# N329AE: 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-329
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 23, 1993
- Certificate issued: April 24, 2019
- Expires: April 30, 2029
- Mode S code: A38FC4
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=329AE
- Page: https://openairdocs.org/aircraft/N329AE

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/N329AE/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 (1)

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 LAX98LA057](https://openairdocs.org/ntsb/LAX98LA057), Dec 11, 1997: Saab-Scania 340B (N329AE), Ventura, CA, no damage. Probable cause: Seat belt not used. A related factor was the unforecasted severe air turbulence.

## FAA accident and incident reports (1)

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.

- [Accident 19971211045509A](https://openairdocs.org/incident/19971211045509A), Dec 11, 1997: Saab 340B (N329AE), Ventura, CA. (.4) The captain reported that 20 minutes into a smooth flight, and 10 minutes before landing, he felt some light chop so he turned on the seat belt sign.…

## Service difficulty reports (44)

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 2024FA0000388](https://openairdocs.org/sdr/2024FA0000388), May 23, 2024: PROCESSING UNIT. SMOKE. PILOT REPORTS “L SIDE EADI WENT BLANK FOLLOWED BY STRONG, VISIBLE SMOKE IN THE COCKPIT. NO CB'S POPPED AT TIME OF FAILURE. DPU1 IN AVIONICS BAY FOUND TO BE THE 
- [SDR 2024FA0000387](https://openairdocs.org/sdr/2024FA0000387), May 23, 2024: PROCESSING UNIT. SMOKE. PILOT REPORTS “L SIDE EADI WENT BLANK FOLLOWED BY STRONG, VISIBLE SMOKE IN THE COCKPIT. NO CB'S POPPED AT TIME OF FAILURE. DPU1 IN AVIONICS BAY FOUND TO BE THE 
- [SDR SIMA200812107](https://openairdocs.org/sdr/SIMA200812107), Apr 16, 2008: SEAT TRACK. CORRODED. DURING A HMBV INSPECTION, THE SEAT TRACK AT BL 0.0 WAS FOUND TO BE CORRODED BETWEEN FS 297 TO FS 314. REMOVED 31 OF SEAT 31 OF SEAT TRACK FROM FS 297 TO FS 328.
- [SDR SIMA200725004](https://openairdocs.org/sdr/SIMA200725004), Sep 4, 2007: SMOKE DETECTOR. FAILED. AVIONIC SMOKE LIGHT INFLIGHT, WENT OUT AFTER 10 MINUTES FOLLOWING LEFT AND RIGHT AVIONIC SWITCHES SELECTED TO OFF. EMERGENCY DECLARED, RETURNED TO LAX. REMOVED 
- [SDR SIMA200718603](https://openairdocs.org/sdr/SIMA200718603), Jul 1, 2007: POWER SUPPLY. FAILED. EMERGENCY FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED 20LN EMERGENCY POWER SUPPLY IAW SAAB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
- [SDR SIMA200529003](https://openairdocs.org/sdr/SIMA200529003), Oct 14, 2005: DPU. INOPERATIVE. CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. REPLACED NR 2 DPU IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600453) (K)
- [SDR SIMA200526406](https://openairdocs.org/sdr/SIMA200526406), Sep 13, 2005: SEAT TRACK. CORRODED. SEAT TRACK BL0 WAS FOUND TO BE CORRODED BETWEEN STA 339 AND 363. BLENDED THE SEAT TRACKS TO REMOVE THE CORROSION. CUT A SECTION FROM U-BEAM FOR REPAIR. CLEANED 
