STC SR01394SE

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) SR01394SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 27 the Federal Aviation Regulations H9EU Airbus Helicopters AS350B, AS350B1, AS350B2, AS350B3, AS350BA, and AS350D Fabrication of Onboard Systems Models 200-287-00 and 200-287-01 Cargo Hook Kits in accordance with Onboard Systems Master Drawing List No. 155-096-00, Rev. 8, dated February 18, 2014, or later FAA approved revision; and Installation of the Model 200-287-00 cargo hook kit in accordance with Onboard Systems Owner’s Manual No. 120-108-00, Rev. 10, dated March 10, 2010, or later FAA approved revision.

Approval of this change in type design applies to only those Airbus Helicopters models listed above which are equipped with cargo hook fixed parts per Airbus Helicopters Service Bulletin No. 25.00.04. This approval should not be extended to helicopters 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 helicopter.

March 31, 2003 October 7, 2021 April 9, 2004 April 29, 2014 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:

SR01394SE 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 the Type Design Change continued:

SR01394SE Inspect and Maintain the Model 200-287-00 cargo hook kit in accordance with Section 5 of Onboard Systems Instructions for Continued Airworthiness (ICA) Document 123 015-00, Revision 7, dated March 23, 2014, or later FAA accepted revision, and Onboard Systems Cargo Hook Component Maintenance Manual 122-005-00, Revision 26, dated March 26, 2013, or later FAA-accepted revision. Installation of the 200-287-01 cargo hook kit in accordance with Onboard Systems Owner’s Manual No. 120-108-01, Revision 0, dated November 18, 2013, or later FAA approved revision. Inspect and Maintain the Model 200-287-01 cargo hook kit in accordance with Section 5 of Onboard Systems Instructions for Continued Airworthiness (ICA) Document 123-015-01, Revision 0, dated February 17, 2014, or later FAA accepted revision, and Onboard Systems Cargo Hook Component Maintenance Manual 122-017-00, rev. 17, dated July 31, 2012, or later FAA accepted revision.

3 3 Rotorcraft modified in accordance with this STC must be operated in accordance with a copy of the FAA approved Onboard Systems Rotorcraft Flight Manual Supplement (RFMS), Document No. 121-016-00, revision 1, dated March 7, 2008, or later FAA approved revision for the 200-287-00 cargo hook kit or Onboard Systems RFMS, Document No. 121-016-01, revision 0, dated April 15, 2014, or later FAA approved revision for the 200-287-01 cargo hook kit. A copy of this Certificate, applicable Owner’s Manual, ICA, Component Maintenance Manual and a copy of the FAA approved Rotorcraft Flight Manual Supplement must be maintained as part of the permanent records of the modified helicopter.

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.