# N2201F: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 1
- Last cancelled: August 2, 2020
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2201F
- Page: https://openairdocs.org/aircraft/N2201F

## Aircraft that carried N2201F

- [Cancelled 2020-08-02](https://openairdocs.org/deregistered/N2201F-2020-08-02): Johnson Vernon R DOMINATOR, S/N 1, built 2000. Registration expired, pending cancellation. Owner: [Johnson Vernon R](https://openairdocs.org/faa-owner/JOHNSON%20VERNON%20R), [Lakeview, MI](https://openairdocs.org/faa-place/MI/Lakeview)

## NTSB investigations on N2201F (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 MIA96LA076](https://openairdocs.org/ntsb/MIA96LA076), Feb 8, 1996: Cessna 310L (N2201F), Auburn, AL, substantial damage. Probable cause: an overstress failure of the left main gear side brace lock end fitting for undetermined reasons.

## FAA accident and incident reports on N2201F (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 19980810027199I](https://openairdocs.org/incident/19980810027199I), Aug 10, 1998: Cessna 310L (N2201F), Bessemer, AL, Minor damage. Pilot accomplished a no flap crosswind landing at bessener airport. He did not use flaps due to the gusty winds (11 knot gusts by his estimation). The pilot…
- [Accident 19960208001459A](https://openairdocs.org/incident/19960208001459A), Feb 8, 1996: Cessna 310L (N2201F), Auburn, AL, Substantial damage. Left main landing gear failed on landing roll. Side brace lock end fitting had failed from over stress.

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