# N417XJ: 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: 340B417
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 7, 1997
- Certificate issued: November 12, 2021
- Expires: November 30, 2028
- Mode S code: A4F037
- 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=417XJ
- Page: https://openairdocs.org/aircraft/N417XJ

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/N417XJ/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 N417XJ.

## FAA accident and incident reports

None matched to N417XJ.

## Service difficulty reports (96, newest 50)

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 4EZF20250215001](https://openairdocs.org/sdr/4EZF20250215001), Feb 10, 2025: STARTER GEN. DEFECTIVE. FLIGHT CREW PIREP: RIGHT ENGINE WOULD NOT START - AFTER TROUBLESHOOTING MAINTENANCE REPLACED THE RT STARTER GENERATOR & GCU. OPERATIONAL TEST PERFORMED OK FOR S
- [SDR 4EZF20240715001](https://openairdocs.org/sdr/4EZF20240715001), Jul 15, 2024: WINDSHIELD. NONE. FLIGHT CREW REPORT: BIRD STRIKE DURING DEPARTURE TNCB, INSPECTION REQUIRED. MTX ACTION: PERFORMED INSPECTION OF THE FRONT AND SIDE WINDSHIELD, NO DISCREPANCY FO
- [SDR 4EZF202405240001](https://openairdocs.org/sdr/4EZF202405240001), May 23, 2024: NONE. NONE. CREW ENTRY: BIRD STRIKE ON ROTATION (TNCC) - MTX ENTRY: CARRIED OUT A GVI AS PER GMM/AMP FOUND NO DAMAGE TO NLG OR NLG DOORS WHERE BLOOD STAINS WERE NOTED.
- [SDR 4EZF0803202401](https://openairdocs.org/sdr/4EZF0803202401), Apr 2, 2024: CONNECTOR. DIRTY. LEFT PROP OIL GAUGE FLUCTUATION HEAVILY THEN TO FULL SCALE DEFLECTION VARIOUS POWER SETTINGS. SYSTEM HAS BEEN CHECKED FOR LEAKAGE AND BLOCKAGE NO LEAK HAS BEEN 
- [SDR 4EZF2023032700001](https://openairdocs.org/sdr/4EZF2023032700001), Mar 26, 2023: UNKNOWN. UNKNOWN. N417XJ, WITH FLIGHT NUMBER 7Z500 WAS IN ROUTE FROM BON WITH DESTINATION MDE. DURING THE CRUISE, THE FLIGHT CREW EXPERIENCED R BLEED FAULT AT FL220 (CABIN PRESSU
- [SDR 4EZF20230326001](https://openairdocs.org/sdr/4EZF20230326001), Mar 26, 2023: UNKNOWN. UNKNOWN. CREW REPORT: R BLEED FAULT AT FL220 AND RH-ENG TRQ DROPPED TO 0%. ITT WENT UP TO 1000°, OV TEMP LIGHT CAME ON.
- [SDR 4EZF202301310038](https://openairdocs.org/sdr/4EZF202301310038), Jan 30, 2023: ENGINE. POWER LOSS. AFTER INITIATING DESCENT (ROUTE SKRG TO TNCC) A LOUD SOUND WAS HEARD COMING FROM LEFT ENGINE AND LOST TORQUE AND ITT RAISED TO APPROXIMATELY 900 DEGREES CELCIUS
- [SDR 2022FA0000597](https://openairdocs.org/sdr/2022FA0000597), Oct 11, 2022: WHEEL. DEFLATED. DURING TOUCH DOWN FLIGHT CREW OBSERVED A SUDDEN PITCH UP OF THE AIRCRAFT, TO COUNTER THE PITCH UP POWER WAS ADDED TO PUSH NOSE DOWN, FOLLOWING WITH BRAKING ACTI
- [SDR 29GA2021022400001](https://openairdocs.org/sdr/29GA2021022400001), Feb 23, 2021: ACTUATOR. FAILED. FLIGHT# 9001 BGR/BGR REPORT: GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH RAN QRH AIR RETURN TO BGR. CORRECTIVE ACTION: REMOVED AND REPLACED NLG RETRACT ACTUATOR P
- [SDR 29GA2020072700001](https://openairdocs.org/sdr/29GA2020072700001), Jul 25, 2020: PUMP. INOPERATIVE. FLIGHT: 0147 BHB/BOS HYDRAULIC CAUTION LIGHT ILLUMINATED IN FLIGHT MAIN PSI DROPPED TO ZERO. CORRECTIVE ACTION: REPLACED MAIN HYDRAULIC PUMP, OPERATIONAL CHECKE
- [SDR 29GA2019041500001](https://openairdocs.org/sdr/29GA2019041500001), Apr 14, 2019: COVER. BROKEN. FLIGHT# 102 2F EMERGENCY EXIT PULL HANDLE COVER FELL OFF. CORRECTIVE ACTION: R/R 2F EMERGENCY EXIT COVER IAW 52-20-05 SAAB AMM.
