STC SA4734SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
August 3, 1982
Applied
March 24, 1982
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA16CE

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-071 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 $tatcs of amrrita Bepartmcnt of Transportation —.federal Situation administration Supplemental Ituje Certificate SA4734SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, IX 76067 wJtifa'£ySi&deAMpmf^-&&f<>t£c>t^ Afl£4^MdA^y^v4>w/h^ee&Jfi&^a*wvw 23 <Sl£&Mta£&nA'.

Federal Aviation

••' A16CE : Cessna 207, T207, 207A, T207A . installation of S-TEC System 60 Pitch Stabilization System, Model ST-071, with Optional Autotrim System according to Bulletin No. 174, dated 2-22-82 and Master Drawing List No. 92100, dated 2-22-82, or later FAA approved revision. (14 Volt System) : See Continuation Sheet, page 2, of this STC.

March 24 1982 AUBUSt 3 1982 *\*r /(Signature) Don P. Watson/ Manager, Aircraft Certification Division

FAA FO«M tl 10-7 (10-68)

tinted gtatrs Bcpartment of 'Cransportation—federal aoiation administration Supplemental ICgpe Certificate(Continuation £httt) tSVMWWeW SA4734SW Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89113, dated 8-3-82, is required for Cessna Models 207A and T207A, S/N 20700483 and UP with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplemental Flight Manual, P/N 89136, dated 8-3-82, is required for Cessna Models 207, T207, 207A, and T207A S/N 20700363 thru S/N 20700482 with S-TEC System 60 Pitch Stabilization System installed.

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

FAA FORM B110-2-1 (10-69) PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <7/> code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <7P 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
Cessna Aircraft Company207A16CE
Cessna Aircraft Company207AA16CE
Cessna Aircraft CompanyT207A16CE
Cessna Aircraft CompanyT207AA16CE