STC SR01064SE

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) SR01064SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 27 the Federal Aviation Regulations H11NM Robinson R44, R44 II Fabrication of Onboard Systems Model 200-265-00 12 Volt Talon LC Keeperless cargo hook kit, Model 200-288-00 28 Volt Talon LC Keeperless cargo hook kit without load weigh, and 200-289-00 28 Volt Talon LC Keeperless cargo hook kit with load weigh, in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-062-00, Revision 15, dated November 24, 2010, or later FAA approved revision.

Approval of this change in type design applies to only the Robinson R44 and R44 II rotorcraft equipped with Robinson hard point/tiedown block P/N D134-1. 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. This modification has been approved by the FAA for Class B and C Rotorcraft-Load Combinations, Non-human External Cargo only. Modified rotorcraft must be operated in accordance with an FAA approved copy of Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-007-00, Revision 3, dated February 22, 2011, or later FAA approved revision for the Robinson R44 rotorcraft and Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-017-00, Revision 2, dated April 22, 2005, or later FAA approved revision, for the Robinson R44 II rotorcraft. A copy of this Certificate, Owner’s Manual, Service Manual and the FAA approved RFMS must be maintained as a 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.

September 22, 2000 October 7, 2021 March 13, 2002 October 17, 2003; August 10, 2004;

March 15, 2011 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:

SR01064SE 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:

SR01064SE Installation of the Onboard Systems cargo hook kit part number 200-265-00 in accordance with FAA approved Onboard Systems Owner’s Manual 120-097-00, Revision 11, dated November 9, 2010, or later FAA approved revision. This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-005-00, Revision 9, dated February 15, 2011, or later FAA approved revision, and Cargo Hook Component Maintenance Manual, 122-005-00, Revision 20, dated November 23, 2010, or later FAA approved revision.

Installation of the Onboard Systems cargo hook kit part numbers 200-288-00 or 200-289-00 in accordance with FAA approved Onboard Systems Owners Manual 120-111-00, Revision 10, dated February 26, 2008, or later FAA approved revision. This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-016-00, Revision 5, dated June 01, 2007, or later FAA approved revision, Suspension System Owner’s Manual 120-111-00, Revision 10, dated February 26, 2008, or later FAA approved revision, and Cargo Hook Component Maintenance Manual, 122-005-00, Revision 20, dated November 23, 2010, or later FAA approved revision.