# STC SR00449DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of removable dual pedal system.
- Applied: February 23, 2001
- Status date: August 22, 2023
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/3b/bb/3bbbf1a2af86dfa2f45ebca0c85ecfc9a133007ea7689f45284e93c194024271
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145137096520231011141557.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00449DE

## 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

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SR00449DE Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 27 the Federal Aviation Regulations H2SW Bell Helicopter 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, and 407 Installation of Removable Dual Pedal System in accordance with Paravion Technology, Inc. Master Drawing List Report No. DL-206/407RDP-100, Revision A, dated March 23, 2001, FAA approved April 25, 2001, or later approved revision.

February 23, 2001 August 22, 2023 April 25, 2001 for Manager, West Certification Branch

1. Compatibility of this design change with previously approved modifications must be determined by installer.

2. Instruction for Continued Airworthiness, Document Number PR-206/407RDP-120M, entitled, "206/407RPD-100 Removable Dual Pedal Installation", Original Revision, dated April 12, 2001, or later FAA accepted revision is required for this installation.

3. A copy of this Certificate must be maintained as part of the permanent records of the modified aircraft.

4. FAA approved Rotorcraft Flight Manual Supplement, Document No. PR-206/407RDP-100M, Revision 0, dated April 25, 2001, or later FAA approved revision is required for this installation.

5. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SR00449DE

## Every issue (2)

- August 22, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3b/bb/3bbbf1a2af86dfa2f45ebca0c85ecfc9a133007ea7689f45284e93c194024271)
- April 25, 2001: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/06/f3/06f3c2fcc93cce8e4c36cbfd6549c4e3334a0288ee3f05a75725e74d511e6bef)

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