What it approves
Fabrication of Onboard Systems Model 200-195-00 (without load weigh) and 200-196-00 (with load weigh) Cargo Hook Suspension Systems.
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:
SR00418SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206L, 206L-1, 206L-3, 206L-4, and 407 Fabrication of Onboard Systems Model 200-195-00 (without load weigh) and 200-196-00 (with load weigh) Cargo Hook Suspension Systems in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-034-00, Revision 16, dated April 24, 2007, or later FAA approved revision; and Installation of these systems in accordance with FAA approved Onboard Systems Owner's Manual No. 120-055-00, Revision 12, dated April 16, 2007, or later FAA approved revision. Inspect suspension system in accordance with Onboard Systems Owner’s Manual No. 120-055-00, Revision 12, dated April 16, 2007, and Service Manual No. 122-001-00, Revision 0, dated June 13, 2000, or later FAA approved revisions.
Approval of this change in type design applies only to those Bell model rotorcraft listed above, which are equipped with an FAA approved installation of Bell Auxiliary Equipment Kit - Cargo Hook Provisions, P/N’s 206-706-341-7, -9, -103, -111, and -113 only. This approval should not be extended to other rotorcraft on which other previously approved modifications are incorporated unless it is determined 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 FAA approved Rotorcraft Flight Manual Supplement (RFMS) No. 121-044-00, dated July 11, 2007, or later FAA approved revision. A copy of this Certificate and FAA Approved RFMS 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.
January 28, 1997 October 7, 2021 July 8, 1997; August 28, 1997; August 18, 2000;
May 1, 2001; January 13, 2003; July 16, 2007 For Acting Manager, Seattle ACO Branch 2 March 24, 1997
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:
SR00418SE 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 5
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 |
| July 16, 2007 | Amended, earlier issue | Certificate |
| January 13, 2003 | Amended, earlier issue | Certificate |