# N362AG: 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: 340B-438
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: May 27, 1998
- Certificate issued: February 14, 2014
- Expires: February 28, 2030
- Mode S code: A413C1
- Registered owner: [Jahn362ag LLC](https://openairdocs.org/faa-owner/JAHN362AG%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: LLC
- Owner's area on the map: 25.7304° N, 80.2336° W: Placed by OpenAirDocs at the center of ZIP code 33133, 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=362AG
- Page: https://openairdocs.org/aircraft/N362AG

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/N362AG/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 N362AG.

## FAA accident and incident reports

None matched to N362AG.

## Service difficulty reports (37)

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

- [SDR 4EZF202510210001](https://openairdocs.org/sdr/4EZF202510210001), Oct 21, 2025: NONE. NO DISCREPANCY. BIRD STRIKE (DURING LANDING AT TNCC) - MTX ACTION: PERFORMED INSPECTION OF THE FUSELAGE IN ACCORDANCE WITH SRM 51-10-00-001 NO DAMAGE FOUND. AIRCRAFT WAS RELEAS
- [SDR 4EZF20261014362AG](https://openairdocs.org/sdr/4EZF20261014362AG), Oct 14, 2025: COMMS UNIT. STUCK. COMM 1 STUCK IN TRANSIT, PERFORMED AN OPERATIONAL TEST OF THE SYSTEM IAW AMM 23-30-00-05 OPERATIONAL TEST SATISFACTORY ON GROUND.
- [SDR 4EZF202407030001](https://openairdocs.org/sdr/4EZF202407030001), Jun 27, 2024: ACM. DEFECTIVE. COCKPIT AIRCO BLOWS HOT AIR UNABLE TO COOL COCKPIT, ACCOMPLISHED TROUBLESHOOTING IAW AMM 21-60-00-01 WAS FOUND AIR CYCLE MACHINE OIL WAS BLACK AND ACM BLOWS HOT
- [SDR 29GA2022052300002](https://openairdocs.org/sdr/29GA2022052300002), May 20, 2022: NONE. INOPERATIVE. SUPPLEMENTAL FLIGHT: 127 SKB/SJU FLOOR PROXIMITY EMERGENCY LIGHT 42 LN INTERMITTENT ALSO EMERGENCY ESCAPE AND PATH MARLING LIGHT. CORRECTIVE ACTION: REPLACED EM
- [SDR 29GA2022052300001](https://openairdocs.org/sdr/29GA2022052300001), May 20, 2022: NONE. INOPERATIVE. FLIGHT: 127 SKB/SJU MAIN CABIN DOOR AND RIGHT EMERGENCY DOOR EMERGENCY LIGHTS INOPERATIVE REPORTED BY THE FLIGHT ATTENDANT. CORRECTIVE ACTION: INSPECTED TROUBLE
- [SDR 29GA2022030100001](https://openairdocs.org/sdr/29GA2022030100001), Feb 25, 2022: BOLT. UNKNOWN. FLIGHT 127 SKB/SJU WHEN SELECED GEAR DOWN WE EXPERIENCED NOISE AND DELAY TO DROP ALL THREE GEARS AND FINALLY WE GOT THREE GREEN LIGHTS DOWN AND LOCKED. CORRECTI
- [SDR 29GA2022011000002](https://openairdocs.org/sdr/29GA2022011000002), Jan 10, 2022: LIGHT. INOPERATIVE. REPORT: EMERGENCY LIGHT NOT WORKING FROM CABIN. CORRECTIVE ACTION: REPLACED LEFT EMERGENCY LIGHT STRIP