- [SDR SIMA200316401](https://openairdocs.org/sdr/SIMA200316401), Jun 11, 2003: ENGINE. INOPERATIVE. AT 11,000 RT ENGINE MADE A LOUD BANG. OIL PRESSURE LIGHT CAME ON AS OIL PRESSURE DROPPED. ITT EXCEEDED 1200C AND INCREASING RAPIDLY, ENGINE SHUT DOWN PERFORMED.
- [SDR SIMA200126103](https://openairdocs.org/sdr/SIMA200126103), Sep 18, 2001: SMOKE DETECTOR. DIRTY. LAX - FLT 3269 - CREW REPORTED THE AVIONICS SMOKE LIGHT CAME ON DURING TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE CLEANED THE A
- [SDR SIMA200121101](https://openairdocs.org/sdr/SIMA200121101), Jul 30, 2001: BATTERY. INOPERATIVE. SAN - FLT 3212 - CREW REPORTED THE EMERGENCY OVERHEAD LIGHTS AT SEATS 9A, AND 11A, EMERGENCY EXIT LIGHT OVER SEAT 8A, AND FLOOR PROXIMITY LIGHTS AT 8BC AND 10BC
- [SDR SIMA200117601](https://openairdocs.org/sdr/SIMA200117601), Jun 25, 2001: BATTERY. INOPERATIVE. SBP - FOUND CABIN EMERGENCY EXIT LIGHTS OUT. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY IAW SAAB AMM 33-50-00. (M)
- [SDR SIMA200117403](https://openairdocs.org/sdr/SIMA200117403), Jun 23, 2001: MODULE. MALFUNCTIONED. SBA - FLT 3037 - ON TAKEOFF ROLL, LEFT ENGINE APR DID NOT ARM. ABORTED TAKEOFF. ISSUED MEL 76-02. (M)
- [SDR SIMA20011295](https://openairdocs.org/sdr/SIMA20011295), May 9, 2001: BATTERY PACK. DISCHARGED. FLT 3003 - SAN - CREW REPORTED THE EMERGENCY LIGHTS FAIL AFTER 15 SECONDS. AIRCRAFT WAS FERRIED TO LAX FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED BATTERY
- [SDR SIMA2211](https://openairdocs.org/sdr/SIMA2211), Jul 28, 2000: PANEL. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND CORROSION ON THE ENTRY WAY KICK PLATE AT FS 294. REPLACED ENTRY WAY KICK PLATE IAW SAAB AMM 51-40-21 AND 51-20-50. (M)
- [SDR SIMA2212](https://openairdocs.org/sdr/SIMA2212), Jul 28, 2000: SEAT TRACK. CORRODED. SBP - DURING 500 HOUR INSPECTION, FOUND CORROSION ON FORWARD END OF 18.3 BL LEFT SEAT TRACK. CUT SEAT TRACK AT FS 325.8 AND INSTALLED NEW SECTION OF REPAIR TRAC
- [SDR SIMA2215](https://openairdocs.org/sdr/SIMA2215), Jul 28, 2000: RIVET. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND CORROSON ON LOWER FUSELAGE RIVET HEADS BETWEEN STATION 518 AND 535 AT BL 0.0. REPLACED 43 RIVETS IAW SAAB SRM 51-40-21.
- [SDR SIMA2213](https://openairdocs.org/sdr/SIMA2213), Jul 27, 2000: INTERCOSTAL. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND CORROSION ON FUSELAGE INTERCOSTAL AND ANGLE BETWEEN FS 272 AND FS 288 IN CABIN ENTRY AREA. REPLACED INTERCOSTAL P/N 725
- [SDR SIMA2214](https://openairdocs.org/sdr/SIMA2214), Jul 27, 2000: FRAME. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND CORROSION ON FUSELAGE CABIN BOTTOM FRAME AT STATION 272 AT BL 0 BETWEEN BLR 15 AND BLR 24. REPAIRED FRAME BY INSERTION 
- [SDR SIMA22113](https://openairdocs.org/sdr/SIMA22113), Jul 26, 2000: ANGLE. CORRODED. SBP - DURING 5000 HOUR INSPECTIN, FOUND CORROSION ON ANGLE PART NUMBER 7253722-001 AT FUSELAGE STATION 258 IN CABIN ENTRANCE AREA. REPLACED ANGLE IAW SAAB STRUC
