# N286AE: Saab-Scania SAAB 340B

- Status: Valid registration
- Airframe: [Saab-Scania SAAB 340B](https://openairdocs.org/model/saab-scania-saab-340b) (registry code 7860101, 37 seats)
- Engine: [GE CT7-SER series](https://openairdocs.org/engine/ge-ct7-ser-series) (registry code 30031)
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (Saab AB) (OpenAirDocs)
- Serial number: 340B-286
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 1992
- Certificate issued: February 13, 2026
- Expires: February 28, 2033
- Mode S code: A2E44A
- Registered owner: [Aviation Inventory Resources Inc](https://openairdocs.org/faa-owner/AVIATION%20INVENTORY%20RESOURCES%20INC)
- Location: [Alvarado, TX](https://openairdocs.org/faa-place/TX/Alvarado)
- Owner type: Corporation
- Owner's area on the map: 32.4162° N, 97.2002° W: Placed by OpenAirDocs at the center of ZIP code 76009, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=286AE
- Page: https://openairdocs.org/aircraft/N286AE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CT7-SER model are included.

## ADs that may apply (OpenAirDocs): 132 in force

### Matched by airframe (Saab-Scania SAAB 340B)

- [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 2023-13-07 R1](https://openairdocs.org/ad/2023-13-07-R1): Standard practices/structures · Saab AB Support and Services SAAB 340B. Effective Apr 18, 2024
- [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 2021-23-07](https://openairdocs.org/ad/2021-23-07): Lights · Saab AB Support and Services SAAB 340B. Effective Jan 5, 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 2017-22-09](https://openairdocs.org/ad/2017-22-09): Flight Controls · Saab AB, Saab Aeronautics SAAB 340B. Effective Dec 11, 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 2014-26-03](https://openairdocs.org/ad/2014-26-03): Flight controls · Saab AB, Saab Aerosystems SAAB 340B. Effective Feb 9, 2015
- [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 2004-11-02](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 2004-09-39](https://openairdocs.org/ad/2004-09-39): Remote controlled circuit breakers (RCCB) · Saab AB, Saab Aerosystems SAAB 340B. Effective Jun 15, 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 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 2000-23-29](https://openairdocs.org/ad/2000-23-29): Flight Idle Position · Saab AB, Saab Aerosystems SAAB 340B. Effective Dec 27, 2000
- [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

