# N266AE: 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-266
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 1991
- Certificate issued: February 12, 2026
- Expires: February 28, 2033
- Mode S code: A2954C
- 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=266AE
- Page: https://openairdocs.org/aircraft/N266AE

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/N266AE/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 N266AE.

## FAA accident and incident reports (3)

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 20011130032479I](https://openairdocs.org/incident/20011130032479I), Nov 30, 2001: Saab 340B (N266AE), Boston, MA, Minor damage. (-23) After landing on 04R, the aircraft turned left onto runway 33L at Logan international airport. The right propeller and right landing gear struck a runway…
- [Incident 20000602020479I](https://openairdocs.org/incident/20000602020479I), Jun 2, 2000: Saab 340B (N266AE), Syracuse, NY, Minor damage. (-23) On June 2, 2000, at 2345EST, a Saab SF-340-B, s/n 340B-266, N266AE, registered to American eagle airlines inc., experienced hydraulic failure inbound to…
- [Incident 19920712034389I](https://openairdocs.org/incident/19920712034389I), Jul 12, 1992: Saab 340B (N266AE), Rochester, NY. Unsafe landing gear indication on approach. Landed safely. Found a faulty micoswitch.

## Service difficulty reports (37)

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 SMIA200807305](https://openairdocs.org/sdr/SMIA200807305), Mar 10, 2008: OVERHEAT SENSOR. MALFUNCTIONED. ON FLIGHT 3306, CREW REPORTED ON THE GROUND THEY GOT A LEFT ENGINE TAIL PIPE HOT LIGHT DURING CLIMB-OUT FOLLOWED AOM. LIGHT DID NOT GO OUT THEY THEN SHUT DOWN E
- [SDR SIMA200629001](https://openairdocs.org/sdr/SIMA200629001), Oct 16, 2006: WARNING LIGHT. FALSE ACTIVATION. CLL - FLT 3218 - RIGHT TAILPIPE HOT LIGHT CAME ON AT ROTATION ON TAKEOFF, LIGHT WENT OUT WITHIN 10 SECONDS. WEATHER TEMP 24 DEGREE CELSIUS AT 300 FEET, HEAVY RA
- [SDR SIMA200628204](https://openairdocs.org/sdr/SIMA200628204), Oct 7, 2006: BATTERY PACK. DISCHARGED. FLT 3218 - DFW - FRONT ENTRY EXIT SIGN, FORWARD EXIT SIGNS WILL NOT STAY ILLUMINATED. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY 21LN, IAW SAAB 340, AMM
- [SDR SIMA200621309](https://openairdocs.org/sdr/SIMA200621309), Jul 29, 2006: POWER SUPPLY. DISCHARGED. DFW - FLT 3224 - SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE AT FLOOR STATIONS 5B, 6B, 7B. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT 22L, IAW SAAB AMM 3
- [SDR SIMA200619406](https://openairdocs.org/sdr/SIMA200619406), Jul 11, 2006: DPU. FAILED. DFW - FLT 3243 - ABORTED TAKEOFF AND RETURNED TO GATE. DURING TAKEOFF ROLL A STRONG SMOKE ODOR WAS NOTICED IN THE CABIN. FOUND NR 1 DPU LOOSE IN RACK. REMOVED N
- [SDR SIMA200615904](https://openairdocs.org/sdr/SIMA200615904), Jun 6, 2006: ENGINE. MALFUNCTIONED. ABI - FLT 3234 - LEFT ENGINE OVERTEMP ON TAKEOFF 927 ABORTED TAKEOFF. LEFT ENGINE TEMP WITH LIMITS PER CT7-9B MM 72-00-00 FIG 201 SHEET 1. AIRCRAFT RETURNED TO 
- [SDR SIMA200220004](https://openairdocs.org/sdr/SIMA200220004), Jul 19, 2002: BATTERY. INOPERATIVE. EMERGENCY FLOOR LIGHTS, INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY SUPPLY IAW MM. OPS CHECK GOOD.
- [SDR SIMA200116001](https://openairdocs.org/sdr/SIMA200116001), Jun 8, 2001: POWER SUPPLY. DISCHARGED. BOS - FLT 4903 - ALL EMERGENCY LIGHTS OUT. REMOVED AND REPLACED ALL EMERGENCY POWER SUPPLIES (S/N 18592, 20519, 18440, 1878, 17288) IAW AMM, LOCATION 20LN - 24L
