# N346AG: 1998 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: 340B446
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 20, 1998
- Certificate issued: June 30, 2022
- Expires: June 30, 2029
- Mode S code: A3D39F
- 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=346AG
- Page: https://openairdocs.org/aircraft/N346AG

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/N346AG/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 N346AG.

## FAA accident and incident reports

None matched to N346AG.

## Service difficulty reports (41)

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 29GA2019090400001](https://openairdocs.org/sdr/29GA2019090400001), Aug 30, 2019: BRAKE SYS. CONTAMINATED. FLIGHT: 72 GGT/FLL UPON LANDING REDUCE BREAKING AFFECTIVENESS. CORRECTIVE ACTION:PERFORMED BLEEDING OF BRAKES ASSEMBLIES IAW AMM 32-42-00-02. BRAKE SYSTEM TEST 
- [SDR 29GA2019060400001](https://openairdocs.org/sdr/29GA2019060400001), Jun 3, 2019: CONTROL UNIT. FAULTY. FLIGHT 0140, AFTER TAKE OFF TRIED TO PULL THE L/G HANDLE UP POSITION, HANDLE WOULD NOT MOVE, A LITTLE LATER HANDLE SUCESSFULLY MOVED TO THE UP POSITION. R & R L
- [SDR 29GA2019050300001](https://openairdocs.org/sdr/29GA2019050300001), May 2, 2019: LIGHT. UNSECURE. FLIGHT 0067 FLL/MCO REPORT: BETWEEN ROWS 3+4 ESCAPE PATH LIGHTING FALLS OFF INTO THE AISLE. CORRECTIVE ACTION: RESECURED ESCAPE PATH LIGHTING IAW AMM 33-50-20,
- [SDR 29GA2019040432503](https://openairdocs.org/sdr/29GA2019040432503), Mar 24, 2019: SLIDER. BROKEN. FLIGHT# 0102 REPORT: AIR STAIRS DOOR WILL NOT CLOSE. REMOVED & REPLACED SLIDING UNIT ASSY, NOT DEFECTS FOUND AT THIS TIME IAW SAAB 340 AMM 52-10-00.
- [SDR 29GA2018123100001](https://openairdocs.org/sdr/29GA2018123100001), Dec 29, 2018: WARNING LIGHT. FALSE ACTIVATION. FLIGHT#0059 PNS/TPA REPORT: LANDING GEAR IN TRANSIT LIGHT ILLUMINATED DESCENDING THROUGH SEVEN THOUSAND FEET. CORRECTIVE ACTION: PERFORMED GEAR SWING OPERATIONA
- [SDR 29GA2018122400001](https://openairdocs.org/sdr/29GA2018122400001), Dec 22, 2018: CONTROL PANEL. FAILED. FLIGHT# 0129 TLH/FLL REPORT: ON DESCENT SEGMENT LANDING GEAR HANDLE LIGHT ILLUMINATED AMBER COLOR WITHOUT MOVING THE HANDLE. CORRECTIVE ACTION: R/R LANDING GEAR
- [SDR 29GA2018121700004](https://openairdocs.org/sdr/29GA2018121700004), Dec 15, 2018: PRESSURE SWITCH. FAILED. FLIGHT# 0076 TPA/FLL REPORT: GEAR IN TRANSIT LIGHT ILLUMINATED IN FLIGHT UNTIL GEAR WAS PUT DOWN AND LOCKED. CORRECTIVE ACTION: R&R HYD PRESSURE SWITCH IAW SAAB
- [SDR 29GA2018060600001](https://openairdocs.org/sdr/29GA2018060600001), Jun 6, 2018: POWER SUPPLY. FAILED. SEVERAL SECTIONS OF THE EMERGENCY LIGHTS WERE INOPERATIVE. R & R THE POWER SUPPLIES 20LN AND 23LN IAW AMM 33-50-10-04-1. OPS CHECKED GOOD.
- [SDR 29GA201806028002](https://openairdocs.org/sdr/29GA201806028002), May 28, 2018: SKIN. DAMAGED. RAMP REPORTED DAMAGE TO LOWER FUSELAGE BELOW CARGO DOOR. INSPECTED AND FOUND THREE DENTS BELOW CARGO DOOR. MAPPED AREA FROM BS 649 TO APPROX THREE INCHES FWD OF
- [SDR 29GA2018052900001](https://openairdocs.org/sdr/29GA2018052900001), May 27, 2018: SPRING. FAULTY. MAIN CABIN DOOR HOLD OPEN LATCH, NOT WORKING PROPERLY. R & R THE SPRING ON DOOR LATCH IAW AMM 52-10-00-05.
