# N5285: 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: September 12, 2006
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5285
- Page: https://openairdocs.org/aircraft/N5285

## Aircraft that carried N5285

- [Cancelled 2006-09-12](https://openairdocs.org/deregistered/N5285-2006-09-12): Grumman G-164A, S/N 565, built 1968. Exported to Philippines. Owner: [Clifford Eric S](https://openairdocs.org/faa-owner/CLIFFORD%20ERIC%20S), [Paris, TX](https://openairdocs.org/faa-place/TX/Paris)

## NTSB investigations on N5285 (3)

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 SEA87LA121](https://openairdocs.org/ntsb/SEA87LA121), Jun 24, 1987: Grumman G-164A (N5285), Viola, ID, substantial damage
- [NTSB SEA85LA098](https://openairdocs.org/ntsb/SEA85LA098), Apr 26, 1985: Grumman G-164A (N5285), Kendrick, ID, substantial damage
- [NTSB DEN69F0161](https://openairdocs.org/ntsb/DEN69F0161), Jan 6, 1969: Grumman G-164A (N5285), Snowville, UT, substantial damage

## FAA accident and incident reports on N5285 (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.

- [Accident 19870623026429A](https://openairdocs.org/incident/19870623026429A), Jun 23, 1987: Scwzer G164 (N5285), Viola, ID, Substantial damage. Engine quit. Forced landing. Left gear torn off on impact with ground. Flipped over. Supercharger impeller failed.
- [Accident 19850426015089A](https://openairdocs.org/incident/19850426015089A), Apr 26, 1985: Scwzer G164A (N5285), Kendrick, ID, Substantial damage. The left main gear collapsed on landing. Overstress caused by a hard landing or side load on gear.

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