- [SDR 29GA2018072000001](https://openairdocs.org/sdr/29GA2018072000001), Jul 19, 2018: CONNECTOR. DIRTY. FLIGHT 0068 FLL/MHH REPORT: EMERGENCY LIGHTS ARE NOT ILLUMINATED FROM FORWARD EMERGENCY EXITS TO ROW 7 AND FA EMERGENCY LIGHT SWITCH IS NOT WORKING. CLEANED AND
- [SDR 29GA2018060700001](https://openairdocs.org/sdr/29GA2018060700001), Jun 6, 2018: LIGHT. INOPERATIVE. DURING PREFLIGHT, EMERGENCY LIGHT WAS NOT WORKING. CYCLED CIRCUIT BREAKER L-8. OPS CHECKED GOOD IAW AMM 33-50-00.
- [SDR 29GA2018032600001](https://openairdocs.org/sdr/29GA2018032600001), Mar 25, 2018: SENSOR. UNKNOWN. NR 2 ENGINE SHUTDOWN DUE TO UNCONTROLLABLE PROPELLER RPM. EMERGENCY LANDING. DOWNLOADED FDR IAW TASK CARD 31-30-10. CHECKED WIRING FOR THE RT ENGINE PROPELLER S
- [SDR 29GA2018031200001](https://openairdocs.org/sdr/29GA2018031200001), Mar 10, 2018: LIGHT. INOPERATIVE. FLIGHT 0093 FLL/EYW REPORT: F/A REPORTS DURING PREFLIGHT EMERGENCY LIGHT SWITCH DOOR INOP. FOUND LIGHT BULB AT FAULT. REPLACED 1 EA EMERGENCY LIGHT SWITCH BULB 
- [SDR 29GA2017103000001](https://openairdocs.org/sdr/29GA2017103000001), Oct 30, 2017: UPLOCK SWITCH. OUT OF LIMITS. IN TRANSIT LIGHT STAYED ON WITH GEAR HANDLE IN THE UP POSITION. INSPECTED AND FOUND THE UPLOCK SWITCH OUT OF LIMITS. ADJUSTED IAW AMM 32-61-15. LUBRICATED THE C
- [SDR 29GA2017080300001](https://openairdocs.org/sdr/29GA2017080300001), Aug 2, 2017: UPLOCK SWITCH. OUT OF ADJUST. FLIGHT 117 FPO/FLL AFTER TAKEOFF TRANSITION HANDLE LIGHT STAY ILLUMINATED TO 800 FEET LANDING GEAR LIGHT ANNUNCIATOR WERE EXTINGUISHED. FOUND NLG UP LOCK SWITCH
- [SDR 29GA2017080200001](https://openairdocs.org/sdr/29GA2017080200001), Aug 1, 2017: WARNING LIGHT. ILLUMINATED. AFTER TAKE OFF, A POSITIVE CLIMB INDICATED, ONLY THE GEAR HANDLE REMAINED ILLUMINATED FROM RETRACTION TO ABOUT 1100 FEET, THEN THE IN-TRANSIT LIGHT EXTINGUISHED
- [SDR 29GA2017073100002](https://openairdocs.org/sdr/29GA2017073100002), Jul 29, 2017: BULB. INOPERATIVE. EMERGECNY LIGHT SWITCH ARM AND ON INDICATORS DO NOT ILLUMINATE. REPLACED EMERGENCY LIGHT SWITCH BULBS, OPERATIONAL CHECKED NORMAL.