- [SDR 29GA0222011000001](https://openairdocs.org/sdr/29GA0222011000001), Jan 9, 2022: LANDING GEAR. FAULTY. 100 EIS/SJU DURING GEAR EXTENSION THE INTRANSIT LIGHT DID NOT COME ON. CORRECTIVE ACTION: REPLACED LANDING GEAR CONTROL, OPERATIONAL CHECK GOOD.
- [SDR 29GA2022011000001](https://openairdocs.org/sdr/29GA2022011000001), Jan 9, 2022: INDICATOR. NO INDICATION. FLIGHT: 100 EIS/SJU DURING GEAR EXTENSION THE INTRANSIT LIGHT DID NOT COME ON. CORRECTIVE ACTION: OPEN
- [SDR 29GA2020032300001](https://openairdocs.org/sdr/29GA2020032300001), Mar 22, 2020: UPLOCK SWITCH. FAULTY. SUPPLEMENTAL FLIGHT# 0094 FLL/EYW REPORT: GEAR TRANSIT LIGHT DOES NOT EXTINGUISH DURING RETRACTION. PERFORMED QRH 10-3 AND LIGHT DID NOT EXTINGUISH. EXTENDED GE
- [SDR 29GA2020030300001](https://openairdocs.org/sdr/29GA2020030300001), Mar 2, 2020: DOWNLOCK SWITCH. DIRTY. SUPPLEMENTAL FLIGHT# 0085 FLL/EYW REPORT: RIGHT MAIN GEAR INDICATION DID NOT ILLUMINATE ON 1ST ATTEMPT. RAN QRH RECYCLED GEAR GOT AURAL INDICATE 3 GREEN. CORREC
- [SDR 29GA2019110700001](https://openairdocs.org/sdr/29GA2019110700001), Nov 6, 2019: UNKNOWN. MALFUNCTIONED. FLIGHT 0061, ENGINE INDICATION IRRATIC FOLLOWED BY A LOUD BANG RAN QRH WITH OVERTEMP, CREW SHUT DOWN 1 ENGINE. PERFORMED DFDR DOWNLOAD AND BORESCOPE OF LH HOT A
- [SDR 29GA2019051300001](https://openairdocs.org/sdr/29GA2019051300001), May 10, 2019: UNKNOWN. ODOR. FLIGHT 0072 FLL/GGT: REPORT: BURNING SMELL IN COCKPIT & CABIN. AND VERY WEAK AIRFLOW. CORRECTIVE ACTION: PERFORMED BOTH ENGINE RUN REF AMM 72-00-00. INSPECTED A
- [SDR 29GA2019030700002](https://openairdocs.org/sdr/29GA2019030700002), Mar 6, 2019: SIGN. WORN. FLIGHT 7012 SJU/STX REPORT: EMERGENCY EXIT SIGN OVER FA SEAT RIGHT ARROW WORN. CORRECTIVE ACTION: REPLACED EMERGENCY EXIT SIGN OVER FA SEAT.
- [SDR 29GA2018121800001](https://openairdocs.org/sdr/29GA2018121800001), Dec 17, 2018: HUB CAP. BROKEN. FLIGHT# 7016 STX/SJU REPORT: LOSS BRAKES WHILE TAXIING TO THE GATE ON BOTH SIDES (CA&FO) CORRECTIVE ACTION: SLAVED IN ANTI-SKID CONTROL BOX IAW AMM 32-43-05-04.
- [SDR 29GA2018121700001](https://openairdocs.org/sdr/29GA2018121700001), Dec 16, 2018: SWIVEL. LOOSE. FLIGHT# 7016 SJU/STT REPORT: LOSS BRAKES WHILE TAXIING TO THE GATE. CORRECTIVE ACTION: DISCOVERED LH BRAKE SWIVEL ON THE MAIN LANDING GEAR TO BE LOOSE. ADJUSTED
- [SDR 29GA2018120700001](https://openairdocs.org/sdr/29GA2018120700001), Dec 7, 2018: CONTROL VALVE. FAILED. FLIGHT# 7004 SJU/STT REPORT: WHEN WE TRY TO STOP THE AIRPLANE THE PIC BRAKE DID NOT WORK NEITHER THE SIC BRAKES. THIS HAPPEN AT THE GATE. CORRECTIVE ACTION: REM