### Matched by engine (GE CT7-SER series)

- [AD 2025-05-15](https://openairdocs.org/ad/2025-05-15): Engine (Turbine/Turboprop) · General Electric Company GE CT7-2E1. Effective Apr 17, 2025
- [AD 2025-05-02](https://openairdocs.org/ad/2025-05-02): Engine (Turbine/Turboprop) · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective Apr 8, 2025
- [AD 2024-06-51](https://openairdocs.org/ad/2024-06-51): Engine (Turbine/Turboprop); Turbine Section · General Electric CT7-2E1, CT7-2F1, CT7-8A and 2 more. Effective Apr 23, 2024
- [AD 2023-21-07](https://openairdocs.org/ad/2023-21-07): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Dec 11, 2023
- [AD 2022-18-16](https://openairdocs.org/ad/2022-18-16): Turbine Engine Combustion Section, Turbine Section · General Electric CT7-8A. Effective Oct 7, 2022
- [AD 2017-19-20](https://openairdocs.org/ad/2017-19-20): Turbine Engine Compressor Section · General Electric CT7-8A and CT7-9B. Effective Oct 27, 2017
- [AD 2011-21-17](https://openairdocs.org/ad/2011-21-17): Fuel filter differential pressure switch. · General Electric CT7-8A, CT7-8A1, CT7-8E and 1 more. Effective Nov 17, 2011
- [AD 2011-19-03](https://openairdocs.org/ad/2011-19-03): Accessory gearbox (AGB) · General Electric CT7-8, CT7-8A, CT7-8A1 and 2 more. Effective Nov 9, 2011
- [AD 2010-23-20](https://openairdocs.org/ad/2010-23-20): Gas generator turbine (GGT) shafts · General Electric CT7-9C and CT7-9C3. Effective Dec 22, 2010
- [AD 2008-26-02](https://openairdocs.org/ad/2008-26-02): Electrical chip detectors · General Electric CT7-8A. Effective Jan 26, 2009
- [AD 2007-08-01](https://openairdocs.org/ad/2007-08-01): Eddy current inspection (ECI) of boltholes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective May 14, 2007
- [AD 2004-16-07](https://openairdocs.org/ad/2004-16-07): Turbine Stage 2 Aft Cooling Plates · General Electric CT7-2D1. Effective Aug 23, 2004
- [AD 2004-07-09](https://openairdocs.org/ad/2004-07-09): PGB oil filter impending bypass button (IBB) · General Electric CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective May 11, 2004
- [AD 2003-08-52](https://openairdocs.org/ad/2003-08-52): Compressor variable geometry (VG) · General Electric CT7-9B. Effective Jun 2, 2003
- [AD 2002-01-03](https://openairdocs.org/ad/2002-01-03): Stage 2 Turbine Aft Cooling Plates · General Electric CT7-5A2, CT7-5A3, CT7-7A and 1 more. Effective Feb 12, 2002
- [AD 97-25-07](https://openairdocs.org/ad/97-25-07): Stage 1 or 2 Gas Generator Turbine (GGT) Disk · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Jan 28, 1998
- [AD 96-26-01](https://openairdocs.org/ad/96-26-01): GGT Stage 2 Forward Cooling Plate · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Mar 10, 1997
