# N6517R: 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: November 23, 1990
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6517R
- Page: https://openairdocs.org/aircraft/N6517R

## Aircraft that carried N6517R

- [Cancelled 1990-11-23](https://openairdocs.org/deregistered/N6517R-1990-11-23): Bell 206L-3, S/N 51410. Exported to Germany. Owner: [Helicopter Aviation Services Corporation](https://openairdocs.org/faa-owner/HELICOPTER%20AVIATION%20SERVICES%20CORPORATION), [Mount Pleasant, PA](https://openairdocs.org/faa-place/PA/Mount%20Pleasant)
- [Cancelled 1989-08-23](https://openairdocs.org/deregistered/N6517R-1989-08-23): Beech B19, S/N MB709. Triennial form not returned

## NTSB investigations on N6517R (2)

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 CHI86LA190](https://openairdocs.org/ntsb/CHI86LA190), Jul 30, 1986: Beech B-19 (N6517R), Manchester, MI, substantial damage
- [NTSB DEN76FTE21](https://openairdocs.org/ntsb/DEN76FTE21), Aug 27, 1975: Beech B19 (N6517R), Broomfield, CO, substantial damage

## FAA accident and incident reports on N6517R (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 19860730036629A](https://openairdocs.org/incident/19860730036629A), Jul 30, 1986: Beech B19 (N6517R), Manchester, MI, Substantial damage. The aircraft ballooned and landed hard. Student pilot.
- [Accident 19750827026229A](https://openairdocs.org/incident/19750827026229A), Aug 27, 1975: Beech B19 (N6517R), Broomfield, CO, Substantial damage. Max gust 38KT.acft encountered wind shear 200FT AGL and descended to grnd level lower than arpt.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.