STC SA4644SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
July 7, 1982
Applied
February 4, 1982
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 60 pitch stabilization system, Model ST-087 with optional Autotrim System

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.

United States of amtrica Bepartmcnt of transportation—federal Situation administration Supplemental 'Cgpe Certificate <sltaMta£&nA.

fJrtairuid \Jrvetuet SA4644SW S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 \/n&<Jufie's£tedjjctrtvf^JSt&f<>t6eurtm JfoM&i*ve>i& 3 Civil Air 2A13 Piper PA-28-151, PA-28-161, PA-28-181, PA-28-236 ': installation of S-TEC System 60 Pitch Stabilization System, Model ST-087 with optional Autotrim System according to Bulletin No. 190, Revision 1, dated 4-21-82 and Master Drawing List No. 9293, Revision A, dated 4-21-82, or later FAA approved revision. (14 Volt System) gee Continuation Sheet, page 2, of this STC.

^ February 4, 1982 April 5, 1982 July 7, 1982 Revision 1 (Signature) Manager, Aircraft Certification DivisionSouthwest Region (Titlt)

FAA Font 8110-2 (IO-68)

ttnittd &tatu of amtrira Bepartment of "Cransportation— $ Edcral Sttation administration Supplemental l^gpe Certificate(Continuation £heet) SA4644SW Revision 1 Limitations and Conditions:

FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89107 dated 4/5/82, is required for Piper Models PA-28-151, S/N 78-7615001 and UP, PA-28-161, and PA-28-181 with S-TEC Pitch Stabilization System installed;

OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89107-1 dated 7-7-82, is required for Piper Model PA-28-151, PA-28-161, PA-28-181, and PA-28-236 with S-TEC System 60 Pitch Stabilization System installed.

2. Compatibility of this modification with other previously approved modifications must be determined by the installer.

FAA FORM 8110-2-1 (1O-69) PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name oj transferee) (Address of transferee) (Number and street) ( City, Slate, 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):

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 · 4

MakeModelData sheet
Piper Aircraft Inc.PA-28-1512A13
Piper Aircraft Inc.PA-28-1612A13
Piper Aircraft Inc.PA-28-1812A13
Piper Aircraft Inc.PA-28-2362A13