# STC SR09316RC - Type: Supplemental type certificate - Status: Current, Amended - Holder: Global Spar LLC, United States - Description: Fabrication, modification, and installation of a new vertical fin spar in accordance with Global Helicopter Technology, Inc., Drawing number VTF-030-801, Revision B, dated April 5, 2001, or later FAA approved revision. - Applied: November 1, 2000 - Status date: December 8, 2011 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H5SO](https://openairdocs.org/tcds/H5SO), [TCDS H7SO](https://openairdocs.org/tcds/H7SO), [TCDS H3SO](https://openairdocs.org/tcds/H3SO), [TCDS H13WE](https://openairdocs.org/tcds/H13WE), [TCDS H3NM](https://openairdocs.org/tcds/H3NM), [TCDS H5NM](https://openairdocs.org/tcds/H5NM), [TCDS H1RM](https://openairdocs.org/tcds/H1RM), [TCDS H8NM](https://openairdocs.org/tcds/H8NM), [TCDS R00012AT](https://openairdocs.org/tcds/R00012AT), [TCDS H6SO](https://openairdocs.org/tcds/H6SO), [TCDS H4NM](https://openairdocs.org/tcds/H4NM) - Certificate PDF: https://openairdocs.org/files/sha256/a3/8a/a38a2cecea7ad3c9d4b049e1d760123bf4ad079354b233a1f10e8b6996ed81eb - Approved model list and other attachments: [SR09316RCR1 AML .pdf](https://openairdocs.org/files/sha256/b7/54/b754d22452dd1f7209cbc36a51ba519345da9c9c8dee1baa5a36c7050607c9aa) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/71343B620D66394A862579730056F303.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR09316RC ## ADs that name it (0) None. ## Approved models (19) - International Helicopters Inc. UH-1B ([TCDS H5SO](https://openairdocs.org/tcds/H5SO)) - Overseas Aircraft Support Inc TH-1L ([TCDS H7SO](https://openairdocs.org/tcds/H7SO)) - Overseas Aircraft Support Inc UH-1E ([TCDS H7SO](https://openairdocs.org/tcds/H7SO)) - Overseas Aircraft Support Inc UH-1L ([TCDS H7SO](https://openairdocs.org/tcds/H7SO)) - Richards Heavylift Helo Inc. UH-1B ([TCDS H3SO](https://openairdocs.org/tcds/H3SO)) - Rotorcraft Development Corporation HH-1K ([TCDS H5NM](https://openairdocs.org/tcds/H5NM)) - Rotorcraft Development Corporation TH-1L ([TCDS H5NM](https://openairdocs.org/tcds/H5NM)) - Rotorcraft Development Corporation UH-1B ([TCDS H13WE](https://openairdocs.org/tcds/H13WE)) - Rotorcraft Development Corporation UH-1B ([TCDS H3NM](https://openairdocs.org/tcds/H3NM)) - Rotorcraft Development Corporation UH-1E ([TCDS H5NM](https://openairdocs.org/tcds/H5NM)) - Rotorcraft Development Corporation UH-1L ([TCDS H5NM](https://openairdocs.org/tcds/H5NM)) - San Joaquin Helicopters UH-1B ([TCDS H1RM](https://openairdocs.org/tcds/H1RM)) - Smith Helicopters UH-1E ([TCDS H8NM](https://openairdocs.org/tcds/H8NM)) - Southern Helicopter Inc. UH-1B ([TCDS R00012AT](https://openairdocs.org/tcds/R00012AT)) - Southwest Florida Aviation International SW204 (UH-1B) ([TCDS H6SO](https://openairdocs.org/tcds/H6SO)) - Southwest Florida Aviation International SW204HP (UH-1B) ([TCDS H6SO](https://openairdocs.org/tcds/H6SO)) - US Helicopter Inc. TH-1L ([TCDS H4NM](https://openairdocs.org/tcds/H4NM)) - US Helicopter Inc. UH-1E ([TCDS H4NM](https://openairdocs.org/tcds/H4NM)) - US Helicopter Inc. UH-1L ([TCDS H4NM](https://openairdocs.org/tcds/H4NM)) ## 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 SR09316RC 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: ** See Associated FAA Approved Model List (AML) Make: ** Model: ** Description of the Type Design Change: Fabrication of Global Spar LLC Vertical Fin Spar Kit, Part No. VTF-030-801-001, 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-100-UH1, Revision C, dated June 5, 2008, or later FAA approved revision. Maintained in accordance with GHTI Instructions for Continued Airworthiness, Document No. GHT-425-105, Revision 3, dated January 24, 2003, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to rotorcraft models specified on associated AML SR09316RC only, that are equipped with standard tail booms with part number 204-031-090-1, fin assemblies 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: November 1, 2000 Date reissued: January 27, 2004; October 29, 2010 Date of issuance: April 16, 2001 Date amended: 4/22/2011; 5/18/2011; 12/8/11 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) Number SR09316RC Global Spar LLC Issued: April 16, 2001 Reissued: January 27, 2004; October 29, 2010 Amended: 4/22/2011; 5/18/2011; 12/8/11 Limitations and Conditions continued: 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 Sheets listed on the associated FAA approved AML. 