What it approves
Installation of Onboard Systems International Cargo Hook Kit and Load Weight
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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:
SR00896SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206A and 206B Installation of Onboard Systems International Cargo Hook Kit and Load Weight Kit in accordance with Onboard Master Drawing List No. 155-063-00, Revision 9, dated August 25, 2015, or later Federal Aviation Administration (FAA) approved revision. Maintained in accordance with Owner’s Manual Document 120-098-00, Revision 7, dated June 16, 2010, Owner’s Manual, Document 120-098-01, Revision 3, dated October 17, 2014, or later FAA approved revisions; or Instructions for Continued Airworthiness (ICA) Document 123-042-00, Revision 0, dated August 18, 2015, or later FAA accepted revision, as applicable. Operated in accordance with FAA-approved Rotorcraft Flight Manual Supplement (RFMS) Documents 121-008-00, Revision 2; 121-008-01, Revision 1; or 121-059-00, Revision 0; all dated November 30, 2015, as applicable Approval of this change in type design applies only to those Bell model rotorcraft listed above, which were previously equipped with an FAA approved installation of Bell cargo hook suspension system, Part Number (P/N) 206-072-900-1, 206-072-900-101, or 206-072-900-103; Bell cargo hook provisions kit, P/N 206-706-335-3, 206-706-335-5, or 206-706-335-105; and Breeze Eastern cargo hook, P/N SP 4232-4, SP 4232-5, or SP 4232-5L. 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. A copy of this certificate, the Owner’s Manual identified in the MDL, the applicable FAA approved RFMS, and the ICA (if applicable) must be maintained as a 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.
September 22, 2000 October 7, 2021
May 17, 2001; January 13, 2003; March 31, 2010; December 7, 2015 For Acting Manager, Seattle ACO Branch 2 March 26, 2001
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:
SR00896SE 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 7, 2021 | Reissued, current | Certificate |
| December 7, 2015 | Amended, earlier issue | Certificate |
| March 31, 2010 | Amended, earlier issue | Certificate |
| January 13, 2003 | Amended, earlier issue | Certificate |