# STC SR09341RC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Scott's Bell 47 Inc, United States
- Description: Installation of the main rotor grips with integral drag brace clevis, new drag brace, and matching adapter nut for wood blade configurations
- Applied: January 25, 2002
- Status date: August 7, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H-1](https://openairdocs.org/tcds/H-1)
- Certificate PDF: https://openairdocs.org/files/sha256/ee/8b/ee8b547dc82135f26485aa19ffb0c3af97c8f7f7bb2af9e1ccf28f15d779d6b6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D78058161EC5C4EA86257DC800500FE1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09341RC

## ADs that name it (0)

None.

## Approved models (7)

- Scotts-Bell 47 Inc 47B ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47B3 ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47D ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47D1 ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47G ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47G-2 ([TCDS H-1](https://openairdocs.org/tcds/H-1))
- Scotts-Bell 47 Inc 47H-1 ([TCDS H-1](https://openairdocs.org/tcds/H-1))

## 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.

Part 6 of the Civil Air R egulations.

Original Product --Type Certificate N umber :

Installation of the main rotor grips with integral drag brace clevis, new drag brace, and matching adapter nut for wood blade configurations in accordance with Texas Helicopters Co, Inc. FAA Drawing List THC-2002-51, revision IR, Dated January 25, 2002, or later Federal Aviation Administration (FAA) approved revision.

1. Instructions for Continued Airworthiness, Texas Helicopter Co., Inc. Document THC-2002-52 revision IR, dated January 25, 2002, or later FAA accepted revision is required.

2. The installer must determine whether this design change is compatible with previously approved modifications.

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

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.

Scott’s-Bell 47, Inc.

100 Minnesota Avenue Le Sueur, MN 56058

H-1 M ake : Bell Helicopter Textron M odel : 47B; 47B3; 47D; 47D1; 47G; 47G-2; 47H-1 Date of application : January 25, 2002

Date of issuance : July 15, 2002 Date reissued : December 15, 2010; August 7, 2014

B y direction of the A dministrator

Original Signed By:

Karol Mordasiewicz (Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

## Every issue (2)

- August 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ee/8b/ee8b547dc82135f26485aa19ffb0c3af97c8f7f7bb2af9e1ccf28f15d779d6b6)
- December 15, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/22/b6/22b6c6f4b801d5c620194159153c43ff66b4caa087c139ea5d8b32692d6185d5)

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