- [AD 94-17-16](https://openairdocs.org/ad/94-17-16): Propeller Gearboxes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Sep 15, 1994
- [AD 93-25-17](https://openairdocs.org/ad/93-25-17): Gas Generator Turbine (GGT) Disks and Cooling Plates · General Electric CT7-2A, CT7-5A2, CT7-6 and 2 more. Effective Feb 2, 1994
- [AD 93-23-05](https://openairdocs.org/ad/93-23-05): Gas Generator Turbine (GGT) Rotor Assembly Parts and Power Turbine (PT) Disks · General Electric CT7-5A2 and CT7-7A. Effective Jan 10, 1994
- [AD 88-07-08](https://openairdocs.org/ad/88-07-08): Power Turbine Overspeed · General Electric CT7-5A2. Effective May 9, 1988

### Historical (superseded or no longer in force)

- [AD 2023-13-07](https://openairdocs.org/ad/2023-13-07) (historical): Standard practices/structures · Saab AB Support and Services SAAB 340B. Effective Jul 21, 2023
- [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 2005-04-12](https://openairdocs.org/ad/2005-04-12) (historical): Direct current (DC) starter generator · Saab SAAB 340B and SAAB SF340A. Effective Apr 1, 2005
- [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 2001-23-12](https://openairdocs.org/ad/2001-23-12) (historical): Aluminum Skin of Airplane · Saab SAAB 340B and SAAB SF340A. Effective Dec 31, 2001
- [AD 98-20-11](https://openairdocs.org/ad/98-20-11) (historical): Landing Gear · Saab SAAB 340B and SAAB SF340A. Effective Oct 28, 1998
- [AD 97-13-06](https://openairdocs.org/ad/97-13-06) (historical): Inspect Fluorescent Lamps And Lampholders · Saab AB, Saab Aerosystems SAAB 2000 and SAAB 340B. Effective Jul 7, 1997
- [AD 96-25-06 R1](https://openairdocs.org/ad/96-25-06-R1) (historical): Bushings in the Flap Fittings · Saab SAAB 340B and SAAB SF340A. Effective Jan 27, 1997
- [AD 96-25-06](https://openairdocs.org/ad/96-25-06) (historical): Bushings in the Flap Fittings · Saab SAAB 340B and SAAB SF340A. Effective Jan 27, 1997
- [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
- [AD 2024-05-51](https://openairdocs.org/ad/2024-05-51) (historical): Turbine Section · General Electric CT7-2E1, CT7-2F1, CT7-8A and 11 more. Effective Apr 1, 2024
- [AD 2018-03-13](https://openairdocs.org/ad/2018-03-13) (historical): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Feb 28, 2018
- [AD 2006-06-51](https://openairdocs.org/ad/2006-06-51) (historical): Electrical chip detectors for the No. 3 bearing · General Electric CT7-8A. Effective May 2, 2006
- [AD 2005-18-01](https://openairdocs.org/ad/2005-18-01) (historical): Turbine aft cooling plate boltholes · General Electric Aircraft Engines CT7-5A2, CT7-5A3, CT7-7A and 4 more. Effective Oct 24, 2005
- [AD 2003-06-03](https://openairdocs.org/ad/2003-06-03) (historical): Propeller gearbox (PGB) oil filter · General Electric Aircraft Engines CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective Apr 24, 2003

