# N840MA: 1974 Mitsubishi MU-2B-35, registration cancelled 2009-09-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 21, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Mitsubishi MU-2B-35](https://openairdocs.org/model/mitsubishi-mu-2b-35) (registry code 5780411)
- Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514)
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC) (OpenAirDocs)
- Serial number: 612
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: June 12, 1998
- Certificate issued: August 30, 2002
- Last registry action: August 19, 2008
- Mode S code: AB80ED
- Owner when cancelled: [Air 1st Aviation Companies Inc](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20COMPANIES%20INC)
- Location: [Aiken, SC](https://openairdocs.org/faa-place/SC/Aiken)
- Owner type: Corporation
- Owner's area on the map: 33.6419° N, 81.6141° W: Placed by OpenAirDocs at the center of ZIP code 29805, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N840MA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=840MA
- Page: https://openairdocs.org/deregistered/N840MA-2009-09-21

From the FAA registry file of November 5, 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 Mitsubishi MU-2B-35: https://openairdocs.org/model/mitsubishi-mu-2b-35.md

## Service difficulty reports (2)

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

- [SDR HMN2002F00002](https://openairdocs.org/sdr/HMN2002F00002), May 30, 2002: CONTROL CABLE. FRAYED. FRAYED THROTTLE CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED.
- [SDR 2002FA0000749](https://openairdocs.org/sdr/2002FA0000749), Mar 26, 2002: CONTROL CABLE. FRAYED. DURING ROUTINE MAINTENANCE FOUND A FRAYED ENGINE CONTROL CABLE. THE FRAYED PORTION WAS LOCATED IN THE AFT FUSELAGE WHERE THE CABE GOES OVER A 90DEGREE TURN PULL

## Other aircraft with N840MA

- [Registered now](https://openairdocs.org/aircraft/N840MA): Cessna 208B, S/N 208B2423, built 2013

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