# N6569Y: 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: May 25, 1995
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6569Y
- Page: https://openairdocs.org/aircraft/N6569Y

## Aircraft that carried N6569Y

- [Cancelled 1995-05-25](https://openairdocs.org/deregistered/N6569Y-1995-05-25): Piper PA-23-250, S/N 273866. Triennial form not returned. Owner: [Business Air Inc](https://openairdocs.org/faa-owner/BUSINESS%20AIR%20INC), [Nashville, TN](https://openairdocs.org/faa-place/TN/Nashville)

## FAA accident and incident reports on N6569Y (5)

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 19800725082069I](https://openairdocs.org/incident/19800725082069I), Jul 25, 1980: Piper PA23250 (N6569Y), Albany, NY, Minor damage. After starting the engine, and while preoccupied in the cockpit the aircraft crept forward into another airplane.
- [Incident 19791016052099I](https://openairdocs.org/incident/19791016052099I), Oct 16, 1979: Piper PA23250 (N6569Y), Islip, NY. Gear unsafe indication due to faulty microswitch.
- [Incident 19790412014089I](https://openairdocs.org/incident/19790412014089I), Apr 12, 1979: Piper PA23250 (N6569Y), Albany, NY. Immovable trim tab due to binding from a broken deice boot pressure line clamp.
- [Incident 19790226007719I](https://openairdocs.org/incident/19790226007719I), Feb 26, 1979: Piper PA23250 (N6569Y), Albany, NY. Lost all navcom. Broken ground wire on alternator. Pilot not aware of auxillary regulator system.
- [Incident 19781030027859I](https://openairdocs.org/incident/19781030027859I), Oct 30, 1978: Piper PA23250 (N6569Y), Albany, NY, Minor damage. Prop spinner came apart, punched holes in the fuselage. Crack existed prior to failure.

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