# STC SR00169DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of a fuel cap hinge and hardware. (206B S/N 3567 and subsquent)
- Applied: April 27, 1995
- Status date: July 5, 2023
- Product: Aircraft, Rotorcraft
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/20/15/2015e98e5bb07ebc69d001e3eb5194b89593fdc68c099afb5169f869adb8f8da
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108121020320230814164010.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00169DE

## ADs that name it (0)

None.

## Approved models (5)

- Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-4 ([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 SR00169DE Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 6 the Civil Air Regulations H2SW Bell Textron Canada Limited 206L, 206L-1, 206L-3, 206L-4, 206B, S/N 3567: and subsequent Installation of a Fuel Cap Hinge and Hardware per Paravion Technology, Inc. Drawing List No. DL-206FH-100, N/C, dated April 27, 1995, or later FAA approved revision.

April 27, 1995 July 5, 2023 July 6, 1995 for Manager, West Certification Branch

1. This approval should not be extended to rotorcraft on which previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft.

2. A Copy of this Certificate must be maintained as part of the permanent record for the modified rotorcraft.

3. 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 SR00169DE

## Every issue (2)

- July 5, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/20/15/2015e98e5bb07ebc69d001e3eb5194b89593fdc68c099afb5169f869adb8f8da)
- July 6, 1995: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/5d/f3/5df30285efda7104347a24c894e7e89f77d7f0403f752326d72a47f64c239bb0)

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