# N530CH: 1992 Beech C90A, registration cancelled 2021-08-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 11, 2021
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Beech C90A](https://openairdocs.org/model/beech-c90a) (registry code 1152911)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20) (OpenAirDocs)
- Serial number: LJ-1322
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: December 21, 1992
- Certificate issued: July 14, 2021
- Last registry action: July 14, 2021
- Mode S code: A6B0A7
- Owner when cancelled: [Kenmore Crew Leasing Inc Trustee](https://openairdocs.org/faa-owner/KENMORE%20CREW%20LEASING%20INC%20TRUSTEE)
- Location: [Bellingham, WA](https://openairdocs.org/faa-place/WA/Bellingham)
- Owner type: Corporation
- Owner's area on the map: 48.7973° N, 122.4315° W: Placed by OpenAirDocs at the center of ZIP code 98226, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N530CH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=530CH
- Page: https://openairdocs.org/deregistered/N530CH-2021-08-11

From the FAA registry file of November 12, 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 Beech C90A: https://openairdocs.org/model/beech-c90a.md

## Service difficulty reports (1)

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

- [SDR 2006FA0000567](https://openairdocs.org/sdr/2006FA0000567), Jun 1, 2006: BEARING. FAILED. THE BEARING IN FUEL CONTROL UNIT FAILED CAUSING THE LT ENGINE TO SURGE AND EXCEED THE N1, ITT AND TORQUE LIMITS. THE ITT EXCEEDED 1000 C AND THE TORQUE EXCEEDED

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