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** ### SR09316RCR1 AML .pdf FAA APPROVED MODEL LIST (AML) SR09316RC FOR Fabrication, modification, and installation of a new vertical fin spar. ISSUE DATE: May 18, 2011 Page 1 of 2 **FAA APPROVED** **ROTORCRAFT FLIGHT** **MANUAL SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** **ITEM ROTORCRAFT MAKE** **ROTORCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** ALTERATION Number Revision* Drawing Revision* AML REV DATE 1. Richard’s Heavylift Helo, Inc. UH-1B H3SO 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 2. Southwest Florida Aviation International Inc. UH-1B H6SO 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 3. Rotorcraft Dev. Corp. UH-1B H3NM 21.25 (a) (2) as Amended by 21-42 dated January 6, 1975 N/A N/A VTF-392-110 Revision L 12/8/11 4. Rotorcraft Dev. Corp. UH-1B H13WE 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 5. San Joaquin Helicopters UH-1B H1RM 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 6. International Helicopters, Inc. UH-1B H5SO 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 7. Southern Helicopter, Inc. UH-1B R00012AT 21.25 (a) (2) Effective February 1, 1965 Including Amendments 21-1 through 21-71 N/A N/A VTF-392-110 Revision L 12/8/11 8. Bell Helicopter Textron, Inc. UH-1E, TH-1L, UH-1L H4NM FAR 21.25 (a) (2) Including Amendments 21-2 through 21-65 Effective February 8, 1982 N/A N/A VTF-392-110 Revision L 12/8/11 * Or later FAA Approved Revision FAA APPROVED MODEL LIST (AML) SR09316RC FOR Fabrication, modification, and installation of a new vertical fin spar. ISSUE DATE: May 18, 2011 Page 2 of 2 **FAA APPROVED** **ROTORCRAFT FLIGHT** **MANUAL SUPPLEMENT** **FAA APPROVED** **MASTER DRAWING LIST** **ITEM ROTORCRAFT MAKE** **ROTORCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** ALTERATION Number Revision* Drawing Revision* AML REV DATE 9. Rotorcraft Dev. Corp. UH-1E, HH-1K, UH-1L, TH-1L H5NM FAR 21.25 (a) (2) Including Amendments 21-1 through 21-56 Effective February 8, 1982 N/A N/A VTF-392-110 Revision L 12/8/11 10. Overseas Aircraft Support Inc. UH-1E, TH-1L, UH-1L H7SO FAR 21.25 (a) (2) Including Amendments 21-1 through 21-56 Effective February 8, 1982 N/A N/A VTF-392-110 Revision L 12/8/11 11. Smith Helicopters UH-1E H8NM FAR 21.25 (a) (2) Effective February 1, 1965 N/A N/A VTF-392-110 Revision L 12/8/11 FAA Approved: Acting Manager, Seattle Aircraft Certification Office AMENDED: December 8, 2011 ## Every issue (4) - December 8, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a3/8a/a38a2cecea7ad3c9d4b049e1d760123bf4ad079354b233a1f10e8b6996ed81eb), [SR09316RCR1 AML .pdf](https://openairdocs.org/files/sha256/b7/54/b754d22452dd1f7209cbc36a51ba519345da9c9c8dee1baa5a36c7050607c9aa) - May 18, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/9b/fb/9bfbfac12f979bcf36571dea73226dd9bbde261e43ab0c912d94b2e8e196b06e), [SR09316RC AML.pdf](https://openairdocs.org/files/sha256/0f/b3/0fb30ec9d4eaada4399b8beb9657577e33c35205a7af14502fcb82531a83a85e) - April 22, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ba/d5/bad549ec3631fc99d06fefcc9ef210010e9a3714e97764ddbd356886098c96e8) - January 27, 2004: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/1c/84/1c8400a48b1171b6692510140c826f4d3596663af30b546f4f53f67f65ce8ff3) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.