What it approves
Replacement of Bell magnesium cargo hook bumper and ring Part Nos. 204-072-901-1 or -3, and 204-072-905-3, respectively, with Onboard bumper ring kit No. 210-092-00. Fabrication of Onboard Systems Model 210-092-00 bumper ring kit
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:
SH5737NM Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part * the * Regulations * * *See attached Approved Model List (AML) No. SH5737NM for list of approved rotorcraft models and applicable airworthiness regulations.
Replacement of Bell magnesium cargo hook bumper and ring Part Nos. 204-072-901-1 or -3, and 204-072-905-3, respectively, with Onboard bumper ring kit No.
210 092-00. Fabrication of Onboard Systems Model 210-092-00 bumper ring kit in accordance with FAA approved Onboard Systems Master Drawing List No.
155-021-00, Revision 2, dated March 10, 1999, or later FAA approved revision; and installation of this system in accordance with FAA approved Onboard Systems Owner’s Manual No. 120-033-01, Revision 3, dated July 10, 1996, or later FAA approved revision. Inspect cargo hook bumper rings in accordance with Section 4 of Onboard Systems Owner’s Manual No. 120-033-01, Revision 3, dated July 10, 1996, or later approved revision.
Approval of this change in type design applies to only those Bell model rotorcraft listed on AML SH5737NM, amended May 5, 1999, or later FAA approved amendments, which were previously equipped with an FAA approved installation of Bell cargo hook suspension assembly, P/N 204-072-915-103, with either Breeze-Eastern Cargo Hook P/N SP7109-12 or SP7109 62. 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. Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of the Rotorcraft Flight Manual Supplement, revised May 5, 1999, or later FAA approved revision. A copy of this Certificate, Continuation Sheet No. SH5737NM, AML No. SH5737NM, and FAA approved Rotorcraft Flight Manual Supplement 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 the permission.
July 1, 1992 October 7, 2021 May 5, 1999; January 13, 2003 For Acting Manager, Seattle ACO Branch 2 July 27, 1992
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:
SH5737NM 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 7
Every issue · 2
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 | CertificateAML_SH5737NM |
| January 13, 2003 | Amended, earlier issue | Certificate |