# STC SA5164SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilizer system Model ST-163 with optional automatic electric trim system.
- Applied: May 12, 1983
- Status date: February 23, 1993
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3SO](https://openairdocs.org/tcds/A3SO)
- Certificate PDF: https://openairdocs.org/files/sha256/e2/66/e266bfff04247a4596fe0746950689a8d73744d3b6d2556be037b60d34b87448
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C6841092CA4E6E7485256CC200122725.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5164SW-D

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

At 300 e 20 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA51645W-0 This certificate issued to: S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 Port 3 of the CIVIl Air Regulations Original Product -Typobortificato Number: A3S0 Make: PIPER Model: PA-32-260, PA-32-300, and PA-32R-300 Description of Type Design Change:

Installation of S-TEC System 60 Pitch Stabilization System, Model ST-163, with optional Automatic Electric Trim System, according to Bulletin No. 263, Revision 2, dated 2-12-93 and Master Drawing List No. 92193, Revision B, dated 2-12-93 or later FAA Approved revisions of the above data (14 Volt System).

FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89209, dated 6-06-83 is required for Piper Models PA-32-260 and PA-32-300 or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC.)

Date of Application: 5-12-83 Dals miserad:

Galoofisnanco:: 6-06-83 Date Amended: 3-28-84, 2-23-93, Revision 2 FEDERAL AVIATION By Direction of the Administrator ( Signature) Wiliam J. Thomas DAS Staff Coordinator, DAS 5 SW (Tille)

**PAA FOR 81 10-2 (10-68)**

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA51645W-D, Revision 2 Limitations and Conditions: (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89209-1, dated 2-23-93 is required for Piper Models PA-32-260 and PA-32-300 or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89436, dated 3-28-84 is required for Piper Model PA-32R-300 or later FAA Approved revisions of the above supplement.

4. Compatibility of this modification with other previously installed modifications must be determined by the installer.

**17 PAGE 2 OF 2 PAGES**

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code ) from (Name of grantor) (Print or type) _ (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Date of Transfer: _ Signature of grantor (In ink):.

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF-205-579

## Every issue (1)

- February 23, 1993: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e2/66/e266bfff04247a4596fe0746950689a8d73744d3b6d2556be037b60d34b87448)

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