All 150: https://openairdocs.org/aircraft/N286AE/ads.md

## Information bulletins (advisory) (2 in force)

- [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
- [SAIB ANE-98-31](https://openairdocs.org/saib/ANE-98-31): . Issued May 15, 1998

## NTSB investigations

None matched to N286AE.

## FAA accident and incident reports

None matched to N286AE.

## Service difficulty reports (25)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SIMA200700601](https://openairdocs.org/sdr/SIMA200700601), Mar 1, 2007: CONTROL UNIT. FAILED. LEFT TAIL PIPE HOT WILL NOT TEST. REMOVED AND REPLACED LEFT FIRE DETECTION CONTROL UNIT IAW SAAB AMM 26-11-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERV
- [SDR SIMA200704408](https://openairdocs.org/sdr/SIMA200704408), Feb 10, 2007: UNKNOWN. UNKNOWN. LEFT TAIL PIPE LIGHT WOULD NOT ILLUMINATE DURING TEST. PERFORMED OPERATIONAL CHECK OF FIRE TEST SYSTEM WITH NO DEFECT NOTED IAW SAAB AMM 33-10-00. RETURNED AIRC
- [SDR SIMA200631817](https://openairdocs.org/sdr/SIMA200631817), Oct 21, 2006: FRAME. CORRODED. DISC - FOUND FUSELAGE FRAME STATION 225 CORRODED. REMOVED CORRISION WITH CUTOUT, FABRICATED FILLER AND DOUBLER, INSTALLED IAW SAAB SRM 53-70-30. AIRCRAFT RETURN
- [SDR SIMA200124902](https://openairdocs.org/sdr/SIMA200124902), Sep 6, 2001: CONTROL HANDLE. FAULTY. BGR - FLT 4929 - CREW INITIATED EMERGENCY LANDING DUE TO THE LEFT MAIN LANDING GEAR INDICATION NOT SHOWING DOWN AND LOCKED (GREEN) DURING APPROACH. MAINTENANCE 
- [SDR SIMA200121301](https://openairdocs.org/sdr/SIMA200121301), Aug 1, 2001: BATTERY. DISCHARGED. JFK - FLT 5018 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY ROW 4 AND 5 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT POSITION 20L
- [SDR SIMA20011414](https://openairdocs.org/sdr/SIMA20011414), May 21, 2001: BULB. INOPERATIVE. BOS - FLT 4932 - FOUND EMERGENCY OVERHEAD LIGHT AT ROW 10C IS INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB FOR EMERGENCY OVERHEAD LIGHT IAW SAAB AMM CH 33-50-00
- [SDR SIMA20011264](https://openairdocs.org/sdr/SIMA20011264), May 6, 2001: WEU. BOS - FLT 4749 - CREW REPORTED THE WARNING ELECTRONIC UNIT (WEU) BITE LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE WEU IAW SAAB MM. OP
- [SDR SIMA0932](https://openairdocs.org/sdr/SIMA0932), Apr 3, 2001: BULB. INOPERATIVE. BOS - FLT 5122 - CREW REPORTED AN EMERGENCY FLOOR LIGHT AT ROW 7BC TO BE INOPERATIVE. MAINTENANCE REPLACED BULB AT ROW 7BC IAW SAAB AMM. OPERATIONAL CHECK WAS G
- [SDR SIMA3601](https://openairdocs.org/sdr/SIMA3601), Dec 25, 2000: WARNING SYSTEM. MALFUNCTIONED. YOW - FLT 4598 - MAIN PAX DOOR HANDLE ILLUMINATED ON TO RETURNED TO YOW AND ISSUED MEL 52-1-2 AUTH 120661 CAT C. OPS CHECK OF SYSTEM NOTED NO PROBLEM. AIRCRAFT 
- [SDR SIMA2562](https://openairdocs.org/sdr/SIMA2562), Sep 12, 2000: ROLLER. LACK OF LUBE. SJT - FLT 3600 - GEAR INTRANSIT LIGHT STAYED ILLUMINATED AFTER GEAR WAS SELECTED UP. GEAR WAS CYCLED AND CONDITION REMAINED THE SAME. AIRCRAFT RETURNED TO FIELD
- [SDR SIMA2033](https://openairdocs.org/sdr/SIMA2033), Jul 21, 2000: FUSE. FAILED. DFW - FLT 3594 - EMERGENCY LIGHT AT ROW 4A AND 5B APPEARS TO BE BURNED OUT. PUT ON MEL AT THIS TIME. REMOVED AND REPLACED FUSE AT 65CN IAW 33-50-00. OPS CHECK G
