STC SA4338SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
May 6, 1981
Applied
April 22, 1981
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A12

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of S-TEC pitch stabilization system, Model ST-042

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 Bepartment of tonsportation— Jpederal 2toiation administration >upplemental 'Cgpe Certificate tJleaM£a£ A5240SW-DS S*TEC Corporation Rt. 3, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 x<£C^^^^x^^ 3 Civil Air 3A12 Cessna 172M, 172N installation of S-TEC Pitch Stabilization System, Model ST-042, according to Bulletin No. 145, dated 4/22/81 and Master Drawing List No. 9244, dated 4/22/81, or later FAA approved revision.

(14 Volt System)

1. Supplemental Flight Manual P/N 8947 FAA Approved, dated May 6, 1981, is required.

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

n^dadws^^ ^ SXc^n^fit April 22, 1981 May 6, 1981 (Signature ) P. WatsonChief, Engineering and Manufacturing Branch (Title) ~~~~~

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 Company172M3A12
Cessna Aircraft Company172N3A12