STC SA5218SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 6, 1983
Applied
August 31, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 1, Part 21
Data sheet
TCDS3A17

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-207-40/50.

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.

ttnod goto Btpartmcnt of transportation—federal atriation administration Supplemental 'Cgpe Certificate SA5218SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 3 -cd^kf ClVll Air dr*aen&t *Jfocu&c£ — — •.S'ufiC' ~&e*£u!tca£e\/u*mc«i* •' J M 1 / CESSNA 172RG Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-207-40/50, according to Bulletin No. 307, dated 8-10-83 and Master Drawing List No. 92226, dated 8-10-83 and/or later FAA Approved revisions of the above data, (28 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/ or FAA Approved Airplane Flight Manual, P/N 89281, dated 10-6-83 is required for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC).

><!^^ SX£&n*ni&&a£rr-*J' • & ' 8-31-83 10-6-83 (Signalurt) Harold W, Holdeman DAS Staff Coordinator, DAS 5 SW (Titlt)

This certificate may bt transferred in accordance with FAR 21.47.

FAA POM II10-J ()0-6«|

ttrattdgtattsofamcrica Bepartment of ^Transportation— Jftteal Sttn'ation Administration Supplemental t^pe Certificate(Continuation £heet) SA5218SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89282, dated 10-6-83, is required for S-TEC System 50, and/or later FAA Approved revisions of the above supplement.

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

.-1 rc v alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

FAA FORM stio-2-1 (1O-69) This certificate may be transferred in accordance ivith FAR i'1.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, Stale, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <XP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

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 · 1

MakeModelData sheet
Cessna Aircraft Company172RG3A17