STC SA5164SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
February 23, 1993
Applied
May 12, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA3SO

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of S-TEC System 60 pitch stabilizer system Model ST-163 with optional automatic electric trim system.

What the certificate saysOCR

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
Piper Aircraft Inc.PA-32-260A3SO
Piper Aircraft Inc.PA-32-300A3SO
Piper Aircraft Inc.PA-32R-300A3SO