR 6 CYLINDER HEAD SEPARATED BY FAILING THOUGH THE ALUMINUM CASTING. ENGINE WAS SHUTDOWN AND PROP FEATHERED AND LANDING WAS CARRIED OUT. THE ENGINE IS - [SDR 9BYR2014022000091](https://openairdocs.org/sdr/9BYR2014022000091), Feb 12, 2014: CYLINDER HEAD. CRACKED. PILOT STATED LOSS OF POWER/ROUGH RUNNING. DURING INVESTIGATION FOUND CYLINDER NR 3 CRACKED FROM TOP SPARK PLUG HOLE TO EXHAUST VALVE. CYLINDER NR 2 HEAD HAD SEP - [SDR 2013FA0000740](https://openairdocs.org/sdr/2013FA0000740), Dec 5, 2013: PIVOT ASSY. FAILED. BOTH PIVOT ARMS SUPPORTING THE PILOT SEAT BACK FAILED DURING TAXI, RENDERING THE SEATBACK USELESS. SPECIFIC INSPECTION FOR CRACKS AND CORROSION ON THE SEAT PIVO - [SDR 2013FA0000682](https://openairdocs.org/sdr/2013FA0000682), Nov 23, 2013: CYLINDER. CRACKED. CYLINDER ENGINE CRACKED. - [SDR 2013FA0000681](https://openairdocs.org/sdr/2013FA0000681), Nov 23, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR 2013FA0000680](https://openairdocs.org/sdr/2013FA0000680), Nov 23, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR LZ2R2014121700045](https://openairdocs.org/sdr/LZ2R2014121700045), Nov 13, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. - [SDR LZ2R2014121700035](https://openairdocs.org/sdr/LZ2R2014121700035), Nov 13, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. - [SDR LZ2R2013121600037](https://openairdocs.org/sdr/LZ2R2013121600037), Nov 13, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. - [SDR LZ2R2013121600754](https://openairdocs.org/sdr/LZ2R2013121600754), Nov 13, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. - [SDR 2013FA0000688](https://openairdocs.org/sdr/2013FA0000688), Nov 13, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR 2013FA0000687](https://openairdocs.org/sdr/2013FA0000687), Nov 13, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR 2013FA0000686](https://openairdocs.org/sdr/2013FA0000686), Nov 13, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR 2013FA0000685](https://openairdocs.org/sdr/2013FA0000685), Nov 13, 2013: CYLINDER. CRACKED. CRACKED ENGINE CYLINDER. - [SDR LZ2R2013121600028](https://openairdocs.org/sdr/LZ2R2013121600028), Jul 22, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. - [SDR LZ2R2013121600025](https://openairdocs.org/sdr/LZ2R2013121600025), Jul 22, 2013: CYLINDER. CRACKED. DURING INSPECTION, FOUND CYLINDER CRACKED. All 369: https://openairdocs.org/model/saab-fairchild-340a/reports.md ## STCs that may be installed (OpenAirDocs) (102, 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 ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc - [STC SA1673GL](https://openairdocs.org/stc/SA1673GL): Installation of landing gear harnesses. Aereos Repairs LLC - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST01701WI](https://openairdocs.org/stc/ST01701WI): Installation of a Collins HF-220 High Frequency Communication System. Worldwide Aviation LLC - [STC ST04683NY](https://openairdocs.org/stc/ST04683NY): Installation of an upgrade of Universal (UNS) Flight Management System, LPV monitor and/or an upgrade of TDR-94D for MODE S and ADS-B out. Scandinavian Avionics Design ApS - [STC ST04671NY](https://openairdocs.org/stc/ST04671NY): Dual Garmin GTN-650 Xi GPS/NAV/COMMs. Saskatoon Avionics Ltd - [STC SA9075SC-D](https://openairdocs.org/stc/SA9075SC-D): Recore of Hamilton Standard Heat Exchangers 779215-1 and 779215-2 for installation on the SAAB SF340A and 340B in accordance with Honeywell LORI Sealed Drawing List SDL3400-1, Revision B, dated 10 October 2005 or later FAA approved revision. Honeywell International Inc - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST03687NY](https://openairdocs.org/stc/ST03687NY): Installation of Alternate Cargo Net Location. Taby Air Maintenance - [STC ST00146WI-D](https://openairdocs.org/stc/ST00146WI-D): Installation of Bendix/King CAS 66A