- [SDR 29GA2017070600001](https://openairdocs.org/sdr/29GA2017070600001), Jul 5, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT PUSH ON BUTTON AT FLIGHT ATTENDANT STATION NOT ILLUMINATING. REPLACED FLIGHT ATTENDANT EMERGENCY PUSH BUTTON BULB, OPERATIONAL CHECKED GOOD.
- [SDR 29GA2017062100001](https://openairdocs.org/sdr/29GA2017062100001), Jun 20, 2017: POWER SUPPLY. FAILED. FLIGHT 130: EMERGENCY LIGHT FLICKERING ON/OFF SOME NOT COMING ON. R&R POWER SUPPLY 23LN IAW MM 33-50-10-04-01.
- [SDR 29GA2017061100001](https://openairdocs.org/sdr/29GA2017061100001), May 27, 2017: UNKNOWN. MALFUNCTIONED. AIRCRAFT VEERED OFF TAXI WAY AFTER LOSS OF HYD PRESSURE, FOUND DAMAGE FROM FS 839 TO 853.0, WL 104.0 TO 139.0. PERFORMED SHEET METAL REPAIR IAW SDS 043001.
- [SDR 29GA2017053100003](https://openairdocs.org/sdr/29GA2017053100003), May 26, 2017: MOTOR. FAILED. AIRCRAFT VEERED OFF TAXIWAY AFTER LOSS OF HYDRAULIC PRESSURE. R & R THE HYDRAULIC PUMP MOTOR OPS AND LEAK CHECKED GOOD. MAIN HYDRAULIC SYSTEM FUNCTIUONAL CHECKE
- [SDR 29GA2017053000003](https://openairdocs.org/sdr/29GA2017053000003), May 26, 2017: PUMP. WEAK. AIRCRAFT VEERED OFF TAXIWAY AFTER LOSS OF HYDRAULIC PRESSURE. R & R THE HYDRAULIC PUMP MOTOR, OPS AND LEAK CHECKED GOOD. MAIN HYDRAULIC SYSTEM FUNCTIUONAL CHECK
- [SDR 29GA2017032500002](https://openairdocs.org/sdr/29GA2017032500002), Mar 24, 2017: ENGINE. MALFUNCTIONED. FLIGHT 92 FLL. ON TAKEOFF ROLL PUSHED POWER LEVERS TO APPROX 80 ON TORQUE, FO SET POWER OF 90. ROLL WAS NORMAL, ROTATION WAS NORMAL. RIGHT ENGINE STARTED MAKING
- [SDR 29GA2016043000001](https://openairdocs.org/sdr/29GA2016043000001), Apr 29, 2016: SWITCH. MISSING. EMERGENCY LIGHT SWITCH ON F/A PANEL MISSING. R & R EMERGENCY LIGHT SWITCH COVER ON F/A PANEL IAW AMM 25-25-25. OPS CHECKED NORMAL.
- [SDR 29GA2016042200001](https://openairdocs.org/sdr/29GA2016042200001), Apr 21, 2016: SPRING. UNKNOWN. DURING MAINTENANCE, AIR STAIR DOOR GAS SPRING BROKEN. R & R AIR STAIR DOOR GAS SPRING IAW CMM 52-60-01. OPS CHECK GOOD, PN ON & OFF 6-15-32-1-400 113-145AA.
- [SDR 29GA2016021300001](https://openairdocs.org/sdr/29GA2016021300001), Feb 13, 2016: SIGN. LOOSE. F/A NOTICED FORWARD EMERGENCY EXIT SIGN IN CABIN IS COMING OFF. SECURED EXIT SIGN IAW AMM 20-10-00
- [SDR 29GA20161300001](https://openairdocs.org/sdr/29GA20161300001), Feb 13, 2016: SIGN. LOOSE. F/A NOTICED FORWARD EMERGENCY EXIT SIGN IN CABIN IS COMING OFF. SECURED EXIT SIGN IAW AMM 20-10-00.