- [SDR 29GA2018052500001](https://openairdocs.org/sdr/29GA2018052500001), May 24, 2018: BULB. INOPERATIVE. ARM LIGHT ON THE FLIGHT ATTENDANT LIGHT PANEL, THE EMERGENCY LIGHT SWITCH WAS INOPERATIVE. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BULB, OPS CHECKED GO
- [SDR 29GA2018050100001](https://openairdocs.org/sdr/29GA2018050100001), May 1, 2018: LIGHT. MALFUNCTIONED. GALLEY EMERGENCY LIGHTS ILLUMINATED WHEN THE FA TESTED EMERGENCY LIGHT SYSTEM. CYCLED THE CIRCUIT BREAKER L8. OPS CHECKED GOOD IAW AMM 33-50-00-02, 33-50-00-01,
- [SDR 29GA2018021900001](https://openairdocs.org/sdr/29GA2018021900001), Feb 17, 2018: CIRCUIT BREAKER. TRIPPED. CIRCUIT BREAKER L8 FOR THE CABIN & EXIT EMERGENCY LIGHTS, TRIPPED. RESET THE CIRCUIT BREAKER IAW 33-50-00, OPS CHECKED NORMAL..
- [SDR 29GA2017122900002](https://openairdocs.org/sdr/29GA2017122900002), Dec 29, 2017: SWITCH. LOOSE. FA EMERGENCY ARM LIGHT INOERATIVE. SECURED EMERGENCY ARM SWITCH ON THE FLIGHT ATTENDANT PANEL, EMERGENCY LIGHTING OPS TESTED GOOD IAW AMM 33-50-00-05.
- [SDR 29GA2017111800001](https://openairdocs.org/sdr/29GA2017111800001), Nov 17, 2017: BATTERY. FAILED. F/A EMERGENCY FLASHLIGHT INOP. R&R BATTERY FOR FO`S FLASHLIGHT IAW MM 25-62-10-04, OPS CHECK GOOD.
- [SDR 29GA2017082800001](https://openairdocs.org/sdr/29GA2017082800001), Aug 28, 2017: UPLOCK SWITCH. OUT OF ADJUST. GEAR TRANSIT LIGHT CAME ON FOR A FEW SECONDS THEN WENT OUT. 7,000 FEET AND 230 KTS. ADJUSTED NOSE GEAR UPLOCK SWITCH IAW AMM 32-69-15-02. LANDING GEAR EXTENSION
- [SDR 29GA201708240002](https://openairdocs.org/sdr/29GA201708240002), Aug 23, 2017: LANDING GEAR. MALFUNCTIONED. WHEN RETRACTING LANDING GEAR AFTER TAKEOFF THERE WAS A LOUD KNOCKING SOUND IN THE NOSE GEAR WELL, FOLLOWED BY A HIGH PITCHED WHINE FROM THE HYDRAULIC PUMP. RETR
- [SDR 29GA2017061800002](https://openairdocs.org/sdr/29GA2017061800002), Jun 16, 2017: UNKNOWN. MALFUNCTIONED. FLIGHT 0115 BIM/FLL. EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER ENGINE SHUT DOWN. RESET EMERGENCY EXIT LIGHTS IAW AMM 33-50-10. OPS CHECK NORMAL.
- [SDR 29GA2017032500001](https://openairdocs.org/sdr/29GA2017032500001), Mar 22, 2017: UNKNOWN. MALFUNCTIONED. FLIGHT 72 JAX-TPA. ON DECENT A/S INCREASED TO 240 KTS, FLAP LOCK UP LIGHT ILLUMINATED AS WELL AS GREEN LIGHT ON TEST PANEL, FLAP INDICATOR STARTED TO OSCILLATE 
- [SDR 29GA2017032300001](https://openairdocs.org/sdr/29GA2017032300001), Mar 22, 2017: RUDDER. BINDING. ON LANDING, RUDDER JAMMED ON CAPTAIN SIDE. I HAD NO MOVEMENT ON THE RUDDER PEDDLES LEFT OR RIGHT , THE COPIOT WAS ABEL TO ASSIST & THE ACFT SAFTLEY STOPPED TAI 
- [SDR 29GA2017030600001](https://openairdocs.org/sdr/29GA2017030600001), Mar 5, 2017: NUT. LOOSE. MAIN DOOR LATCHING MECHIANISM BROKEN. INSPECTED AND FOUND JAM NUT LOOSE ON TOP MAIN LATCHING MECHANISM. SECURED IAW CMM 52-60-01.