- [SDR 29GA2018121000002](https://openairdocs.org/sdr/29GA2018121000002), Dec 7, 2018: CONTROL VALVE. FAILED. FLIGHT# 7004 SJU/STT REPORT: WHEN WE TRY TO STOP THE AIRPLANE THE PIC BRAKE DID NOT WORK NEITHER THE SIC BRAKES. THIS HAPPEN AT THE GATE. CORRECTIVE ACTION: REM
- [SDR 29GA2018102500001](https://openairdocs.org/sdr/29GA2018102500001), Oct 24, 2018: FLAP. OUT OF ADJUST. FLIGHT 0117 FLL/FPO REPORT: F/A REPORTS MAIN CABIN DOOR NOT CLOSING SMOOTHLY AND FLAP GET STUCK WHILE DOOR TRAVEL FOR CLOSURE. CORRECTIVE ACTION: ADJUSTED THE D
- [SDR 29GA2018102200001](https://openairdocs.org/sdr/29GA2018102200001), Oct 19, 2018: SIGN. BROKEN. FLIGHT 0118 MCO/FLL REPORT: EMERGENCY EXIT SIGN ABOVE AIRSTAIR DOOR BROKE. CORRECTIVE ACTION: R&R EMERGENCY EXIT SIGN ABOVE AIRSTAIRS DOOR IAW AMM 20-00-00,
- [SDR 29GA2018101900002](https://openairdocs.org/sdr/29GA2018101900002), Oct 19, 2018: WIRE. DISCONNECTED. FLIGHT 0118 MCO/FLL REPORT: F/A EMERGENCY LIGHTING SYSTEM DOES NOT TEST. RE-SOLDER WIRE ON F/A EMERGENCY SWITCH IAW AMM WM 20-20-00, OPS CHECK GOOD IAW AMM 33-5
- [SDR 29GA2018101600001](https://openairdocs.org/sdr/29GA2018101600001), Oct 13, 2018: CONNECTOR. NOT SEATED. FLIGHT 0053 MCO/MCO REPORT: LT GEAR WILL NOT COME UP FI STOP OPEN ILLUMINATED. CORRECTIVE ACTION: FOUND LT GEAR WOW CONNECTOR 5GA P1 NOT FULLY SECURED IN ITS PO
- [SDR 29GA2018071900001](https://openairdocs.org/sdr/29GA2018071900001), Jul 18, 2018: UNKNOWN. ODOR. FLIGHT 0076 FLL/GGT REPORT: DURING PASSENGER BOARDING AND AFTER SEATING F/A WENT THROUGH THE AISLE PAX 7A REPORTED PLASTIC ELECTRIC BURNT ODOR ALSO PASSENGER SE
- [SDR 29GA2018020200001](https://openairdocs.org/sdr/29GA2018020200001), Feb 1, 2018: LOCK. DIRTY. FLL/ELH REPORT: AIRSTAIR DOORS WILL NOT LOCK IN STOWED POSITION. CLEANED AND LUBED AIRSTAIR DOOR LOCK IAW CMM 52-60-01. OPS CHECK GOOD.
- [SDR 29GA2017112900001](https://openairdocs.org/sdr/29GA2017112900001), Nov 29, 2017: LIGHT. MALFUNCTIONED. GEAR HANDLE LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED UP. PREFORMED GEAR EXTENTION AND RETRACTIONS MULTIPLE TIMES, NO DEFECT NOTED IAW AMM 32-30-00-05. COMP
- [SDR 29GA2017101600002](https://openairdocs.org/sdr/29GA2017101600002), Oct 14, 2017: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS, SEATS 8A TO 12A INOPERATIVE, AND TWO EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY, OPS CHECKED GOOD.
- [SDR 29GA2017092300001](https://openairdocs.org/sdr/29GA2017092300001), Sep 22, 2017: UPLOCK SWITCH. OUT OF ADJUST. FLIGHT 9004 TLH-MCO, GEAR INTRANSIT LIGHT STAYED ON WHILE GEAR HANDLE WAS IN THE UP POSITION. ADJUSTED NLG UPLOCK SWITCH IAW AMM 32-61-15-02, OPS CHECK GOOD.
