What it approves
Fabrication of Onboard Systems Model 200-321-00 Cargo Hook Swing Suspension Kit and 200-322-00 Cargo Hook Sling Suspension 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:
(See Continuation Sheet Page 3 of 3 Pages) SR01815SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 27 the Federal AviationRegulations H9EU Airbus Helicopters EC130B4 Fabrication of Onboard Systems Model 200-321-00 Cargo Hook Swing Suspension Kit and 200-322-00 Cargo Hook Sling Suspension Kit in accordance with FAA approved On board Systems Master Drawing List No. 155-121-00, Revision 1, dated February 6, 2008, or later FAA approved revision; and installation of the 200-321-00 Cargo Hook Swing Suspension Kit or 200-322-00 Cargo Hook Sling Suspension Kit in accordance with FAA approved Onboard Systems Owner's Manual No. 120-131-00, Revision 1, dated February 4, 2008, or later FAA approved revision.
Approval of this change in type design applies only to those Airbus Helicopters model rotorcraft listed above equipped with reinforced fuel tank supports installed per Eurocopter Service Bulletin 25-032, OP3630. 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. Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-046-00, revision 0, dated February 19, 2008, or later May 18, 2007 October 7, 2021 February 20, 2008 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:
SR01815SE 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:
SR01815SE This modification must be inspected and maintained in accordance with Section ATA 5 of the FAA approved Onboard Systems Instructions for Continued Airworthiness (ICA) Document No. 123-029-00, Revision 0, dated September 12, 2007, or later FAA approved revision, for the 200-321-00 swing kit, or Section ATA 5 of the FAA approved On board Systems ICA Document No.
123-031-00, Revision 0, dated September 12, 2007, or later FAA approved revision, for the 200-322-00 sling kit, and Onboard Systems Cargo Hook Service Manual No. 122-015-00, Revision 2, dated November 9, 2005, or later FAA approved revision.
3 3 FAA approved revision, for the 200-321-00 Cargo Hook Swing Suspension Kit, or RFMS No.
121-049-00, dated February 19, 2008, or later FAA approved revision, for the 200-322-00 Cargo Hook Sling Suspension Kit. A copy of this Certificate, FAA approved RFMS, ICA document, and Maintenance 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.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Airbus Helicopters | EC130B4 | H9EU |