# STC SA00943SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Merlyn Products Inc., United States
- Description: Installation of Merlyn Products Inertia Link on the above model aircraft per Merlyn Top Drawing List 91.50-TDL, Revision A, dated July 13, 2001, and Merlyn Installation Instructions Report 91.50-1, Revision N/C, dated June 12, 2001, or later FAA approved revision of either of these documents.
- Applied: June 12, 2001
- Status date: July 18, 2001
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE)
- Certificate PDF: https://openairdocs.org/files/sha256/66/bb/66bbd8c8bf3fbd7fba89482b1d631dbe3667bd9bea9b763e00abfe61f6269813
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/623930FC4AA41BA286257959006CC774.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00943SE

## ADs that name it (0)

None.

## Approved models (5)

- Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))

## 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 SA00943SE This certificate, issued to Merlyn Products, Inc.

West 7500 Park Drive Spokane, WA 99224-5726 Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A17WE Make: Aerostar Model: 600, 601, 601P, 602P, and 700P

Description of the Type Design Change: Installation of Merlyn Products Inertia Link on the above model aircraft per Merlyn Top Drawing List 91.50-TDL, Revision A, dated July 13, 2001, and Merlyn Installation Instructions Report 91.50-1, Revision N/C, dated June 12, 2001, or later FAA approved revision of either of these documents.

Limitations and Conditions: Incorporation of this change in type design, when accomplished in accordance with the above data, constitutes an alternate means of compliance for Airworthiness Directive 2001-08-10 (Docket No. 2000-CE-31-AD). Approval of this change in type design applies to the above models only. This approval should not be extended to aircraft of this model 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 must be maintained as part of the permanent records for the modified aircraft.

Date of application: June 12, 2001 Date reissued:

Date of issuance: July 18, 2001 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- July 18, 2001: Issued, Current. [certificate](https://openairdocs.org/files/sha256/66/bb/66bbd8c8bf3fbd7fba89482b1d631dbe3667bd9bea9b763e00abfe61f6269813)

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