- [SDR 29GA201601260001](https://openairdocs.org/sdr/29GA201601260001), Jan 20, 2016: WARNING SYSTEM. FALSE INDICATION. TOO LOW FLAPS WARNING ALARMED WITH FLAPS AT 20 DEGREES. WENT AROUND AND FLAPS CAUTION LIGHT ILLUMINATED ON RETRACTION. EMERGENCY DECLARED, FLAPS 0 DEGREE LANDIN
- [SDR 29GA2016011800001](https://openairdocs.org/sdr/29GA2016011800001), Jan 15, 2016: BULB. BURNED OUT. RED EMERGENCY LIGHT ON F/A PANEL DOESN'T COME ON WHEN EMERGENCY BUTTON ON PILOT PANEL TURNED ON. R&R RED EMERGENCY LIGHT BULB ON F/A PANEL IAW AMM 20-10-00, OPS
- [SDR 29GA2015082600001](https://openairdocs.org/sdr/29GA2015082600001), Aug 22, 2015: LAMP. INOPERATIVE. CABIN LIGHTING PANEL EMERGENCY LIGHT SWITCH "ARM" DOESN'T ILLUMINATE. R & R LAMP ON CABIN EMERGENCY LIGHT SWITCH IAW AMM 33-50-00, OPS CHECK NORMAL.
- [SDR 29GA2015052200001](https://openairdocs.org/sdr/29GA2015052200001), May 20, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT INDICATOR ON F/A PANEL IS NOT WORKING. REPLACED EMERGENCY LIGHT INDICATOR BULB ON F/A PANEL, OPS CHECKED GOOD.
- [SDR 29GA2015011100001](https://openairdocs.org/sdr/29GA2015011100001), Jan 11, 2015: INDICATOR. INOPERATIVE. MAIN ACCUMULATOR PRESSURE DROPPED TO ZERO IN FLIGHT. REPLACED MAIN EMERGENCY HYDRAULIC DUAL PRESSURE INDICATOR, OPS CHECKED GOOD.
- [SDR 29GA2014011100001](https://openairdocs.org/sdr/29GA2014011100001), Jan 11, 2015: HYDRAULIC SYSTEM. LOW PRESSURE. TEN MINUTES AFTER DEPARTURE, CREW REPORTED LOW HYDRAULIC ACCUMULATOR PRESSURE. RETURNED TO DEPARTURE LANDED SAFELY.
- [SDR 29GA2014092300002](https://openairdocs.org/sdr/29GA2014092300002), Sep 20, 2014: HANDLE. LACK OF LUBE. CABIN DOOR HANDLE IS VERY HARD TO OPEN . CLEANED DOOR SEAL AND LUBED DOOR MECHANISM.
- [SDR 29GA2014072100002](https://openairdocs.org/sdr/29GA2014072100002), Jul 13, 2014: CHIP DETECTOR. DIRTY. LEFT CHIP DETECTOR INDICATOR ILLUMINATED DURING FLIGHT, AT ALL TIMES NO CHANGES TO ENGINE PARAMETERS. REMOVED AND CLEANED SMALL CARBON DEPOSITS FROM CHIP DETECT
- [SDR 29GA2014070400001](https://openairdocs.org/sdr/29GA2014070400001), Jul 4, 2014: ANNUNCIATOR. MALFUNCTIONED. RIGHT MAIN GEAR ANNUCIATOR DID NOT ILLUMINATE DURING INITIAL APPROACH. PERFORMED GEAR SWINGS, OPS CHECKED GOOD, NO DEFECTS NOTED.
- [SDR 29GA31732020914](https://openairdocs.org/sdr/29GA31732020914), Feb 9, 2014: HANDLE. MALFUNCTIONED. GEAR UNSAFE LIGHT ON FOLLOWED QRH AND LIGHT EXTINGUISHED. GEAR SWINGS EIGHT TIMES, NO DEFECT FOUND. OPS CHECKED GOOD.
