# N7382B: Beech E35, registration cancelled 2018-03-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 28, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Beech E35](https://openairdocs.org/model/beech-e35) (registry code 1151512)
- Engine: [Continental E225 series](https://openairdocs.org/engine/continental-e225-series) (registry code 17015)
- Data sheets: [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS E-267](https://openairdocs.org/tcds/E-267) (OpenAirDocs)
- Serial number: D-3845
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard
- Airworthiness date: November 11, 1955
- Certificate issued: April 3, 2014
- Last registry action: April 3, 2014
- Mode S code: A9EB63
- Owner when cancelled: [Crossville Aircraft Brokers Inc](https://openairdocs.org/faa-owner/CROSSVILLE%20AIRCRAFT%20BROKERS%20INC)
- Location: [Crossville, TN](https://openairdocs.org/faa-place/TN/Crossville)
- Owner type: Corporation
- Owner's area on the map: 35.8827° N, 84.9800° W: Placed by OpenAirDocs at the center of ZIP code 38555, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N7382B
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7382B
- Page: https://openairdocs.org/deregistered/N7382B-2018-03-28

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 E35: https://openairdocs.org/model/beech-e35.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 20000531SH022](https://openairdocs.org/sdr/20000531SH022), May 4, 2000: CYLINDER. SEPARATED. AT ANNUAL INSPECTION, FOUND SIGNS OF SEEPAGE AT BARREL (INDICATIONS OF BARREL SEPARATING FROM HEAD) IN NR 4, NR 5, NR 6 CYLINDERS. POSSIBLE CAUSE IS AGE ON CYLI
- [SDR 20000531SH020](https://openairdocs.org/sdr/20000531SH020), May 4, 2000: PRIMER LINE. CRACKED. AT CYLINDER REPLACEMENT, FOUND PRIMER LINES NR 1, NR 3 CYLINDERS CRACKED (3/4 AROUND) UNDER ADEL CLAMP AREA. EVIDENCE OF FATIGUE AND CORROSION. (X)

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