# N231BY: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 2
- Last cancelled: December 17, 2014
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=231BY
- Page: https://openairdocs.org/aircraft/N231BY

## Aircraft that carried N231BY

- [Cancelled 2014-12-17](https://openairdocs.org/deregistered/N231BY-2014-12-17): Beechcraft B200GT, S/N BY-231. Exported to Brazil. Owner: [Beechcraft Corp](https://openairdocs.org/faa-owner/BEECHCRAFT%20CORP), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 2000-02-04](https://openairdocs.org/deregistered/N231BY-2000-02-04): Mooney M20K, S/N 25-0115. Owner: [Application Associates Inc](https://openairdocs.org/faa-owner/APPLICATION%20ASSOCIATES%20INC), [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento)

## NTSB investigations on N231BY (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 LAX98FA154](https://openairdocs.org/ntsb/LAX98FA154), May 5, 1998: Mooney M20K (N231BY), Bakersfield, CA, destroyed, 1 fatal. Probable cause: The pilot's operation of the airplane at a speed well in excess of it's designed never exceed speed that resulted in elevator flutter and in-flight failure of the airplane. Turbulence and icing…

## FAA accident and incident reports on N231BY (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 19980505008399A](https://openairdocs.org/incident/19980505008399A), May 5, 1998: Mooney M20K (N231BY), Bakersfield, CA, Destroyed, 1 fatal. S enroute at 9000FT. Requested vectors to L45. Broke up infligh t during descent. Exceed design loads. (.4) from an examination of the accident site and…

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