- [SDR SIMA200115623](https://openairdocs.org/sdr/SIMA200115623), Jun 5, 2001: LEVER. OUT OF RIG. ABI - FLT 9730 - ON TAKEOFF ROLL, LEFT ENGINE CTOT DID NOT ENGAGE. RIGGED LEFT CONDITION LEVERS IAW AMM 76-10-00. OPS CHECK GOOD. (M)
- [SDR SIMA20011411](https://openairdocs.org/sdr/SIMA20011411), May 21, 2001: WINDSHIELD. CRACKED. SMX - FLT 3146 - CREW REPORTED DURING CRUISE FLIGHT, THE FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED TO SMX. MAINTENANCE REMOVED AND REPLACED THE
- [SDR SIMA20011296](https://openairdocs.org/sdr/SIMA20011296), May 9, 2001: SMOKE DETECTOR. MALFUNCTIONED. PSP - FLT 3091 - AFTER START CREW GOT A CARGO SMOKE LIGHT INDICATION. CREW COMPLIED WITH CHECKLIST AND DISCHARGED FIRE BOTTLE. AIRCRAFT WAS FERRIED TO LAX FOR M
- [SDR SIMA200112203](https://openairdocs.org/sdr/SIMA200112203), May 2, 2001: LIGHT. INOPERATIVE. PSP - FLT 3098 - LEFT APR LIGHT FAILED TO ILLUMINATE ON TAKEOFF WHEN APR SELECTED ON. ABORTED TAKEOFF, MEL 76-2. REF LOG PAGE 1019987. (M)
- [SDR SIMA20011056](https://openairdocs.org/sdr/SIMA20011056), Apr 15, 2001: RELAY. FAILED. SAN - FLT 3210 - AFTER ARMING THE APR SYSTEM ON TAKEOFF ROLL, THE LEFT APR LIGHT DID NOT ILLUMINATE. PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DI
- [SDR 20010504AP005](https://openairdocs.org/sdr/20010504AP005), Jan 27, 2001: BULB. INOPERATIVE. SBP - FLT 3207 - EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE REPLACED BULB AT SEAT 11A AND FUSE AT POSITION 76LN. OPERATIONAL CHECK WAS GOOD AND 
- [SDR SIMA200102702](https://openairdocs.org/sdr/SIMA200102702), Jan 27, 2001: FUSE. INOPERATIVE. SBP - FLT 3207 - EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE REPLACED BULB AT SEAT 11A AND FUSE AT POSITION 76LN. OPERATIONAL CHECK WAS GOOD AND 
- [SDR 20010222SG001](https://openairdocs.org/sdr/20010222SG001), Jan 27, 2001: LIGHT. INOPERATIVE. SBP - MAINTENANCE REPORTED EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE FOUND FUSE 76LN AND REPLACED BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT
- [SDR SIMA0276](https://openairdocs.org/sdr/SIMA0276), Jan 27, 2001: FUSE. BLOWN. SBP - MAINTENANCE REPORTED EMERGENCY LIGHT ABOVE SEAT 11A IS INOPERATIVE. MAINTENANCE FOUND FUSE 76LN AND REPLACED BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT
- [SDR SIMA3433](https://openairdocs.org/sdr/SIMA3433), Dec 8, 2000: LAMP SOCKET. BURNED. LAX - FLT 3025 - CREW REPORTED BURNING SMELL IN CABIN BY ROW 3. MAINTENANCE INSPECTED AND FOUND SEAT 5BC WINDOW LIGHT FLOURESCENT LAMP HOLDER BURNED. LAMP HOLDE
- [SDR SIMA27313](https://openairdocs.org/sdr/SIMA27313), Dec 4, 2000: FRAME. CORRODED. SBP - LOWER FUSELAGE FRAME BELOW BULKHEAD 622 HAD CORROSION ON TEN RIVET HEADS. REMOVED AND REPLACED RIVETS IAW SAAB SRM. (X)
- [SDR SIMA2738](https://openairdocs.org/sdr/SIMA2738), Sep 25, 2000: RIVET. CORRODED. SBP - RIVETS AFT AND TO THE RIGHT OF THE FIRST OFFICER'S YOKE ARE CORRODED. MAINTENANCE REPLACED RIVETS IAW SAAB SRM. (X)
- [SDR SIMA2737](https://openairdocs.org/sdr/SIMA2737), Sep 25, 2000: FLOOR PANEL. CORRODED. SBP - AREA TO THE RIGHT OF THE FIRST OFFICER'S YOKE HAD CORROSION UNDER THE PAINT. MAINTENANCE REMOVED CORROSION AND REPAIRED WITH A DOUBLER IAW SAAB SRM . (X)
- [SDR SIMA2736](https://openairdocs.org/sdr/SIMA2736), Sep 25, 2000: STIFFENER. CORRODED. SBP - NUTPLATE BRACKETS AT BL 24L BETWEEN STA 272 AND STA 288 FOUND CORRODED AND CRACKED. MAINTEANCE REMOVED AND REPLACED BRACKETS IAW SAAB MM. (X)
