# STC SR00472DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of mounting hardware to support blade folding kit.
- Applied: January 24, 2002
- Status date: July 5, 2023
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Data sheets: [TCDS R00001RC](https://openairdocs.org/tcds/R00001RC)
- Certificate PDF: https://openairdocs.org/files/sha256/15/83/158343ace267cf7dc386f6f7204efe5e8a35b97ca503e8719295f32eb3f255a4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122595220320230816140355.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00472DE

## ADs that name it (0)

None.

## Approved models (1)

- Bell Textron Canada Limited 427 ([TCDS R00001RC](https://openairdocs.org/tcds/R00001RC))

## 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 SR00472DE Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 27 the Federal Aviation Regulations R00001RC Bell Textron Canada Limited Bell 427 Installation of mounting hardware to support blade folding kit in accordance with Paravion Technology Master Drawing List DL-427BF-100, Revision A, dated May 3, 2002, FAA approved dated May 23, 2002, or later FAA approved revision.

January 24, 2002 July 5, 2023 May 23, 2002 for Manager, West Certification Branch

1. This approval should not be extended to rotorcraft of this model on which other 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 records for the modified rotorcraft.

3. Instructions for Continued Airworthiness, Report PR-427BF-120M, Revision 0, dated May 6, 2002, FAA accepted dated May 9, 2002, or later FAA accepted revision is required for this installation.

4. 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 SR00472DE

## Every issue (2)

- July 5, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/15/83/158343ace267cf7dc386f6f7204efe5e8a35b97ca503e8719295f32eb3f255a4)
- May 23, 2002: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/06/0e/060e869227dc0c2784491b57ecda1bfecf8c23e93200115a285ba0928176d4e8)

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