# N711FM: 1956 Beech C-50, registration cancelled 2004-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2004
- Exported to: Venezuela
- Status when cancelled: Sale reported
- Airframe: [Beech C-50](https://openairdocs.org/model/beech-c-50) (registry code 1152510)
- Engine: [Lycoming GSO&IGSO-480 series](https://openairdocs.org/engine/lycoming-gso-igso-480-series) (registry code 41529)
- Data sheets: [TCDS 5A4](https://openairdocs.org/tcds/5A4), [TCDS E-284](https://openairdocs.org/tcds/E-284) (OpenAirDocs)
- Serial number: CH-137
- Year built: 1956
- Type of aircraft: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard
- Last registry action: January 14, 1977
- Mode S code: A9804D
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Corporation
- Owner's area on the map: 35.4676° N, 97.5164° W: Placed by OpenAirDocs: center of Oklahoma City, OK, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N711FM
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=711FM
- Page: https://openairdocs.org/deregistered/N711FM-2004-02-12

From the FAA registry file of October 31, 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 Beech C-50: https://openairdocs.org/model/beech-c-50.md

## FAA accident and incident reports (1)

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 19981208045839I](https://openairdocs.org/incident/19981208045839I), Dec 8, 1998: Beech C50 (N711FM), Guam, Guam, Minor damage. The failure of the gear to extend was attributed to the left main landing gear drag brace assembly and shock absorber. The parts were examined by the…

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