# STC SR00895SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Onboard Systems International, United States - Description: Fabrication of Onboard Systems Model 200-268-00, 200-268-01, 200-269-00, 200-269-02, or 200-269-03 Cargo Hook Kits - Applied: September 22, 2000 - Status date: January 20, 2012 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/6c/4a/6c4a664dbee3f37f2f1d3d2b24fb24ebc24b0b5b6d1fe82cc5182f07ca0ff2a9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/84B47042837973C78625798E007090D0.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR00895SE ## ADs that name it (0) None. ## Approved models (2) - Bell Helicopter Textron (Canada) 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) ## What the certificate says Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: (See Continuation Sheet Page 3 of 3 Pages) SR00895SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206A and 2068 Fabrication of Onboard Systems Model 200-268-00, 200-268-01, 200-269-00, 200-269-02, or 200-269-03 Cargo Hook Kits in accordance with Federal Aviation Administration(FAA) approved Onboard Systems Master Drawing List No. 155-064-00, Revision 11, dated August 15, 2011, or later FAA-approved revision. Approval of this change in type design applies to only those Bell model rotorcraft listed above which are equipped with Bell part number 206-706-335-3, -5, -105, or -109 Auxiliary Equipment Kit•Cargo Hook Provisions. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship 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. September 22, 2000 October 7, 2021 March 26, 2001 January 13, 2003; October 1, 2007; April 23, 2008; January 20, 2012 For Acting Manager, Seattle ACO Branch 3 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00895SE 3 FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration TOMMISTRATO Supplemental Type Certificate (Continuation Sheet) Number: SR008955E Description of Type Design Change: Continued: Installation of these On board Systems kits in accordance with FAA-approved Onboard Systems Owner's Manual listed in the table below, or later FAA-approved revision. This modification must be inspected and maintained in accordance with FAA-approved Onboard Systems Owner's Manual and Component Maintenance Manual listed in the table below, or later FAA-approved revision. System Part No. Owner's Manual No. Component Maintenance Manual No. 200-268-00 120-099-00, Revision 9, dated 122-005-00, Revision 21, dated March 2, 2010 April 7, 2011 200-268-01 July 19, 2011 120-099-01, Revision o, dated 122-017-00, Revision 14, dated September 2, 2011 200-269-00 120-099-00, Revision 9, dated 122-005-00, Revision 21, dated March 2, 2010 April 7, 2011 200-269-02 120-099-00, Revision 9, dated 122-005-00, Revision 21, dated March 2, 2010 April 7, 2011 200-269-03 120-099-01, Revision 0, dated 122-017-00, Revision 14, dated July 19, 2011 September 2, 2011 Limitations and Conditions: Continued: Rotorcraft modified in accordance with this STC must be operated in accordance with FAA-approved Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121 009 00, Revision 2, dated September 27, 2007, or later FAA-approved revision, for the 200-268-00, 200-269-00, 200 269 02 cargo hook kits or Onboard Systems RFMS 121-009-01, Revision 0, dated November 30, 2011, or later FAA-approved revision, for the 200-268-01 or 200-269-03 cargo hook kits. A copy of this certificate, a copy of the FAA-approved RFMS, Owner's Manual, and Component Maintenance Manual must be maintained as part of the permanent records for the modified rotorcraft. 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. End This FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 3 of 3 ## Every issue (4) - January 20, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/6c/4a/6c4a664dbee3f37f2f1d3d2b24fb24ebc24b0b5b6d1fe82cc5182f07ca0ff2a9) - April 3, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/60/4c/604c32b34f685dfed7300a916f9c812aa1b8110e50d795d4a8c31f872a389bd0) - October 1, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/45/72/4572248e2d4d17287600f6e94340eadaa35726720aebc1325ca7e0c1662e8137) - January 13, 2003: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ba/ee/baee865b79b19bba60a7079d13234b1209fdf8bd486005e425a026ecc48a66b9) --- 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.