- [SDR SIMA1874](https://openairdocs.org/sdr/SIMA1874), Jul 5, 2000: WARNING LIGHT. ILLUMINATED. ACT - FLT 3635 - AT 11,000 FEET CRUISE, SETTING UP FOR TREND, RT ENGINE OIL TEMPERATURE RISING ABOVE 150. RT OIL PRESSURE SLOWLY DROPPED BELOW 50. MONITORED AND
- [SDR SIMA1211](https://openairdocs.org/sdr/SIMA1211), Apr 30, 2000: SMOKE DETECTOR. MALFUNCTIONED. DFW - FLT 3395 - CARGO SMOKE LIGHT ILLUMINATED IN-FLIGHT. DISCHARGED FIRE EXTINGUISHER, DECLARED EMERGENCY. RETURNED TO DFW. FOUND AFT CARGO SMOKE DETECTOR DEFE
- [SDR SIMA0862](https://openairdocs.org/sdr/SIMA0862), Mar 26, 2000: BULB. INOPERATIVE. DFW - FLT 3607 - EMERGENCY FLOOR LIGHTS INOPERATIVE AT 9B. REMOVED AND REPLACED BULB AT 9B. OPS CHECK GOOD. (M)
- [SDR SIMA0194](https://openairdocs.org/sdr/SIMA0194), Jan 19, 2000: SEAT TRACK. CORRODED. ABI - REPAIR AT END OF SEAT TRACK BL 0.0 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED AREA OF SEAT TRACK AND REPAIR AREA IAW SAAB SRM 7
- [SDR SIMA0161](https://openairdocs.org/sdr/SIMA0161), Jan 16, 2000: SWITCH. INOPERATIVE. DFW - FLT 3687 - FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH WILL NOT STAY IN THE ON POSITION. LIGHT GOES OUT WHEN RELEASED. REMOVED AND REPLACED FLIGHT ATTENDANT E
- [SDR SIMA0081](https://openairdocs.org/sdr/SIMA0081), Jan 8, 2000: SEAT TRACK. CORRODED. ABI - FORWARD END OF SEAT TRACK AT BL 0 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED 11.5 INCHES OF SEAT TRACK AT BL 0 IAW SAAB SRM 72LKS 3079, 
- [SDR SIMA991371](https://openairdocs.org/sdr/SIMA991371), May 17, 1999: SMOKE DETECTOR. MALFUNCTIONED. SAN - FLT 3212 - AVIONICS SMOKE LIGHT ILLUMINATED. VERIFIED EVENT WAS A FALSE WARNING. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVIC
- [SDR SIMA991131](https://openairdocs.org/sdr/SIMA991131), Apr 23, 1999: SWITCH. FAILED. MRY - FLT 3215 - LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. DEFERRED LANDING GEAR AND ROUTED AIRCRAFT INTO SBP WHERE THE LEFT MAIN LANDING GEAR DO
- [SDR WWMA9800070](https://openairdocs.org/sdr/WWMA9800070), Apr 10, 1998: ENGINE. FIRE. DURING START OF NR 2 ENGINE, THE RAMPER OBSERVED FLAMES COMING FROM THE ENGINE TAILPIPE. START WAS ABORTED AND FIRE HANDLE WAS PULLED. RIGHT ENGINE FIRE BOTTLE 
- [SDR WWMA9700164](https://openairdocs.org/sdr/WWMA9700164), Oct 18, 1997: SMOKE DETECTOR. DEFECTIVE. DURING DESCENT, THE CARGO FIRE LIGHT ON THE CENTRAL WARNING PANEL ILLUMINATED, AFTER SEVERAL CYCLES IT SELF EXTINGUISHED. MAINTENANCE REPLACED BOTH THE FORWARD 
- [SDR WWMA9700041](https://openairdocs.org/sdr/WWMA9700041), Mar 22, 1997: ELECTRICAL SYS. ODOR. CREW REPORTED, BURNING SMELL COMING FROM THE AVIONICS BAY. MAINTENANCE PERFORMED OPERATIONAL CHECK OF ELECTRICAL SYSTEM, AVIONICS, INTERIOR LIGHTS AND HOT JUGS.
- [SDR WWMA9700023](https://openairdocs.org/sdr/WWMA9700023), Feb 10, 1997: BATTERY. DISCHARGED. DURING PREFLIGHT, THE CREW FOUND THE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHTING BATTERIES.
- [SDR WWMA9600108](https://openairdocs.org/sdr/WWMA9600108), Dec 22, 1996: PLUG. ARCED. CREW REPORTED AN UNUSUAL ODOR EMMITTING FROM THE HOT WATER JUGS. MAINTENANCE FOUND THE NR 1 HOT JUG ELECTRICAL PLUG ARCED, SYSTEM WAS DEACTIVATED AND DEFERRED D
- [SDR WWMA9600087](https://openairdocs.org/sdr/WWMA9600087), Oct 22, 1996: SMOKE DETECTOR. DEFECTIVE. CARGO SMOKE LIGHT CAME ON AND WOULD NOT GO OUT AFTER LANDING. MAINTENANCE REPLACED THE FORWARD CARGO SMOKE DETECTOR.

