# N324EC: 1971 Beech A100, registration cancelled 2018-02-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 8, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Beech A100](https://openairdocs.org/model/beech-a100) (registry code 1152915)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE) (OpenAirDocs)
- Serial number: B-99
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: February 21, 2000
- Certificate issued: August 11, 2007
- Last registry action: April 9, 2012
- Mode S code: A37D93
- Owner when cancelled: [C & M Aviation LLC](https://openairdocs.org/faa-owner/C%20%26%20M%20AVIATION%20LLC)
- Location: [Dewey, OK](https://openairdocs.org/faa-place/OK/Dewey)
- Owner type: Corporation
- Owner's area on the map: 36.8229° N, 95.8899° W: Placed by OpenAirDocs at the center of ZIP code 74029, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N324EC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=324EC
- Page: https://openairdocs.org/deregistered/N324EC-2018-02-08

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 Beech A100: https://openairdocs.org/model/beech-a100.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 324EC200601](https://openairdocs.org/sdr/324EC200601), Jul 6, 2006: RELAY. OPEN. HORIZONTAL STABILIZER TRIM WOULD NOT ACTUATE IN THE NOSE-DOWN TRAVEL DIRECTION (MAIN SYSTEM). STANDBY TRIM SYSTEM FUNCTIONED PROPERLY. FOUND THE MAIN CONTACTS O
- [SDR DIX2005F00000](https://openairdocs.org/sdr/DIX2005F00000), Oct 13, 2005: TURBINE BLADES. ACTIVATED. NR 2 ENGINE EXPERIENCED AN INTERNAL HOT SECTION FAILURE RESULTING IN COMPLETE LOSS OF POWER AND FLAMEOUT. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO THE FAILUR

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