# STC SR00850SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Onboard Systems International, United States - Description: Fabrication of Onboard Systems Model 200-260-00 Cargo Hook Kit and Model 200-260-01 Cargo Hook Kit - Applied: July 11, 2000 - Status date: October 7, 2021 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/ba/c8/bac8894d8bbb6427dcf1a983f690b873003ef19cbb9ab6bd4696383eaf6cfc22 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9724B9DE6E3D41BB8625880C00517C33.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR00850SE ## ADs that name it (0) None. ## Approved models (5) - Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 407 ([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. 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) SR00850SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Federal Aviation Regulations H2SW Bell 206L, 206L-1, 206L-3, 206L-4, and 407 Fabrication of Onboard Systems Model 200-260-00 Cargo Hook Kit and Model 200-260-01 Cargo Hook Kit in accordance with FAA approved Onboard Systems Master Drawing List No. 155-057-00, Revision 19, dated October 30, 2009, or later FAA approved revision. Installation of the 200-260-00 Cargo Hook Kit in accordance with FAA approved Onboard Systems Owner’s Manual 120-093-00, Revision 8, dated September 15, 2009, or later FAA approved revision. Approval of this change in type design applies to only those Bell model rotorcraft listed above, which were previously equipped with an FAA approved installation of Bell cargo hook suspension systems 206-706-341-5, 206-706-341-101, or 206-706-341-109; and either Breeze Eastern cargo hooks 17149-2, 17149-6, or Onboard Systems Cargo Hooks, part number 528-010-04 or 528-023-01. This approval should not be extended to 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. July 11, 2000 October 7, 2021 December 15, 2000 January 13, 2003; December 16, 2003; March 29, 2010 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: SR00850SE 3 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: End Description of Type Design Change Continued: SR00850SE This modification must be inspected and maintained in accordance with Section ATA 5 of the FAA approved Onboard Systems Instructions for Continued Airworthiness, Document No. 123-001-00, Revision 4, dated August 11, 2009, or later FAA approved revision and Onboard Systems Cargo Hook Service Manual, Document No. 122-005-00, Revision 15, dated April 23, 2009, or later FAA approved revision. Installation of the 200-260-01 Cargo Hook Kit in accordance with FAA approved Onboard Systems Owner’s Manual No. 120-093-01, Revision 0, dated September 30, 2009, or later FAA approved revision. This modification must be inspected and maintained in accordance with Section ATA 5 of the FAA approved Onboard Systems Instructions for Continued Airworthiness, Document No. 123-001-01, Revision 0, dated October 8, 2009, or later FAA approved revision, and Onboard Systems Cargo Hook Service Manual No. 122-017-00, Revision 5, dated July 27, 2009, or later FAA approved revision. 3 3 Rotorcraft modified in accordance with this STC must be operated in accordance with a copy of an FAA approved Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-002-00, Revision 1, dated September 10, 2004, or later FAA approved revision, for the 200-260-00 cargo hook kit, and Onboard Systems Rotorcraft Flight Manual Supplement No. 121-002-01, Revision 0, dated march 4, 2010, or later FAA approved revision, for the 200-260-01 cargo hook kit. A copy of this certificate, FAA approved RFMS, Owner’s Manual, and Service Manual, must be maintained as part of the permanent records of 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. ## Every issue (4) - October 7, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ba/c8/bac8894d8bbb6427dcf1a983f690b873003ef19cbb9ab6bd4696383eaf6cfc22) - March 15, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/39/d4/39d41cf9160ae1813c7ce21032fb70630b2e9eb27a17eea1a76d86d3f262bd88) - March 29, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/36/13/36135af2df588a36097b6b006214c11ab5a7d6520f86c852d4774a920f6de0da) - December 16, 2003: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f1/7a/f17a165167f7db37d8819af11d7920ebd3b60c8820d19e60c5a7a2f2e5efa343) --- 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.