STC SA5161SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
February 23, 1984
Applied
May 5, 1983
Product
Aircraft · Small Airplane
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 yaw damper system model ST-164.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

tlmtri Statti of aamea Bepartmcnt of transportation—federal atriation administration Supplemental t^uje Certificate SA5161SW-D S-TEC Corporation Rt. 4-, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Ja^4Jitt^ited^4A*e£*n.'/rnee&-J<n&Ja4i*i*M>i*£fan4A^ 3 j&^rie> L "I V 1 I Air

•-/lea*6ta£u>nA,.

A-JjU PIPER PA-32-260, PA-32-300, AND PA-32R-300 Installation of S-TEC Yaw Damper System, Model ST-164, according to Bulletin No. 264, Revision 1, dated 1-16-84 and Master Drawing List No. 92190, Revision A, dated 1-16-84 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89205, dated 5-20-83 and/or later FAA Approved revisions of the above supplement.

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

5-5-83 SL^^ut^u^: 2-23-84, Revision 1 5-20-83 ' QL (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

Tkii artificatt may In transftmd in accordance with FAR 21.47.

ttnitrfl gtatts of amtrira ©epartmtnt of ^transportation— Jp cteal aoiation administration upplemental t:gpt Certificate(Continuation £heet) SA5161SW-D, Revision 1 Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89361, dated 2-23-84 and/or later FAA Approved revisions of the above supplement.

3. Compatability of this modification with other previously approved modifications must be determined by the installer.

3 years, or both.

FAA FORM sno-2-1 (1O-69) This certificate may be transferred in accordance with FAR IV. 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 £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

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