STC SA4444SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
August 13, 1981
Applied
July 27, 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 pitch stabilization system, Model ST-048 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 America Bepartment of tonsportation— federal 2toiation administration Supplemental Ttgpe Certificate SA4444SW Project A5373SW-DS FKP-213S-TEC Corporation Rt. 3, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^J'W^fte'dedjicvwfw^fo^c&oivvi^fiM^^ .<yk*^<«^^^ Civil Air 3A13 Cessna 182Q, 182R . Installation of S-TEC System 60 Pitch Stabilization System, Model ST-048 with Optional Autotrim System according to Bulletin No. 151, dated 7-27-81 and Master Drawing List No. 9263, dated 7-27-81, or later FAA approved revision. (28 Volt System) See Continuation Sheet, page 2 of this STC.

July 27, 1981 August 13, 1981 . Watson (Sismture) Chief, Engineering and Manufacturing Branch (Title) ~~~~~~

FAA FORM 81 10-2(10-68)

United States of America Bcpartmcnt of Transportation— federal atriation autministtation Supplemental ¥j)pe Certificate(Continuation 3hect) SAA444SW Limitations and Conditions:

1. Supplemental Flight Manual FAA Approved P/N 8964 dated August 13, 1981, is required for Cessna Models 1820, S/N 18266590 and Below with S-TEC System 60 Pitch Stabilization System (28 Volt System).

2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement FAA Approved P/N 8976 dated August 13, 1981, is required for Cessna Model 1820, S/N 18266591 and up with S-TEC System 60 Pitch Stabilization System (28 Volt System).

3. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement FAA Approved P/N 8967 dated August 13, 1981, is required for Cessna Hodal 182R with S-TEC System 60 Pitch Stabilization System (28 Volt System).

i. Compatibility of this modification with other previously approved modifications mist be determined by the installer.

FAA FORM 8HO-2-1 (10-69) PAGE 2 OF 2 PAGES

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 Company182Q3A13
Cessna Aircraft Company182R3A13