# STC SA01663SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Merlyn Products Inc., United States - Description: Installation of Turbo Charger System. - Applied: February 25, 2004 - Status date: April 26, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16) - Certificate PDF: https://openairdocs.org/files/sha256/37/b4/37b4a20f25d35f63681d163a6430def3a2d5cabb0b6df8f4263774f873becb41 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F18490C0A1A6F11586257A2100642E59.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01663SE ## ADs that name it (0) None. ## Approved models (5) - Raytheon Aircraft Company 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company G58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) ## 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 SA01663SE This certificate, issued to Merlyn Products Inc. 7500 West Park Drive Spokane, WA 99224 Part 3 of the Civil Aviation Regulations. Original ProductType Certificate Number: 3A16 Make: Raytheon Aircraft Company Model: 95-C55, D55, E55, 58 and G58 Description of the Type Design Change: Installation of Turbo Charger System per Merlyn Sales Inc Reports 101-01, Rev A, dated March 15, 2006, and either 101-02, Rev A, dated March 15, 2006, or 101-03, Rev A, dated March 15, 2006 all titled “Installation Instructions” or later FAA approved revision to any of these documents. Limitations and Conditions: Approval of this change in type design applies to the above models only. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationships 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 the appropriate Airplane Flight Manual Supplement dated April 4, 2006 shall be maintained as part of the permanent records for the modified 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. Date of application: February 25, 2004 Date reissued: Date of issuance: April 26, 2006 Date amended: Original signed by Mike Pasion (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - April 26, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/37/b4/37b4a20f25d35f63681d163a6430def3a2d5cabb0b6df8f4263774f873becb41) --- 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.