- [SDR 29GA2017061700001](https://openairdocs.org/sdr/29GA2017061700001), Jun 15, 2017: LANDING GEAR. MALFUNCTIONED. GEAR EXTENSION WAS ABORMALLY LONG, CAME DOWN AFTER LEVEL OFF, POPPING SOUND, THEN 3 GREEN LIGHTS. HYDRAULIC PUMP RAN AND LEVELS OK. JR 5193 PERFORMED ADJUSTMENT
- [SDR 29GA2017010300001](https://openairdocs.org/sdr/29GA2017010300001), Jan 2, 2017: GCU. FAILED. DURING FLIGHT, LT MAIN BUSS, LT ESS BUSS, AND INVERT LIGHT ILLUMINATED. ALL CAPTAIN SIDE INSTRUMENTS INOPERATIVE. RAN QRH AND L MAIN BUSS, AND LESS BUSS WERE ST
- [SDR 29GA2016020600002](https://openairdocs.org/sdr/29GA2016020600002), Feb 3, 2016: SWITCH. FAILED. EMERGENCY ARM LIGHT ON F/A PANEL NOT WORKING. R & R F/A EMERGENCY ARM SWITCH IAW AMM 39-40-65-04,OPS CHECK GOOD IAW AMM 35-50-00-05.
- [SDR 29GA2015112600002](https://openairdocs.org/sdr/29GA2015112600002), Nov 25, 2015: BRACE. LOOSE. F/A UNABLE TO CLOSE AIRSTAIR DOOR, DOOR BRACES CAME LOOSE BOTH SIDES. RESECURED PLUNGER INTO EXTENSION BRACKET AS REQUIRED. OPS CHECK GOOD.
- [SDR 29GA2015112600001](https://openairdocs.org/sdr/29GA2015112600001), Nov 25, 2015: BRACE. SEPARATED. F/A REPORTS AIR STAIR DOOR BRACE SEPARATED, UNABLE TO CLOSE THE DOOR. RE-INSERTED PLUNGER INTO EXTENSION BRACES AS REQUIRED, OPS CHECK GOOD.
- [SDR 29GA2015062300003](https://openairdocs.org/sdr/29GA2015062300003), Jun 21, 2015: LAMP. INOPERATIVE. F/A'S EMERGENCY LIGHT SWITCH DOES NOT LIGHT UP ARM WHEN THE LIGHTS ARE ARMED. REPLACED LAMP AT F/A'S EMERGENCY LIGHT ARM SWITCH OPS CHECK NORMAL.
- [SDR 29GA2015012200001](https://openairdocs.org/sdr/29GA2015012200001), Jan 22, 2015: LINE. DAMAGED. HYDRAULIC LIGHT ILLUMINATED IN FLIGHT. REPLACED DAMAGED SECTION OF MLG UPLOCK SUPPLY LINE LEAK CHECK GOOD.
- [SDR 29GA2014080600001](https://openairdocs.org/sdr/29GA2014080600001), Aug 2, 2014: DOOR. LACK OF LUBE. MAIN DOOR HARD TO OPEN AND CLOSE. CLEANED AND LUBED MAIN DOOR, OPS CHECKED GOOD.
- [SDR 29GA36232012914](https://openairdocs.org/sdr/29GA36232012914), Jan 29, 2014: CONTROL HANDLE. MALFUNCTIONED. GEAR TRANSIT LIGHT STAYED ILLUMINATED AFTER TAKEOFF, HYDRAULIC PUMP ALSO REMAINED ON. REPLACED LANDING GEAR CONTROL HANDLE GEAR SWINGS, OPERATIONAL CHECKS GOOD.
- [SDR 29GA2014012236232](https://openairdocs.org/sdr/29GA2014012236232), Jan 22, 2014: UPLOCK SWITCH. DIRTY. GEAR INTRANSIT LIGHT ILLUMINATED RECYCLED GEAR AND INTRANSIT LIGHT WOULD NOT EXTINGUISH ALL OTHER INDICATIONS NORMAL. PERFORMED GEAR SWINGS 5 TIMES WITH NO FAUL

## 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/N362AG/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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