- [SDR MALA100126](https://openairdocs.org/sdr/MALA100126), Sep 13, 2010: LAMP. INOPERATIVE. F/A EMERGENCY LIGHT IS INDICATING ON AND NOT SHOWING ARMED ON THE EMERGENCY LIGHTS. RELAMPED F/A ARM/ON BUTTON.
- [SDR MALA100117](https://openairdocs.org/sdr/MALA100117), Aug 25, 2010: SEAT TRACK. CHAFED. DURING HEAVY CHECK, RT FRAME AT BS 630.122 AT OB SEAT TRACK AREA HAS SEVERAL CHAFE'S IN IT. REPAIRED EO S53774.
- [SDR MALA100116](https://openairdocs.org/sdr/MALA100116), Aug 25, 2010: SEAT TRACK. CORRODED. DURING HEAVY CHECK, LT INBD SEAT TRACK WEB AND FLOORBOARD MOUNT ANGLE CORRODED AT STA 294 TO 300. REPAIRED EO S53060.
- [SDR MALA080222](https://openairdocs.org/sdr/MALA080222), Dec 16, 2008: POWER SUPPLY. DISCHARGED. FLOOR PROXIMITY ESCAPE PATH LIGHTS 46LN 47LN 48LN ARE INOP. REPLACED EMERGENCY POWER SUPPLY 24LN IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR MALA080024](https://openairdocs.org/sdr/MALA080024), Feb 10, 2008: SKIN. DENTED. 2 DENTS LOCATED IN LOWER FUSELAGE SKIN AT STA 629, ONE AT EACH FUSELAGE DRAIN. INSTALLED DOUBLER IAW EO NR S53526.
- [SDR MALA070185](https://openairdocs.org/sdr/MALA070185), Nov 24, 2007: INTAKE DUCT. BURNED. AIR RETURN DUE TO A LT LOWER DUCT THAT BURNED AND HAD AN ODOR. REMOVED AND REPLACED IAW JCN NR 7160-301. RAN ENGINE 15 MINUTES, OPS CHECK GOOD, PN ON/OFF: NH246
- [SDR MALA060543](https://openairdocs.org/sdr/MALA060543), Sep 2, 2006: SPAR. CRACKED. THE REAR SPAR OF THE LT FLAP, P/N 7257800-503, S/N 1148, AT WS 142, IS CRACKED IN THE RADIUS OF THE LOWER SPAR CAP ANGLE. THE DAMAGE HAS BEEN REPAIRED IAW MESAB
- [SDR MALA060541](https://openairdocs.org/sdr/MALA060541), Sep 2, 2006: SEAT TRACK. CORRODED. SEAT TRACK AT LBL 18.3, AND FS 630, ON THE INBOARD VERTICAL FLANGE, IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO S53077. REF: EAMS WORK
- [SDR MALA060540](https://openairdocs.org/sdr/MALA060540), Sep 2, 2006: SEAT TRACK. CORRODED. SEAT TRACK AT LBL 18.3, BETWEEN FS 299 AND 317 IS CORRODED OUT OF LIMITS ON THE INBOARD VERTICAL FLANGE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO S53342. REF:
- [SDR MALA060542](https://openairdocs.org/sdr/MALA060542), Sep 2, 2006: SEAT TRACK. CORRODED. SEAT TRACK AT BL 0, FROM FS 630 TO 649, LT VERTICAL FLANGE, IS CORRODED OUT OF LIMITS ON A PREVIOUS REPAIR. THE PREVIOUS REPAIR HAS BEEN REMOVED AND REPLACED IA
- [SDR MALA060344](https://openairdocs.org/sdr/MALA060344), May 19, 2006: SKIN. DAMAGED. RIGHT FLAP SUSTAINED DAMAGE FROM HAIL. TWO DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 3/4 INCH IN DIAMETER AND SKIN WAS PUNCTURED LOCATED 4 3/4 INCH FRO

All 96: https://openairdocs.org/aircraft/N417XJ/reports.md

## 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/N417XJ/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.