- [SDR SIMA22112](https://openairdocs.org/sdr/SIMA22112), Jul 26, 2000: FRAME. CORRODED. DURING 5000 HOUR INSPECTION, FOUND CORROSION ON THE UPPER AFT FACING FLANGE OF CABIN BOTTOM FRAME UPPER FLANGE AT STATION 258 BETWEEN BL10 AND RBL 10.0. CUT OUT
- [SDR SIMA22111](https://openairdocs.org/sdr/SIMA22111), Jul 26, 2000: SEAT TRACK. CORRODED. DURING 5000 HOUR INSPECTION, FOUND SEAT TRACK BL 15.8 AND ATTACHMENT PROFILE FROM STATION 216-272 IN LAVATORY AREA CORRODED. REPLACED LAVATORY TRACK PART NR 725
- [SDR SIMA2219](https://openairdocs.org/sdr/SIMA2219), Jul 17, 2000: TRACK. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND LAVATORY TRACK 15, 8 AND ATTACHMENT PROFILE CORRODED. REPLACED LAVATORY TRACK RBL 15, 8 AND PROFILE, P/N 7253721-495. (
- [SDR SIMA2218](https://openairdocs.org/sdr/SIMA2218), Jul 17, 2000: TRACK. CORRODED. SBP - FOUND DURING 5000 HOUR INSPECTION, FOUND AIRSTAIRS TRACK CORRODED. REPLACED AIRSTAIRS TRACK. (M)
- [SDR SIMA2216](https://openairdocs.org/sdr/SIMA2216), Jul 17, 2000: INTERCOSTAL. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND FUSELAGE INTERCOSTAL UNDER FLOORBOARD IN FORWARD ENTRANCE AREA BETWEEN STATIONS 236.5 AND 258 CORRODED. REPLACED INTERC
- [SDR SIMA2217](https://openairdocs.org/sdr/SIMA2217), Jul 17, 2000: ANGLE. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND FUSELAGE ANGLE UNDER FLOORBOARD IN FORWARD ENTRANCE AREA BETWEEN STATIONS 236.5 AND 258 CORRODED. REPLACED ANGLE. (M)
- [SDR SIMA22110](https://openairdocs.org/sdr/SIMA22110), Jul 16, 2000: INTERCOSTAL. CORRODED. SBP - DURING 5000 HOUR INSPECTION, FOUND INTERCOSTAL IN CABIN ENTRANCE AREA BETWEEN STATION 272 AND 288 CORRODED. REMOVED AND REPLACED INTERCOSTAL. (M)
- [SDR SIMA1536](https://openairdocs.org/sdr/SIMA1536), Jun 1, 2000: SEAL. FAILED. DFW - FLT 3330 - NR 2 OIL CWP WARNING ON IN FLIGHT. SHUT DOWN NR 2 AS PRECAUTION. OIL PRESSURE FLUCTUATED PLUS MINUS 15-20 PSI AV. 20-25 PSI IN YELLOW AND RED A
- [SDR 20000703AP014](https://openairdocs.org/sdr/20000703AP014), May 29, 2000: BATTERY PACK. DISCHARGED. JFK - ALL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW WORK CARD. OPS CHECK GOOD. (M)
- [SDR 20000703AP013](https://openairdocs.org/sdr/20000703AP013), May 29, 2000: BATTERY PACK. DISCHARGED. JFK - ALL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW WORK CARD. OPS CHECKS GOOD. (M)
- [SDR 20000703AP012](https://openairdocs.org/sdr/20000703AP012), May 29, 2000: BATTERY PACK. DISCHARGED. JFK - ALL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW WORK CARD. OPS CHECK GOOD. (M)
- [SDR SIMA1501](https://openairdocs.org/sdr/SIMA1501), May 29, 2000: BATTERY PACK. DISCHARGED. JFK - FOUND ALL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW WORK CARD. OPS CHECK GOOD. (M)
- [SDR SIMA990086](https://openairdocs.org/sdr/SIMA990086), Jan 8, 1999: BULB. FAILED. DFW - FLT 5026 - SEVERAL FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHTS BULBS. OPERATINOAL CHECK GOOD. (M)
