# N961BC: 1989 Saab Scania SAAB SCANIA SF340B

- Status: Valid registration
- Airframe: [Saab Scania SAAB SCANIA SF340B](https://openairdocs.org/model/saab-scania-saab-scania-sf340b) (registry code 786010A, 37 seats)
- Engine: [GE CT7-9B](https://openairdocs.org/engine/ge-ct7-9b) (registry code 30148)
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (Saab AB), [TCDS E8NE](https://openairdocs.org/tcds/E8NE) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 340B-223
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 28, 2022
- Certificate issued: July 19, 2022
- Expires: July 31, 2029
- Mode S code: AD5FF9
- 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=961BC
- Page: https://openairdocs.org/aircraft/N961BC

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.

## ADs that may apply (OpenAirDocs): 9 in force

### Matched by airframe (Saab Scania SAAB SCANIA SF340B)

None in force.

### Matched by engine (GE CT7-9B)

- [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 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 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 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 2004-07-09](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 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

### Historical (superseded or no longer in force)

- [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 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

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N961BC.

## FAA accident and incident reports

None matched to N961BC.

## Service difficulty reports (1)

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 OZCA2026042503961](https://openairdocs.org/sdr/OZCA2026042503961), Apr 22, 2026: HAND PUMP. BROKEN. DURING TAKEOFF FROM MBPV, UPON SELECTING THE LANDING GEAR UP, THE CREW RECEIVED A HYD CWP LIGHT AND NO PRESSURE INDICATION. THE CREW ELECTED TO RETURN TO MBPV, 

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Saab Scania SAAB SCANIA SF340B aircraft: https://openairdocs.org/model/saab-scania-saab-scania-sf340b/aircraft.md
- The GE CT7-9B engine: https://openairdocs.org/engine/ge-ct7-9b.md

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