STC SA4632SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
August 3, 1982
Applied
February 17, 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-068 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.

Baited gtatcs or amtrica Bepartment of transportation—federal Stoiation administration Supplemental t^pe Certificate <-SleaM/a&&nA/.

SA4632SW Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^^^^•a4l^^^,<^^!&«^^^ o^^^w.^.^w^^^^^i^w^^^^/^K/ 23 y^5^Federal Aviation A16CE Cessna : 207A, T207A , „, p „ ^.Installation of S-TEC System 60 Pitch Stabilization System, Model ST-068 with Optional Autotrim System according to Bulletin No. 171, Revision 1 dated 4-01-82 and Master Drawing List No. 9299, Revision A, dated 4-01-82; or later FAA Approved revision. (28 Volt System) See Continuation Sheet, Page 2, of this STC.

s£ev><^^ S^c^mim^t^a^o^^^e' ™: February 17, 1982 March 22, 1982 August 3, 1982 Revision 1 (ffl Ji- f #^/d/WjKvrecS^&n/sfx/A P. Watson Aircraft Certification DivisionSouthwest Region (Title)

tinted States of amtrira Bcpartment of transportation— federal 2toiation administration Supplemental t;gpe Certificate(Continuation £heet) SA4632SW Revision 1 Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89112 dated 3/22/82 is required for Cessna Models 207A and T207A with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89112-1 dated 8/3/82 is required for Cessna Modeh 207A and T207A S/N 20700483 and UP with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplemental Flight Manual P/N 89122 dated 8/3/82 is required for Cessna Models 207A and T207A S/N 20790363 through S/N 20700482 with S-TEC System 60 Pitch Stabilization System.

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

FAA FORM 8110-2-1 (1O-69) PAGE 2OF 2PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^IP 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 · 2

MakeModelData sheet
Cessna Aircraft Company207AA16CE
Cessna Aircraft CompanyT207AA16CE