# STC SA1845WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: FTG Inc., United States - Description: 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. - Applied: June 20, 1968 - Status date: January 3, 2023 - Product: Aircraft, Single-Engine - Certification basis: Part 13, Part 21 - Data sheets: [TCDS 1A8](https://openairdocs.org/tcds/1A8), [TCDS 1A10](https://openairdocs.org/tcds/1A10), [TCDS 1A15](https://openairdocs.org/tcds/1A15), [TCDS 2A10](https://openairdocs.org/tcds/2A10) - Certificate PDF: https://openairdocs.org/files/sha256/ca/22/ca22b994b9e745b5ede8e5d62297751d4d5309198ebf4bdfbf98f3989bc2e9e0 - Approved model list and other attachments: [SA1845WE AML.pdf](https://openairdocs.org/files/sha256/fb/f4/fbf4b75640c78130d799f0fd3b29fd1cbd234641bf4890222fe903f610695b0e) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197729002320230111140903.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1845WE ## ADs that name it (0) None. ## Approved models (7) - Alliance Aircraft Group LLC H-395A ([TCDS 1A8](https://openairdocs.org/tcds/1A8)) - The New Piper Aircraft Inc. PA-23-235 ([TCDS 1A10](https://openairdocs.org/tcds/1A10)) - The New Piper Aircraft Inc. PA-23-250 (Navy UO-1) ([TCDS 1A10](https://openairdocs.org/tcds/1A10)) - The New Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - The New Piper Aircraft Inc. PA-24-260 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - The New Piper Aircraft Inc. PA-25-235 ([TCDS 2A10](https://openairdocs.org/tcds/2A10)) - The New Piper Aircraft Inc. PA-25-260 ([TCDS 2A10](https://openairdocs.org/tcds/2A10)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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 ### SA1845WE AML.pdf **FAA APPROVED MODEL LIST (AML) NO. SA1845WE** **VIBRATION ISOLATION PRODUCTS CORPORATION FOR** **INSTALLATION OF AN ENGINE VIBRATION ISOLATION SYSTEM** Issue Date: December 4, 1968 ITEM **ENGINE MOUNT** **PART NUMBER** **TOP DRAWNING** **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICATE NUMBER CERT.** **BASIS** **AML AMENDMENT** **DATE NUMBER** REVISION & DATE 1 VIP-50804-20 VIP-50804-20 12/3/68 Helio H395A 1A8 CAR 13 2 VIP-50804-20 VIP-50804-20 B, 6/5/00 Piper PA-23-235, PA-23-250 1A10 CAR 13 10/17/02 3 “ “ “ “ PA-23-250, PA-24-260 1A15 CAR 13 “ 4 “ “ “ ” PA-23-235, PA-24-260 2A8, 2A10 “ “ ---------- END OF DATA ---------- Approved: Haifa Haj-Eid Manager, Technical & Administrative Support Section Date: January 3, 2023 ## Every issue (2) - January 3, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ca/22/ca22b994b9e745b5ede8e5d62297751d4d5309198ebf4bdfbf98f3989bc2e9e0), [SA1845WE AML.pdf](https://openairdocs.org/files/sha256/fb/f4/fbf4b75640c78130d799f0fd3b29fd1cbd234641bf4890222fe903f610695b0e) - October 17, 2002: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/6f/d4/6fd481c8d7e6ee4bbf961b043374be3f3924adb6537a09b8687e324761b91ead), [SA1845WE-AML.pdf](https://openairdocs.org/files/sha256/2d/0f/2d0f1f62954b4672f0620b1409a5ea4cb900c0c36c91ef4ad7d624b34045e1cc) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.