- [SDR SIMA2735](https://openairdocs.org/sdr/SIMA2735), Sep 25, 2000: INTERCOSTAL. CRACKED. SBP - INTERCOSTAL AT BL 12L BETWEEN STA 272 AND STA 288 FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL IAW SAAB MM. (X)
- [SDR SIMA2734](https://openairdocs.org/sdr/SIMA2734), Sep 23, 2000: FRAME. CORRODED. SBP - THE UPPER FLANGE ON THE BOTTOM FRAME STA 225 WAS FOUND CORRODED. MAINTENANCE REPAIRED FLANGE IAW SAAB STRUCTURAL STATEMENT 340SDS000132. (X)
- [SDR SIMA27312](https://openairdocs.org/sdr/SIMA27312), Sep 19, 2000: PLATE. CORRODED. SBP - KICKPLATE AT STA 249 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED KICKPLATE IAW SAAB MM. (X)
- [SDR SIMA2733](https://openairdocs.org/sdr/SIMA2733), Sep 19, 2000: LINK. CORRODED. SBP - NOSE WHEEL STEERING LINKAGE HAD CORROSION AT UPPER U-JOINT. UNIVERSAL LINK WAS REMOVED AND REPLACED IAW SAAB MM. (X)
- [SDR SIMA27316](https://openairdocs.org/sdr/SIMA27316), Sep 14, 2000: BEAM. CORRODED. SBP - INTERCOSTAL BELOW LEFT GALLEY CORRODED. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL IAW SAAB SRM. (X)
- [SDR SIMA27315](https://openairdocs.org/sdr/SIMA27315), Sep 14, 2000: TRACK. CORRODED. SBP - AIRCRAFT STAIRS WERE FOUND CORRODED. MAINTENANCE REPLACED AIR STAIRS TRACK IAW SAAB MM. (X)
- [SDR 20001204SH003](https://openairdocs.org/sdr/20001204SH003), Sep 14, 2000: TRACK. CORRODED. SBP - LAVATORY TRACK AND PROFILE WERE FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY TRACK AND PROFILE. REF: OPER CONTROL NR SIMA27314. (X)
- [SDR SIMA27314](https://openairdocs.org/sdr/SIMA27314), Sep 14, 2000: TRACK. CORRODED. SBP - LAVATORY TRACK AND PROFILE WERE FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY TRACK AND PROFILE. REF: OPER CONTROL NR 20001204SH003. (X)
- [SDR SIMA27317](https://openairdocs.org/sdr/SIMA27317), Sep 13, 2000: SEAT TRACK. CORRODED. SBP - CABIN SEAT TRACK BL ZERO CORRODED BETWEEN STA 297 AND STA 351. MAINTENANCE REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION OF SEAT TRACK AND U-
- [SDR SIMA27311](https://openairdocs.org/sdr/SIMA27311), Sep 13, 2000: SUPPORT. CORRODED. SBP - WEB REINFORCEMENT AT STA 288 CORRODED. MAINTENANCE REMOVED AND REPLACED WEB REINFORCEMENT IAW SAAB SRM. (X)
- [SDR SIMA27310](https://openairdocs.org/sdr/SIMA27310), Sep 13, 2000: FRAME. CORRODED. SBP - FUSELAGE FRAME AT STA 272 CORRODED. MAINTENANCE REMOVED CORROSION AND INSTALLED A DOUBLER IAW SAAB STRUCTURAL REPAIR STATEMENT 340SDS000132. (X)
- [SDR SIMA2739](https://openairdocs.org/sdr/SIMA2739), Sep 13, 2000: FRAME. CORRODED. SBP - FUSELAGE FRAME AT STA 258 CORRODED. MAINTENANCE REPAIRED FRAME AT STA 258 IAW SAAB REPAIR STATEMENT 340SDS000132. (X)
- [SDR SIMA2183](https://openairdocs.org/sdr/SIMA2183), Aug 5, 2000: BULB. INOPERATIVE. ROC - FLT 4474 - EMERGENCY FLOOR PATH LIGHT INOPERATIVE AT ROW 7B. PUT ON MEL BY CREW. MAINTENANCE REPLACED EMERGENCY FLOOR PROXIMITY LIGHT BULB. OPERATIONAL CH
- [SDR 96ZZZX1443](https://openairdocs.org/sdr/96ZZZX1443), Dec 4, 1995: BUSHINGS. FAILED. TPA - FLT 5824 - VIBRATIONS IN CONTROLS DURING CLIMB AND DESCENT, DEACTIVATED YAW DAMPER. REPLACED ELEVATOR TAB BUSHINGS. FUNCTIONAL TEST FLT PASSED.
- [SDR 96ZZZM100](https://openairdocs.org/sdr/96ZZZM100), Dec 4, 1995: BUSHINGS. WORN. FLT NR 5824 - TPA - VIBRATIONS IN CONTROLS DURING CLIMB AND DESCENT, DEACTIVATED YAW DAMPER. REPLACED ELEVATOR TAB BUSHINGS. FUNCTIONAL TEST FLT PASSED. (M)

## 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/N266AE/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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