What it approves
Installation of Vibration Isolation Products (VIP) engine mount P/N VIP-50804-20 on various aircraft as shown on FAA Approved Model List (AML) No. SA1845WE.
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.
United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SA184SWE
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 P VIP-50804-20 on various aircraft as shown on FAA Approved Model List (AML) No. SA1845WE.
Limitations and Conditions: Approval of this change in type design applies to those aircraft listed on the FAA Approved Model List No. SA1845WE. 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 ai1worthiness 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. SA1845SWE for list applicable aircraft make, models, and applicable airworthiness regulations.
Date of Application: June 20, 1968 Date Reissued: Aug.15,1986; Sept.16,1986; May 13, 2022 Date of Issuance: December 4, 1968 Date Amended: Oct. 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: SA184SWE
FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 2 of 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
| Make | Model | Data sheet |
|---|---|---|
| Alliance Aircraft Group LLC | H-395A | 1A8 |
| The New Piper Aircraft Inc. | PA-23-235 | 1A10 |
| The New Piper Aircraft Inc. | PA-23-250 (Navy UO-1) | 1A10 |
| The New Piper Aircraft Inc. | PA-24-250 | 1A15 |
| The New Piper Aircraft Inc. | PA-24-260 | 1A15 |
| The New Piper Aircraft Inc. | PA-25-235 | 2A10 |
| The New Piper Aircraft Inc. | PA-25-260 | 2A10 |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| January 3, 2023 | Reissued, current | CertificateApproved model list |
| October 17, 2002 | Amended, earlier issue | CertificateApproved model list |