# STC SA169NW

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Merlyn Products Inc., United States
- Description: Installation of Merlyn Products motor, part number 06-6001
- Applied: December 30, 1974
- Status date: October 4, 2018
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-766](https://openairdocs.org/tcds/A-766)
- Certificate PDF: https://openairdocs.org/files/sha256/3a/3a/3a3a8c66b5a75b8dc3826a69bae6e75c0bccf96c23ee09d6ada25fff1dde1870
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E3EE5F98772B5AD586258322005B6ECF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA169NW

## ADs that name it (0)

None.

## Approved models (2)

- Swift Museum Foundation Inc. GC-1A ([TCDS A-766](https://openairdocs.org/tcds/A-766))
- Swift Museum Foundation Inc. GC-1B ([TCDS A-766](https://openairdocs.org/tcds/A-766))

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA169NW

This certificate, issued to Merlyn Products, Inc.

7500 West Park Drive Spokane, WA 99224

Part 4A of the Civil Aviation Regulations.

Original ProductType Certificate Number: A-766 Make: Swift (Globe, TEMCO) Model: GC-1A, GC-1B

Description of the Type Design Change: Installation of Merlyn Products motor, part number 06-6001-501 or 06-6001-502, in accordance with Merlyn Products Installation Instructions, Report 06-01, Revision F; or installation of Merlyn Products motor, part number 06-6001-550, in accordance with Merlyn Products Installation Instructions, Report 06-01, Revision G, dated March 26, 2018, or later FAA-approved revisions.

Limitations and Conditions: 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 series u nless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate must 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: December 30, 1974 Date reissued: July 21, 1986 Date of issuance: March 28, 1975 Date amended: July 21, 1986; September 22, 2000;

October 4, 2018

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (2)

- October 4, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/3a/3a/3a3a8c66b5a75b8dc3826a69bae6e75c0bccf96c23ee09d6ada25fff1dde1870)
- September 22, 2000: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/13/e0/13e00372bcfcebad2af3f9c7955e985e4dd02a1ffb404cf11f79c0910d9732d6)

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