- [SDR SIMA9822212](https://openairdocs.org/sdr/SIMA9822212), Aug 9, 1998: BATTERY PACK. DISCHARGED. FLT 5055 - CREW FOUND EMERGENCY LIGHT SWITCH WAS LEFT IN THE ARM POSITION, ALL AIRCRAFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED ALL EMERGENCY L
- [SDR WWMA9800065](https://openairdocs.org/sdr/WWMA9800065), Apr 2, 1998: DETECTOR. DEFECTIVE. FLIGHT NR 5042 -BTR-DFW - CARGO SMOKE LIGHT ON CWP ILLUMINATED IN FLIGHT. CARGO EXTINGUISHER NR 1 WAS DISCHARGED. DIVERTED TO AEX. REPLACE NR 1 CARGO FIRE BOTTL
- [SDR WWMA9700214](https://openairdocs.org/sdr/WWMA9700214), Dec 26, 1997: BULB. FAILED. DURING PREFLIGHT, THE EMERGENCY ARM LIGHT ON THE FLIGHT ATTENDENTS PANEL FAILED TO ILLUMINATE. REPLACED BULB.
- [SDR WWMA9700105](https://openairdocs.org/sdr/WWMA9700105), Jul 28, 1997: LAMP. FAILED. EMERGENCY LIGHT ABOVE SEAT 4A WAS INOPERATIVE. MAINTENANCE RELAMPED LIGHT ABOVE 4A.
- [SDR WWMA9700084](https://openairdocs.org/sdr/WWMA9700084), May 28, 1997: SMOKE DETECTOR. DEFECTIVE. DURING FLIGHT, THE CARGO SMOKE LIGHT CAME ON 3 TO 4 TIMES MOMEMTARILY THEN WENT OUT. REPLACED BOTH FORWARD AND AFT CARGO SMOKE DETECTORS.
- [SDR WWMA9700079](https://openairdocs.org/sdr/WWMA9700079), May 23, 1997: SMOKE DETECTOR. DEFECTIVE. LAVATORY SMOKE LIGHT ILLUMINATED. REPLACED LAVATORY SMOKE DETECTOR.
- [SDR WWMA9600086](https://openairdocs.org/sdr/WWMA9600086), Sep 2, 1996: ACM. SEIZED. CREW REPORTED, THAT THE RIGHT AIR CYCLE MACHINE ONLY BLOWS HEAT, SMELLED AN ELECTRICAL SMELL WITH BLEEDS ON AND PASSENGERS REPORTED A GRINDING SOUND IN THE BACK
- [SDR SIMA952771](https://openairdocs.org/sdr/SIMA952771), Oct 4, 1995: PROP BLDE SHEATH. MISSING. DURING CLIMB-OUT AT 4,000, PILOT NOTICED AND ENGINE SURGE AND ASSOCIATED PROP VIBRATION FROM NR 2 ENGINE. UPON RETURNING TO DFW, MAINTENANCE FOUND THE RIGHT PRO
- [SDR SIMA952621](https://openairdocs.org/sdr/SIMA952621), Sep 19, 1995: SMOKE DETECTOR. MALFUNCTIONED. FSM - FLT NR 3690 - AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT, BLEW FIRE BOTTLE AND DIVERTED TO FSM. RAI'D SMOKE DETECTOR (GROUND OPS CHECK GOOD) AND REPLAC
- [SDR SIMA951582](https://openairdocs.org/sdr/SIMA951582), Jun 7, 1995: WHEEL ASSY. BROKEN. DFW - WHEEL ASSEMBLY P/N 5010488, S/N JUL920711, WAS REMOVED FROM AIRCRAFT IN DFW AND SENT TO WHEEL SHOP. THE WHEEL ASSEMBLY HAS A 10 INCH SECTION OF INNER FLAN
- [SDR SIMA950931](https://openairdocs.org/sdr/SIMA950931), Apr 3, 1995: WHEEL. CRACKED. LAW/SHOP - DURING TEAR DOWN AND INSPECTION OF WHEEL ASSEMBLY FOR TIRE REPLACEMENT IN THE SHOP, A .50 INCH CRACK WAS FOUND BY NDT. INSPECTION, TRAVELING ACROSS T
- [SDR SIMA950871](https://openairdocs.org/sdr/SIMA950871), Mar 28, 1995: WHEEL. BROKEN. MLJ - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN MLI AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 12 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER

## 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/N329AE/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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