- [SDR 29GA2016122300001](https://openairdocs.org/sdr/29GA2016122300001), Dec 20, 2016: BATTERY PACK. INTERMITTENT. FORWARD EMERGENCY LIGHT WORKS INTERMITTENTLY. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECKED GOOD.
- [SDR 29GA2016082600001](https://openairdocs.org/sdr/29GA2016082600001), Aug 25, 2016: RETAINING CLIP. MISSING. OPEN DOOR LOCK INOPERATIVE. FOUND RETAINER RING MISSING ON MCD LATCH ASSY. INSTALLED RETAINER RING ON LATCH LEVER MCD GROUND RELEASE KNOB ASSY IAW AMM 52-10-00-
- [SDR 29GA2016032800003](https://openairdocs.org/sdr/29GA2016032800003), Mar 27, 2016: POWER SUPPLY. FAULTY. EMERGENCY POWER LIGHT ILLUMINATED DURING TAXI. R & R EMERGENCY POWER SUPPLY IAW AMM 24-35-10-04. OPS TEST SATISFACTORY.
- [SDR 29GA2016031700001](https://openairdocs.org/sdr/29GA2016031700001), Mar 16, 2016: MOTOR. WEAK. LANDING GEAR MOTOR STRAINS BEFORE COMING OUT OF DOWN AND LOCKED AFTER PLACING HANDLE IN RETRACT POSITION. SERVICED HYDRAULIC SYS LANDING GEAR OPS CHECKS GOOD.
- [SDR 29GA2016010400004](https://openairdocs.org/sdr/29GA2016010400004), Dec 30, 2015: ACCUMULATOR. UNKNOWN. MAIN ACCUMULATOR PRESSURE SETTLES AT 2,000 PSI. PERFORMED OPS CHECK, FOUND TO BE IN GOOD WORKING CONDITION, COULD NOT DUPLICATE.
- [SDR 29GA2016010400003](https://openairdocs.org/sdr/29GA2016010400003), Dec 30, 2015: ACCUMULATOR. PRESSURE LOSS. MAIN ACCUMULATOR LOSES PRESSURE IN FLIGHT WITHIN 2 MINUTES. PERFORMED OPS CHECK, FOUND TO BE IN GOOD WORKING CONDITION, COULD NOT DUPLICATE.
- [SDR 29GA2015122100002](https://openairdocs.org/sdr/29GA2015122100002), Dec 17, 2015: VALVE. MALFUNCTIONED. CAPTAINS SIDE BRAKE AUTHORITY IS MINIMAL REQUIRES EXCESSIVE PRESSURE. REPLACED BRAKE VALVE, OPS CHECK GOOD.
- [SDR 29GA2015120200004](https://openairdocs.org/sdr/29GA2015120200004), Dec 1, 2015: BRAKE. OUT OF LIMITS. WHILE EXITING THE HIGH SPEED TAXIWAY AFTER LANDING, AT APPROXIMATELY 40 KNOTS, LIGHT BRAKES WERE APPLIED. PLANE DID NOT SLOW DOWN WITH INCREASED BRAKING, PLANE 
- [SDR 29GA2015100700002](https://openairdocs.org/sdr/29GA2015100700002), Oct 4, 2015: BRAKE SYS. STIFF. BRAKES HARD TO STOP AIRCRAFT. BRAKES VERY STIFF. BLEED BRAKE SYSTEM IAW AMM 32-42-00-02. BRAKE SYS OPS CHECK GOOD.
