STC SA5124SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
October 27, 1989
Applied
October 15, 1982
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 System 60 single axis automaticflight guidance system Model ST-094.

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.

+frtti Bepartmtnt of transportation —federal atriation administration Supplemental 'Cgpc Certificate iSiU'mvep' SA5124SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 -^-^ejii^v^***^,*™^ ClVll Air 3A12 Cessna 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 1721, 172K and 172L Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-094, according to Bulletin No. 197, Revision 2, dated 10-03-89 and Master Drawing List No. 92145, Revision B, dated 10-03-89 and/or later FAA Approved revisions of the above data (14 Volt System).

Also eligible on the above listed models when modified per STC SA420CE (Lycoming Engine, 0-360-A1D, 180 H.P.).

FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89161, dated 12-2-82 is required and/or later FAA Approved revisions of the above supplement.

Continuation Sheet, Page 2, a part of this STC.

&f*rnt^ SXc/rrUruA **: 10-15-82 12-2-82 10-27-89, Revision 1 (Signalure) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW

This certificate may be transfcrrtJ in acnrjana with FAR 21.17.

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ttnitrd £tatu of amtrira Bcpartmtnt of transportation— Jpedcral aoiation administration Supplemental HTgpe Certificate(Continuation £heet) SA5124SW-D, Revision 1 Limitations and Conditions (con't.)

3. FAA Approved Supplemental Flight Manual, P/N 89161-1, dated 10-27-89 is required and/or later FAA Approved revisions of the above supplement.

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

altrratinn nf this certificate i'j punishable by a fine of not exceeding SI, OOP, or imprisonment not exceeding 3 years, or hnih.

FORM aiio-2-i (10-69) Tf,is certificate may be transferred in accordance with l-'Ali J/.-I7 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 ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : I 966 OF —305-579

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 · 12

MakeModelData sheet
Cessna Aircraft Company1723A12
Cessna Aircraft Company172A3A12
Cessna Aircraft Company172B3A12
Cessna Aircraft Company172C3A12
Cessna Aircraft Company172D3A12
Cessna Aircraft Company172E3A12
Cessna Aircraft Company172F (USAF T-41A)3A12
Cessna Aircraft Company172G3A12
Cessna Aircraft Company172H (USAF T-41A)3A12
Cessna Aircraft Company172I3A12
Cessna Aircraft Company172K3A12
Cessna Aircraft Company172L3A12