# N6603C: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 3
- Last cancelled: December 15, 1999
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=6603C
- Page: https://openairdocs.org/aircraft/N6603C

## Aircraft that carried N6603C

- [Cancelled 1999-12-15](https://openairdocs.org/deregistered/N6603C-1999-12-15): Bell 412, S/N 36011. Exported to Mexico. Owner: [Bell Helicopter Textron Inc](https://openairdocs.org/faa-owner/BELL%20HELICOPTER%20TEXTRON%20INC), [Ft Worth, TX](https://openairdocs.org/faa-place/TX/Ft%20Worth)
- [Cancelled 1970-07-13](https://openairdocs.org/deregistered/N6603C-1970-07-13): Ryan NAVION A, S/N NAV4-1772. Owner: [United States Army](https://openairdocs.org/faa-owner/UNITED%20STATES%20ARMY), [Fort Lewis, WA](https://openairdocs.org/faa-place/WA/Fort%20Lewis)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N6603C-undated): Cessna 210N, S/N 21063927. N-number assigned, not yet registered

## NTSB investigations on N6603C (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 MIA86LA180](https://openairdocs.org/ntsb/MIA86LA180), Jun 12, 1986: Cessna 210N (N6603C), Jacksonville, FL, substantial damage

## FAA accident and incident reports on N6603C (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 19860612070589A](https://openairdocs.org/incident/19860612070589A), Jun 12, 1986: Cessna T210N (N6603C), Jacksonville, FL, Substantial damage. Engine failed inflight. Pilot landed plane in an open field. No cause for the power loss could be determined.

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