TCAS I System. Honeywell International Inc - [STC ST00224WI-D](https://openairdocs.org/stc/ST00224WI-D): Installation of Bendix/King CAS 67A TCAS II System. Honeywell International Inc - [STC ST03688NY](https://openairdocs.org/stc/ST03688NY): Conversion of the main passenger cabin to a class E cargo compartment for the carriage of freight and change to the location of rapid decompression vents for planned future bulk cargo loading operations. Taby Air Manintenance AB - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST04467AT](https://openairdocs.org/stc/ST04467AT): Installation of the dual Becker Avionics BXT6513-(000) ADS-B. Avionics Support Group Inc - [STC ST04012NY](https://openairdocs.org/stc/ST04012NY): Installation of the Garmin GTX-3000 Automatic Dependent Surveillance-Broadcast (ADS-B) Out System. C & L STC Holdings LLC - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST03242NY](https://openairdocs.org/stc/ST03242NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc - [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST02530SE](https://openairdocs.org/stc/ST02530SE): Installation of Securaplane Sealed Lead Acid Batteries. Securaplane Technologies - [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc - [STC ST02516LA](https://openairdocs.org/stc/ST02516LA): Replacement of existing ELT with ACK E-04 ELT Beacon and Sensor Systems S65-1231 ELT Antenna. ACK Technologies Inc - [STC ST01712WI](https://openairdocs.org/stc/ST01712WI): Modification of a Rockwell Collins, Inc. AHC-85( ) (AHRS) installation. Rockwell Collins Inc - [STC ST01474WI-D](https://openairdocs.org/stc/ST01474WI-D): Modication of a Rockwell Collins Weather Radar System installation. Rockwell Collins Inc - [STC SA3538SW](https://openairdocs.org/stc/SA3538SW): Installation of Refuel Panel Door Switch Guard. M7 Aerospace LLC - [STC SA3540SW](https://openairdocs.org/stc/SA3540SW): Installation of 16 place executive interior. M7 Aerospace LLC - [STC SA3657SW](https://openairdocs.org/stc/SA3657SW): Installation of a 19 place executive interior. M7 Aerospace LLC - [STC SA5965SW](https://openairdocs.org/stc/SA5965SW): Installation of rechargeable flashlights. M7 Aerospace LLC - [STC SA5968SW](https://openairdocs.org/stc/SA5968SW): Installation of Dual Davtron Digital Clocks. M7 Aerospace LLC - [STC SA5971SW](https://openairdocs.org/stc/SA5971SW): Installation of J.E.T. Standby Gyro-Horizon. M7 Aerospace LLC - [STC SA5972SW](https://openairdocs.org/stc/SA5972SW): Installation of TAI-80A SAT-TAS-TAT Indicators. M7 Aerospace LLC - [STC SA5973SW](https://openairdocs.org/stc/SA5973SW): Installation of IDC Standby Airspeed and Standby Altimeter. M7 Aerospace LLC - [STC SA5974SW](https://openairdocs.org/stc/SA5974SW): Installation of Copilot s IDC Airspeed, Vertical Speed and Rad-Bar Altimeter. M7 Aerospace LLC - [STC SA5975SW](https://openairdocs.org/stc/SA5975SW): Installation of Flight Fone V Communication System. M7 Aerospace LLC - [STC SA5977SW](https://openairdocs.org/stc/SA5977SW): Installation of 14 place executive interior. M7 Aerospace LLC - [STC ST03135NY](https://openairdocs.org/stc/ST03135NY): Activation of Free Directional Gyro Mode. ACS-NAI Limited - [STC SA3583SW](https://openairdocs.org/stc/SA3583SW): Installation of IDC Pneumatic Encoding Altimeter. M7 Aerospace LLC - [STC SA5967SW](https://openairdocs.org/stc/SA5967SW): Installation of Collins CTL Proline II (CTL-22/22/32/62/92, CAD62, BD136, and IND42C). M7 Aerospace LLC All 102: https://openairdocs.org/model/saab-fairchild-340a/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Cessna 340A](https://openairdocs.org/model/cessna-340a): 541 registered aircraft, registry code 2076405 - [Cessna 340A](https://openairdocs.org/model/cessna-340a): 2 registered aircraft, registry code 2073325 --- 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.