# N105AE: Bell Helicopter Textron 206L-1, registration cancelled 2019-04-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 26, 2019
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Bell Helicopter Textron 206L-1](https://openairdocs.org/model/bell-helicopter-textron-206l-1) (registry code 1182107)
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (OpenAirDocs)
- Serial number: 45297
- Type of aircraft: Rotorcraft
- Airworthiness: Standard, normal
- Airworthiness date: August 31, 1974
- Certificate issued: November 1, 2005
- Last registry action: June 15, 2018
- Mode S code: A0174C
- 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/N105AE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=105AE
- Page: https://openairdocs.org/deregistered/N105AE-2019-04-26

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 (3)

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

- [SDR EVCA201701281](https://openairdocs.org/sdr/EVCA201701281), Jan 28, 2017: MOUNT. DAMAGED. FOUND RIGHT HAND MID ENGINE MOUNT HOLE TO BE ELONGATED MEASURING .280/.286" WHEN NOMINAL HOLE SIZE IS .247/.251". THIS ABNORMAL ELONGATION OF THE HOLE RESULTED 
- [SDR EVCA20160623161](https://openairdocs.org/sdr/EVCA20160623161), Jun 23, 2016: WEB. CRACKED. DURING 300 HR PERIOD INSPECTION, FOUND RT VERTICAL TUNNEL WEBBING, PN: 206-033-110-183, CRACKED NEAR TOP OF PANEL NEAR INTERFACE WITH THE BOX BEAM.
- [SDR EVCA2014082900070](https://openairdocs.org/sdr/EVCA2014082900070), Aug 29, 2014: ATTACH FITTING. CRACKED. DURING ROUTINE INSPECTION FOUND TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001 CRACKED.

## Other aircraft with N105AE

- [Registered now](https://openairdocs.org/aircraft/N105AE): BRM Aero S R O BRISTELL LSA, S/N 874/2026

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