- [SDR 29GA2015082100001](https://openairdocs.org/sdr/29GA2015082100001), Aug 18, 2015: ACCUMULATOR. LOW PRESSURE. MAIN HYDRAULIC ACCUMULATOR WILL NOT HOLD PRESSURE. BRAKES AND NOSE STEERING INTERMITTENT DUE TO LACK OF PRESSURE. PERFORMED OPS CHECK ON MAIN HYDRAULIC SYSTEM. 
- [SDR 29GA2014111100004](https://openairdocs.org/sdr/29GA2014111100004), Nov 10, 2014: COMPRESSOR. SMOKE. DURING CRUISE, F/A REPORTED LOUD BANG FOLLOWED BY ODOR OF SMOKE. REPLACED COMPRESSOR ASSY.
- [SDR 29GA2014071000001](https://openairdocs.org/sdr/29GA2014071000001), Jul 10, 2014: CONTROL PANEL. INOPERATIVE. DURING CLIMBOUT, WHEN GEAR HANDLE WAS MOVED UP, NO IN-TRANSIT LIGHT, GEAR RETRACTED AS NORMAL. DURING LANDING, GEAR IN-TRANSIT LIGHT WORKED OK. PUSH TO TEST ALS
- [SDR 29GA34621020414](https://openairdocs.org/sdr/29GA34621020414), Feb 4, 2014: UNKNOWN. SMOKE. F/A REPORTED SMOKE COMING FROM THE BACK OF THE ACFT, APPROXIMATELY 10 SECONDS FROM LANDING. TROUBLESHOT COOLING SYSTEM, OPENED FLOOR BOARDS, INSPECTED SUP AIR C
- [SDR 29GA34629092013](https://openairdocs.org/sdr/29GA34629092013), Sep 20, 2013: PRESSURE SWITCH. FAILED. LOST HYD PRESSURE IN MAIN ACCUMULATOR BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULL EMERGENCY LANDING GEAR HANDLE DECLARED EMERGENCY 1. T
- [SDR 2013FA0000549](https://openairdocs.org/sdr/2013FA0000549), Sep 20, 2013: HYDRAULIC SYSTEM. FAILED. LOST HYD PRESSURE IN MAIN ACCUMULATOR BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULL EMERGENCY LANDING GEAR HANDLE, DECLARED EMERGENCY 1 T
- [SDR 2013FA0000548](https://openairdocs.org/sdr/2013FA0000548), Sep 20, 2013: HYDRAULIC SYSTEM. FAILED. LOST HYD PRESSURE IN MAIN ACCUMULATOR, BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULLED EMERGENCY LANDING GEAR HANDLE DECLARED EMERGENCY 1
- [SDR 29GA2013031434633](https://openairdocs.org/sdr/29GA2013031434633), Mar 4, 2013: CONNECTOR. DAMAGED. FLIGHT 4021. EMERGENCY LIGHT ILLUMINATED ON THE GROUND AND PA SYSTEM WILL NOT WORK. REPAIRED WIRING ON CONNECTOR, OPS CHECKED SATISFACTORY.
- [SDR 29GA346333040413](https://openairdocs.org/sdr/29GA346333040413), Mar 4, 2013: CONNECTOR. MISWIRED. FLIGHT: 4021 TCB/FLL EMERGENCY LIGHT ILLUMINATED ON THE GROUND AND PA SYSTEM WILL NOT WORK. REPAIRED WIRING ON 463VP-J1 CONNECTOR OPERATIONAL CHECK SATISFACTORY
- [SDR 29GA34633010913](https://openairdocs.org/sdr/29GA34633010913), Jan 9, 2013: CIRCUIT BREAKER. POPPED. FLIGHT:4002 TLH/TPA PILOT REPORTED CIRCUIT BREAKER L8 POPPED IN FLIGHT. INSPECTED EMERGENCY LIGHT CONTROL SYSTEM NO DEFECTS NOTED, RESET EMERGENCY LIGHTS CIRCUI
- [SDR 29GA34632071812](https://openairdocs.org/sdr/29GA34632071812), Jul 18, 2012: DOWNLOCK SWITCH. INTERMITTENT. FLIGHT: TLH/TPA WHEN GEAR SELECTED DOWN HANDLE ONLY LEFT AND NOSE INDICATED DOWN GREEN, NO RIGHT GEAR INDICATED LIGHT RECYCLED GEAR AND GOT ALL THREE GEAR DOWN 

## 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/N346AG/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.