# STC SR01149SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Vector Aerospace Helicopter Services USA Inc., United States - Description: Fabrication of Helipro Corporation International Alternate Drive Cover - Applied: September 9, 2002 - Status date: April 15, 2009 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/c4/1b/c41bb6230c4e8c407f78e27e6e9377d6d6cb6714e7015736a92605f655b58467 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/16592C86471F8523862577150046B718.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR01149SE ## ADs that name it (0) None. ## Approved models (1) - Bell Helicopter Textron Canada Limited 206B ([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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR01149SE This certificate, issued to Vector Aerospace Helicopter Services USA, Inc. 22378 Billie Blackmon Road Andalusia, AL 36421 Part 6 of the Civil Air Regulations. Original Product⎯Type Certificate Number: H2SW Make: Bell Helicopter Textron (Canada) Model: 206B Description of the Type Design Change: Fabrication of Helipro Corporation International Alternate Drive Cover in accordance with Helipro Master Drawing List No. H206-033-408-MDL, Revision A, dated October 31, 2002, or later Federal Aviation Administration (FAA)-approved revision; and installation of this system in accordance with Helipro Drawing Number H206-031-462, "Covers, Drive Shaft, Assembly/Installation Bell 206," Revision A, dated October 31, 2002, or later FAA-approved revision. This modification must be maintained in accordance with Helipro Maintenance Manual Supplement, Document No. HCI-021104, Revision 0, dated November 4, 2002, or later FAA-approved revision. Limitations and Conditions: Approval of this change in type design applies to Bell Model 206B rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modification 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 that helicopter. A copy of this Certificate, and the Maintenance Manual Supplement must be maintained as part of the permanent records of the modified helicopter. 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. This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: September 9, 2002 Date reissued: September 10, 2005, April 15, 2009 Date of issuance: November 19, 2002 Date amended: September 5, 2003 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - April 15, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c4/1b/c41bb6230c4e8c407f78e27e6e9377d6d6cb6714e7015736a92605f655b58467) --- 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.