STC SA5313SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
November 21, 1988
Applied
April 6, 1984
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A21

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 two axis automatic flight guidance system, Model ST-034, with optional automatic electric trim 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 .Starts of arnica Bepartmtnt of transportation— federal atoiation administration >uppltmental 'Cgpe Certificate lfatia SA5313SW-D S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 /A*<J 3A21 Cessna 21 OK and T210K Civil Air ,7 Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-034, with Optional Automatic Electric Trim System according to Bulletin No.

137, Revision 5, dated 10-24-88 and Master Drawing List No. 9236, Revision E, dated 10-24-88 with Optional Flight Director Steering Horizon, and/or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Model T210K When Modified Per STC SA2689SW (RAM Modification) (See Continuation Sheet, Page 2, a part of this STC.)

d //i f J 4-06-84 D-U/-o4 /he'jH^^ : 8-06-85, 11-21-88, Revision 2 (Signature) Harold. W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

This certificate may be transferred in accordance with FAR 21'A7.

FAAFoiuSl 10-2(10-68)

United gtfltti of ammn Btpartmcnt of TttauBportation— .federal atnation administration Supplemental t^pe Certificate(Continuation &heet) SA5313SW-D, Revision 2 Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 8941-2, dated 8-06-85 is required for Cessna Models 210K, T210K and Model T210K When Modified Per STC SA2689SW (RAM Modification) and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplemental Flight Manual, P/N 8941-1, dated 5-07-84 is required for Cessna Models 210K and T210K and/or later FAA Approved revisions of the above supplement.

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

.•t>n alteration nf this certificate is punishable by a fine of not exceeding Sl,000, or imprisonment not exceeding 3 VMM, or both.

TAA FORM 8I10-2-! (1O-69) 7An ctrhftalt may bt transferred in accordance with l-'AK ~t •>•" 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 ZJP 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):

US. 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 · 2

MakeModelData sheet
Cessna Aircraft Company210K3A21
Cessna Aircraft CompanyT210K3A21