# STC SR09318RC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Global Helicopter Technology Inc., United States
- Description: Fabrication, modification, and installation of a new vertical fin spar in accordance with Global Helicopter Technology, Inc., Drawing number VTF-030-800, Revision, E, dated June 6, 2001, or later FAA approved revision.
- Applied: March 27, 2001
- Status date: December 8, 2011
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW)
- Certificate PDF: https://openairdocs.org/files/sha256/ba/43/ba43cde357a49e413943a0a112c6e529243ce6fa865bf2c424b64a33e0f9926a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EB19B07FF8966B3686257973005BF0FA.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR09318RC

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron 204B ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))

## 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.

Number SR09318RC

This certificate, issued to Global Spar LLC 1000 85 th Avenue SE Olympia, WA 98501

Part 21.25 of theFederal Aviation Regulations.

Original ProductType Certificate Number: H1SW Make: Bell Model: 204B

Description of the Type Design Change: Fabrication of Global Spar LLC Vertical Fin Spar Kit, Part No.

VTF-030-800-001, in accordance with Global Helicopter Technology, Inc.(GHTI) Master Drawing List No.

VTF-392-110, Revision L, dated December 1, 2011, or later FAA approved revision. Installed in accordance with GHTI Manual No. GHT-VTF-099-204B, Revision B, dated January 18, 2008, or later FAA approved revision.

Maintained in accordance with GHTI Instructions for Continued Airworthiness, Document No. GHT-445-204B, Revision 2, dated October 5, 2001, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies only to rotorcraft models specified above, that are equipped with a standard tail boom with fin assembly part number 205-030-899-125 installed.

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

Date of application: March 27, 2001 Date reissued: January 27, 2004; October 29, 2010 Date of issuance: June 6, 2001 Date amended: December 8, 2011

FAA FORM 8110-2-1 (10-69) PAGE 1 OF 3 PAGES By direction of the Administrator

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SR09318RC Global Spar LLC Issued: June 6, 2001 Reissued: January 27, 2004; October 29, 2010 Amended: December 8, 2011

This modification is not eligible for aircraft equipped with Bell Helicopter 212 Tail Rotor or other Tail Rotor Retrofit Systems installed (212-011-701, Hub and Blade), or with alternate horsepower engines installed that are not specified on the Type Certificate Data Sheet.

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. No Rotorcraft Flight Manual Supplement was deemed necessary for this modification.

- END -

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (2)

- December 8, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ba/43/ba43cde357a49e413943a0a112c6e529243ce6fa865bf2c424b64a33e0f9926a)
- January 27, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0d/e5/0de52b84523d2cf25649aedf4859cc4bd56e29eebe7fe65dc005042bf3576d82)

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