What it approves
Fabrication of Onboard Systems Model 200-249-00 (without load weigh) or 200-250-00 (with load weigh) cargo hook suspension system
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:
SR00724SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206L-1, 206L-3, 206L-4 and 407 Fabrication of Onboard Systems Model 200-249-00 (without load weigh) or 200-250-00 (with load weigh) cargo hook suspension system in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-049-00, Revision 8, dated April 20, 2007, or later FAA approved revision; and installation of this cargo hook suspension system in accordance with FAA approved Onboard Systems Owner’s Manual No. 120-085-00, Revision 7, dated April 16, 2007, or later FAA approved revision. Inspect this cargo hook kit in accordance with Onboard Systems Owner’s Manual No. 120-085-00, Revision 7, dated April 16, 2007, 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 Auxiliary Equipment Kit – Cargo Hook Provisions P/N 206-706-341-7, -9, -103, -111, or -113. 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. Modified rotorcraft must be operated in accordance with an FAA approved copy of Onboard Rotorcraft Flight Manual Supplement (RFMS) No. 121-045-00, Revision 0, dated August 9, 2007, or later FAA approved revision. A copy of this Certificate and FAA approved RFMS 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.
May 12, 1999 October 7, 2021 January 13, 2003, August 10, 2007 For Acting Manager, Seattle ACO Branch 2 August 4, 1999
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:
SR00724SE 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 4
Every issue · 3
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 |
| August 10, 2007 | Amended, earlier issue | Certificate |
| January 13, 2003 | Amended, earlier issue | Certificate |