## STCs that may be installed (OpenAirDocs) (92, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Saab-Scania SAAB 340B)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [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 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 ST04751NY](https://openairdocs.org/stc/ST04751NY): Installation of Provisions for Underwing Stores. Airborne Holding Inc. dba Airborne Imaging
- [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 ST01436WI](https://openairdocs.org/stc/ST01436WI): Provides substitute floor panels in the cabin and cargo compartments. Worldwide Aviation LLC
- [STC ST01701WI](https://openairdocs.org/stc/ST01701WI): Installation of a Collins HF-220 High Frequency Communication System. Worldwide Aviation LLC
- [STC ST01894WI](https://openairdocs.org/stc/ST01894WI): Passenger to Cargo Service Conversion via the installation of a Class E Cargo Compartment. Worldwide Aviation LLC
- [STC ST03497AT](https://openairdocs.org/stc/ST03497AT): Installation of a Automatic Dependent Surveillance-Broadcast (ADS-B) System (data broadcast only, no cockpit display). Woven Electronics, LLC
- [STC ST03548AT](https://openairdocs.org/stc/ST03548AT): Installation of a Redundant GPS Signal to the Universal UNS-1K Flight Management System and associated hardware. Woven Electronics, 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 SA04179NY](https://openairdocs.org/stc/SA04179NY): Installation of the Special Mission Equipment Provisions. Aviation Repair Resources Inc
- [STC ST04179NY](https://openairdocs.org/stc/ST04179NY): Installation of the Special Mission Equipment Provisions. Aviation Repair Resources 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 ST09518SC](https://openairdocs.org/stc/ST09518SC): Installation of cabin and cargo floorboards. The NORDAM Group LLC
- [STC ST03242NY](https://openairdocs.org/stc/ST03242NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc
- [STC ST02499AK](https://openairdocs.org/stc/ST02499AK): Approval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installed. ADS-B Technologies, LLC
- [STC ST04136CH](https://openairdocs.org/stc/ST04136CH): Installation of a TFD-8601 EFIS (Electronic Flight Instrument System) Display. StandardAero Business Aviation Services, LLC
- [STC ST02530SE](https://openairdocs.org/stc/ST02530SE): Installation of Securaplane Sealed Lead Acid Batteries. Securaplane Technologies
- [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 ST01254AT](https://openairdocs.org/stc/ST01254AT): Enlarge Class 'C' cargo compartment by relocating cargo bay bulkhead forward to F.S. 594.1. SAAB Defense and Security USA LLC
- [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 ST03262NY](https://openairdocs.org/stc/ST03262NY): Installation of Quality Aircraft Interiors Oxygen Cylinder Restraint System (OCRS), P/N OCRS-1730-QAI, Models A & D. Quality Aircraft Interiors
- [STC ST01474WI-D](https://openairdocs.org/stc/ST01474WI-D): Modication of a Rockwell Collins Weather Radar System installation. Rockwell Collins Inc
- [STC ST03135NY](https://openairdocs.org/stc/ST03135NY): Activation of Free Directional Gyro Mode. ACS-NAI Limited
- [STC SA2470CE](https://openairdocs.org/stc/SA2470CE): Installation of B&D Instruments & Avionics, Inc. Electronic Propeller Gear Box Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7330-003-011, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7330-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate. Teledyne Controls
- [STC SA2471CE](https://openairdocs.org/stc/SA2471CE): Installation of B&D Instruments & Avionics, Inc. Electronic Engine Oil Pressure/Temperature Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7380-003-024, dated January 23, 1989, or later FAA Approved revision; (2) for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7380-003-024, dated August 29, 1989, or later FAA Approved revision; and (3) copy of this certificate. Teledyne Controls
- [STC SA2472CE](https://openairdocs.org/stc/SA2472CE): Installation of B&D Instruments & Avionics, Inc. Electronic Gas Generator Speed Indicator. Data required: (1) for the Model SF340A, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7320-003-011, dated January 23, 1989, or later FAA Approved revision; for the Model SF340B, B&D Instruments and Avionics, Inc. Installation Manual Part No. 7320-003-011, Revision B, dated August 29, 1989, or later FAA Approved revision; (2) for the SF340A or SF340B, B&D Instruments & Avionics, Inc. Installation Manual Part No. 7321-004-011 dated September 12, 1989, or later FAA Approved revision; and (3) copy of this certificate. Teledyne Controls

All 92: https://openairdocs.org/aircraft/N286AE/stcs.md

## Related

- Other Saab-Scania SAAB 340B aircraft: https://openairdocs.org/model/saab-scania-saab-340b/aircraft.md
- The GE CT7-SER series engine: https://openairdocs.org/engine/ge-ct7-ser-series.md

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