# N5479S: Cessna 337B, registration cancelled 1985-03-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 28, 1985
- Status when cancelled: Valid registration
- Airframe: [Cessna 337B](https://openairdocs.org/model/cessna-337b) (registry code 2075706)
- Data sheets: [TCDS A6CE](https://openairdocs.org/tcds/A6CE) (OpenAirDocs)
- Serial number: 3370579
- Type of aircraft: Fixed wing multi engine
- Certificate issued: December 5, 1977
- Mode S code: A6F591
- Owner when cancelled: [Shannon Jerome](https://openairdocs.org/faa-owner/SHANNON%20JEROME)
- Location: [Porland, OR](https://openairdocs.org/faa-place/OR/Porland)
- Owner type: Co-owned
- The mark today: https://openairdocs.org/aircraft/N5479S
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5479S
- Page: https://openairdocs.org/deregistered/N5479S-1985-03-28

From the FAA registry file of November 3, 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 Cessna 337B: https://openairdocs.org/model/cessna-337b.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA83LA130](https://openairdocs.org/ntsb/SEA83LA130), Jun 20, 1983: Cessna 337B (N5479S), Dayton, OR, substantial damage

## 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.

- [Accident 19830620026349A](https://openairdocs.org/incident/19830620026349A), Jun 20, 1983: Cessna 337B (N5479S), Dayton, OR, Substantial damage. Pilot was demonstrating steep descent to passenger and engines would not respond to throttle application.

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