# N623CQ: 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: March 12, 2009
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=623CQ
- Page: https://openairdocs.org/aircraft/N623CQ

## Aircraft that carried N623CQ

- [Cancelled 2009-03-12](https://openairdocs.org/deregistered/N623CQ-2009-03-12): Beech A36, S/N E-1382, built 1978. Triennial form not returned. Owner: [C & S Aviation Inc](https://openairdocs.org/faa-owner/C%20%26%20S%20AVIATION%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)

## NTSB investigations on N623CQ (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 NYC08LA112](https://openairdocs.org/ntsb/NYC08LA112), Feb 26, 2008: Beech A36 (N623CQ), Athens, GA, substantial damage. Probable cause: The loss of propeller thrust due to the unseating of an internal propeller hub bushing. Contributing to the accident was the manufacturer's inadequate procedure to secure the bushing.

## FAA accident and incident reports on N623CQ (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 20080226836369A](https://openairdocs.org/incident/20080226836369A), Feb 26, 2008: Beech A36 (N623CQ), Colbert, GA, Substantial damage. (-23) Propeller tear down analysis revealed that the rear bushing, through which the propeller pitch control rod passed, which is part of a rear hub assembly…
- [Incident 19800823080969I](https://openairdocs.org/incident/19800823080969I), Aug 23, 1980: Beech A36 (N623CQ), Chatham, MA, Minor damage. Electrical system failure due to corroded battery lead. Pilot did not use emergency procedure to extend gear.

---
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.