STC SA4511SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 20, 1981
Applied
September 24, 1981
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A21

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 Model ST-039 with optional autotrim

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 Starts of amtrica Bepartment of transportation— federal atnation administration Supplemental t:gpe Certificate ^l«att/a/tc-m^.

SM511SW Pr°ject FKP-213 S-TEC Corporation Route 4, Building 946 Wolters Industrial Complex Mineral Wells, Texas 76067-9990 x<^^/t^<z4l^^ 3 ^J&e, Civil Air 3A21 Cessna 210K, T210K Installation of S-TEC System 60 Pitch Stabilization System, Model ST-039 with Optional Autotrira System according to Bulletin No. 142, dated 9-24-81 and Master Drawing List No. 9247, dated 9-24-81, or later FAA approved revision. (14 Volt System) FAA Approved Supplemental Flight Manual P/N 8948 dated 10/20/81 is required for Cessna Models 210K and T210K with S-TEC System 60 Pitch Stabilization System (14 Volt System).

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

^: September 24, 1981 . October 20, 1981 (Signature) ^™ J. Watson Chief, Engineering and Manufacturing Branch (Title)—————————————————

This certificate may be transferred in accordance with FAR 21 .47.

FAA FOMI 81 10-2 (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 Company210K3A21
Cessna Aircraft CompanyT210K3A21