STC SA1904WE

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SA1904WE

FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 1 of 2

Part 13 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of Vibration Isolation Products (VIP) engine mount PIN VIP-50804-10 on various aircraft as shown on FAA Approved Model List (AML) No. SA1904WE.

Limitations and Conditions: Approval of this change in type design applies to those aircraft listed on the FAA Approved Model List No. SA1904WE. This approval should not be extended to other aircraft of these models on which other previously modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of those aircraft. 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.

This certificate issued to: FTG, Inc.

12750 Center Court Drive S Suite 280 Cerritos, CA 90703 Original Product Type Certificate Number: *See attached FAA Approved Model List (AML) No. SA1904WE for list applicable aircraft make, models, and applicable airworthiness regulations.

Date of Application: December 11, 1968 Date Reissued: Aug.15,1986; Sept.16,1986; May 13, 2022 Date of Issuance: March 13, 1969 Date Amended: October 17, 2002 By Direction of the Administrator Signature:

Title: Aviation Safety Manager, Technical & Administrative Support Section, Los Angeles ACO Branch

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SA1904WE

FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 2 of 2