# N139AE: 1980 Bell Helicopter Textron 206L-1, registration cancelled 2021-10-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 30, 2021
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Bell Helicopter Textron 206L-1](https://openairdocs.org/model/bell-helicopter-textron-206l-1) (registry code 1182107)
- Engine: [Allison 250 SER 250HP](https://openairdocs.org/engine/allison-250-ser-250hp) (registry code 03002)
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (OpenAirDocs)
- Serial number: 45546
- Year built: 1980
- Type of aircraft: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: October 31, 1980
- Certificate issued: October 26, 2005
- Last registry action: March 16, 2018
- Mode S code: A09CA5
- Owner when cancelled: [Air Evac Ems Inc](https://openairdocs.org/faa-owner/AIR%20EVAC%20EMS%20INC)
- Location: [O Fallon, MO](https://openairdocs.org/faa-place/MO/O%20Fallon)
- Owner type: Corporation
- Owner's area on the map: 38.7515° N, 90.7284° W: Placed by OpenAirDocs at the center of ZIP code 63368, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N139AE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=139AE
- Page: https://openairdocs.org/deregistered/N139AE-2021-10-30

From the FAA registry file of November 5, 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 Bell Helicopter Textron 206L-1: https://openairdocs.org/model/bell-helicopter-textron-206l-1.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 2010F00055](https://openairdocs.org/sdr/2010F00055), Mar 2, 2010: SUPPORT. CRACKED. RADIAL CRACK WAS DISCOVERED IN THE BASE OF THE UNIT AT THE RELIEF HOLE. CRACK IS APPROX .25" LONG. THIS SUPPORT ATTACHES THE PILOT'S YOKE TO THE FLOOR OF THE AC

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