STC SA4692SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 4, 1982
Applied
May 7, 1982
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A13

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 Two Axis Automatic Flight Guidance System, Model ST-110 with optional Autotrim System and with optional Flight Director Steering Horizon.

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.

Uratrt £tatt» of antrica department of ^Transportation -federal atnation administration Supplemental t^pe Certificate *sbum*vw SA4692SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 f^jA^^^ Civil Air 2A13 Piper PA-28-140, PA-28-150, PA-28-180, S/N 28-1 through S/N 28-7205318; PA-28-235, S/N 28-10003 through S/N 28-7210023 Installation of S-TEC System 60 Two Axis Automatic Flight Guidance Syatem, Model ST-110 with Optional Autotrim System according to Bulletin No. 213, dated 5-05-82 and Master Drawing List No. 92118, dated 5-05-82 with Optional Flight Director Steering Horizon; or according, to FAA approved revision. (14 Volt System) See Continuation Sheet, page 2, of this STC.

•<0aA^fe>^J<^^wvfWwAnM&A^0naxW;iW'&S!ic£Min&v* May 7, 1982 June 4, 1982 Don P. WatSOn ^~ (Signature) Manager, Aircraft Certification Division Southwest Region

TAu artifieate may be transfemd in accordance with FAR 21.47.

FAA raw si 10-2 (10-68)

ttnittd States of America Bepartment of transportation— federal Sttation administration Supplemental Itjipe Certificate(Continuation &heet) SA4692SW Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89137 dated 6-4-82, is required for Piper Model PA-28-140, PA-28-150, PA-28-160, PA-28-180, S/N 28-1 through S/N 28-7205318 and PA-28-235, S/N 28-10003 through S/N 28-10719 with S-TEC System 60 Two Axis Automatic Flight Guidance System; OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89138 dated 6-4-82, is required for Piper Models PA-28-235 S/N 28-10720 through S/N 28-7210023 with S-TEC System 60 Two Axis Automatic Flight Guidance System without au tot rim.

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

3. Eligible on Piper Model PA-28-180, S/N 28-1 through S/N 28-7205318, Only;

eligible on Piper Model PA-23-235, S/N 28-10003 through S/N 28-7210023, Only;

also eligible on Piper Models PA- 28-140, PA-28-150.

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

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (Cify, State, and ZJP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and %1P 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-28-1402A13
Piper Aircraft Inc.PA-28-1502A13
Piper Aircraft Inc.PA-28-1802A13
Piper Aircraft Inc.PA-28-2352A13