STC SA4441SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
August 6, 1981
Applied
June 11, 1981
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A13

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 single axis automatic flight guidance system model ST-043

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 Btpartmcnt of ^transportation— federal 2toiation administration Supplemental l^gpe Certificate SA4441SW Project A5364SW-DSFKP-213 S-TEC Corporation Rt. 3, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 Jifo^ufi&jciedjta^ Civil Air fjr^^na^' Jrodiict——^^i^'&er^^ca^f'^KtMn^eir-•: 3A13 Cessna R182 and TR182 „ Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-043, according to Bulletin No. 146, dated 6-8-81 and Master Drawing List 9260, dated 6-8-81, or later FAA approved revision. (28 Volt System) —

1. FAA Approved Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Cessna Models R182 and TR182 with S-TEC System 60 Single Axis Automatic Flight Control System FAA Approved P/N 8962 dated8-6-81 > is required.

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

^>^^^eMn4/^^ SXc^n^iiti^a^f-^^e' en : June 11, 1981 AURUSt 6 1981 y^Chie;

(Signature) P. Watson Chief, Engineering and Manufacturing Branch

FAA FOUM 8110-2 (10-68)

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 · 2

MakeModelData sheet
Cessna Aircraft CompanyR1823A13
Cessna Aircraft CompanyTR1823A13