# STC SR00513AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bell Helicopter Textron Inc., United States
- Description: Installation of tail rotor pedal lockout.
- Applied: September 13, 1993
- Status date: October 17, 2012
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/aa/e5/aae58724fb8087d5d442eaeea0e42526397f11754c77df25b58e81a483d6ac03
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/57561A93975D651C86257AD1005ADEBE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00513AT

## ADs that name it (0)

None.

## Approved models (7)

- Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## What the certificate says

The certificate has no text we could read; open the PDF to read it.

## Every issue (1)

- October 17, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/aa/e5/aae58724fb8087d5d442eaeea0e42526397f11754c77df25b58e81a483d6ac03)

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