# N935MA: Saab-Fairchild 340A, registration cancelled 2017-02-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 28, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Saab-Fairchild 340A](https://openairdocs.org/model/saab-fairchild-340a) (registry code 7850100)
- 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) (OpenAirDocs)
- Serial number: 340A-073
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 1989
- Certificate issued: March 31, 2010
- Last registry action: March 31, 2010
- Mode S code: ACF950
- Owner when cancelled: [Worthington Aviation Parts Inc](https://openairdocs.org/faa-owner/WORTHINGTON%20AVIATION%20PARTS%20INC)
- Location: [Eagan, MN](https://openairdocs.org/faa-place/MN/Eagan)
- Owner type: Corporation
- Owner's area on the map: 44.8459° N, 93.1596° W: Placed by OpenAirDocs at the center of ZIP code 55121, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N935MA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=935MA
- Page: https://openairdocs.org/deregistered/N935MA-2017-02-28

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Saab-Fairchild 340A: https://openairdocs.org/model/saab-fairchild-340a.md

## Service difficulty reports (12)

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

- [SDR REXA01002](https://openairdocs.org/sdr/REXA01002), Jan 7, 2001: ENGINE. LEAKING. DURING CRUISE FLIGHT FROM MEM TO TRI, AT FL 190, THE L ENG OIL PRESSURE AND MASTER WARNING LIGHTS ILLUMINATED. LEFT ENGINE OIL PRESSURE GAUGE WAS IN THE LOWER Y
- [SDR REXA99012](https://openairdocs.org/sdr/REXA99012), Apr 19, 1999: SWIVEL. BROKEN. HYDRAULIC LEAK RIGHT GEAR BAY. REMOVED AND REPLACED BROKEN DOWNLOCK SWIVEL ON RIGHT MAIN GEAR. (M)
- [SDR REXA98023](https://openairdocs.org/sdr/REXA98023), Jan 21, 1998: SWITCH. DIRTY. LEFT BLEED FAULT LIGHT CAME ON AND STAYED ON. CLEANED LOW AND HI BLEED VALVE, TEMP SWITCH, AND PRESS SWITCH CONNECTORS ON LEFT ENGINE. (M)
- [SDR REXA98020](https://openairdocs.org/sdr/REXA98020), Jan 19, 1998: CONNECTOR. FAILED. NR 2 COMM INOP. REMOVED AND REPLACED CO-AX CABLE CONNECTOR AT NR 2 COM ANTENNA. (M)
- [SDR REXA98003](https://openairdocs.org/sdr/REXA98003), Jan 6, 1998: RADAR R/T. FAILED. RADAR INTERMITTENT, BUT ALSO CYCLED THROUGH ALL RINGS, MODES, EVEN TURN OFF/ON BY ITSELF. REMOVED AND REPLACED RADAR R/T. (X)
- [SDR REXA97187](https://openairdocs.org/sdr/REXA97187), Jul 1, 1997: T4.5 BIAS TRIM. OUT OF ADJUST. TEMPERATURE REACHED 941 DEGREES CELSIUS AT 108 PERCENT TORQUE ON TAKEOFF ROLL. ADJUSTED T4.5 BIAS TRIMMER. (X)
- [SDR REXA97172](https://openairdocs.org/sdr/REXA97172), Jun 19, 1997: ENGINE. MALFUNCTIONED. RETURNED TO RAMP WITH LEFT ENGINE NOT MAKING TORQUE. GROUND RAN BOTH ENGINES COULD NOT DUPLICATE. (M)
- [SDR REXA97077](https://openairdocs.org/sdr/REXA97077), Mar 26, 1997: DOOR LIGHT. ILLUMINATED. CARGO DOOR LIGHT ON IN FLIGHT, DEFERRED. (M)
- [SDR REXA97052](https://openairdocs.org/sdr/REXA97052), Mar 6, 1997: PRE-COOLER. OIL SOAKED. LEFT BLEED AIR PRE-COOLER HAS SMOKE COMING FROM IT. CLEANED LT PRE-COOLER WITH TRYC AND WATER. (M)
- [SDR REXA97046](https://openairdocs.org/sdr/REXA97046), Mar 1, 1997: OIL QTY GAUGE. FAILED. RIGHT OIL CENTRAL WARNING AND GAUGE BOTH READ ZERO. REMOVED AND REPLACED GAUGE AND PRESSURE TRANSDUCER ON RIGHT SIDE. GROUND RAN AND LEAK CHECK GOOD. OIL LEVEL 
- [SDR REXA96077](https://openairdocs.org/sdr/REXA96077), Dec 20, 1996: PUMP. FAILED. HYD PRESSURE DROPPED TO A 1000 PSI AFTER GEAR RETRACTION AND INTRANSIT LIGHT STAYED ILLUMINATED. REOVED AND REPLACED HYD PUMP. (M)
- [SDR REXA96008](https://openairdocs.org/sdr/REXA96008), Feb 18, 1996: HYD SWIVEL. BROKEN. HYDRAULIC 'CAP' AFTER TAKEOFF. HYDRAULIC FLUID 'LOW PRESS' IN MAIN ACCUMULATOR DROPPED. REMOVED AND REPLACED UPLOCK HYDRAULIC SWIVEL, RT IAW AMM 32. NO LEAKS NO

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19920601029429I](https://openairdocs.org/incident/19920601029429I), Jun 1, 1992: Saab SF340A (N935MA), Shreveport, LA. Lost hydraulic power on approach. Used emergency procedures. Landed safely.
- [Incident 19870811048689I](https://openairdocs.org/incident/19870811048689I), Aug 11, 1987: Saab SF340A (N935MA), Wichita, KS. Engine was shut down due to a bleed air leak light.a safe landing was made. The bleed air duct perry seal was worn.

## Other aircraft with N935MA

- [Registered now](https://openairdocs.org/aircraft/N935MA): Virgil E Irwin BEARHAWK MODEL 5, S/N 5001-1M5/2M5-5004, built 2023
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N935MA-undated): Short Bros SD3-30 200, S/N SH3032. Triennial form not returned

---
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.