# STC SA01548SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Gold Coast Aviation Service Inc, United States - Description: Installation of a Lycoming O-320-E2D engine modified by STC SE3692SW. - Applied: October 14, 2004 - Status date: May 17, 2005 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A13CE](https://openairdocs.org/tcds/A13CE) - Certificate PDF: https://openairdocs.org/files/sha256/61/f2/61f232d4497bfd36632c1efd57668d5f90453a147b92c112581e9f27693a3ca2 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/41A9C7A4B480F06186257074004EF741.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01548SE ## ADs that name it (0) None. ## Approved models (1) - The Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) ## 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. Number SA01548SE This certificate, issued to Gold Coast Aviation Service, Inc. 45 Mortensen Ave. Municipal Airport Salinas, Ca 93905 Part 23 of the Federal Aviation Regulations. Original Product⎯Type Certificate Number: A13CE Make: Cessna Model: 177 Description of the Type Design Change: Installation of a Lycoming O-320-E2D engine modified by STC SE3692SW in a Cessna 177 in accordance with Gold Coast Aviation Service Inc. Report GCA-177-1-04 Initial Release, dated May 5, 2005. Limitations and Conditions: In order for an airplane to be eligible for modification under this STC, RAM STC SE3692SW must have been incorporated on the replacement engine. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined 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 aircraft. A copy of this certificate and Airplane Flight Manual Supplement GCA 177-1-05 dated May 17, 2005 or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft. The engine must be maintained in accordance with the provisions of STC SE3692SW, and other approved instructions. 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. Date of application: October 14, 2004 Date reissued: Date of issuance: May 17, 2005 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - May 17, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/61/f2/61f232d4497bfd36632c1efd57668d5f90453a147b92c112581e9f27693a3ca2) --- 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.