# N21CJ: 1980 Mitsubishi MU-2B-60, registration cancelled 2018-01-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 24, 2018
- Status when cancelled: First renewal notice
- Airframe: [Mitsubishi MU-2B-60](https://openairdocs.org/model/mitsubishi-mu-2b-60) (registry code 5780460)
- Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514)
- Data sheets: [TCDS A10SW](https://openairdocs.org/tcds/A10SW) (OpenAirDocs)
- Serial number: 789 S.A.
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Experimental, showing compliance
- Airworthiness date: January 12, 1981
- Certificate issued: May 14, 2015
- Last registry action: May 14, 2015
- Mode S code: A1B764
- Owner when cancelled: [Air 1st Aviation Companies Inc](https://openairdocs.org/faa-owner/AIR%201ST%20AVIATION%20COMPANIES%20INC)
- Location: [Aiken, SC](https://openairdocs.org/faa-place/SC/Aiken)
- Owner type: Corporation
- Owner's area on the map: 33.6419° N, 81.6141° W: Placed by OpenAirDocs at the center of ZIP code 29805, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N21CJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=21CJ
- Page: https://openairdocs.org/deregistered/N21CJ-2018-01-24

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mitsubishi MU-2B-60: https://openairdocs.org/model/mitsubishi-mu-2b-60.md

## Service difficulty reports (2)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 97ZZZX4894](https://openairdocs.org/sdr/97ZZZX4894), Oct 29, 1997: CLAMP. CRACKED. INSPECTION REPORT CONDUCTED BY HARTZELL PROPELLER INC., REVEALED CRACK IN PROPELLER BLADE CLAMP. SUSPECT CAUSE OF CRACK DUE TO FATIGUE.
- [SDR 97ZZZX4893](https://openairdocs.org/sdr/97ZZZX4893), Oct 29, 1997: CLAMP. CRACKED. INSPECTION REPORT CONDUCTED BY HARTZELL PROPELLER INC., REVEALED CRACK IN PROPELLER BLADE CLAMP. SUSPECT CAUSE OF CRACK DUE TO FATIGUE.

## FAA accident and incident reports (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.

- [Incident 20030307008919I](https://openairdocs.org/incident/20030307008919I), Mar 7, 2003: Mtsbsi MU2B60 (N21CJ), Quincy, FL, Minor damage. (-23) On March 7, 2003, at 1300 local time, a mitsubishi MU-2-60, N21CJ, registered to bankair inc, landed gear up at Quincy airport, Quincy Florida while on a…

## Other aircraft with N21CJ

- [Registered now](https://openairdocs.org/aircraft/N21CJ): Corey Jones RANS S21 OUTBOUND, S/N 11220301, built 2025

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