STC SA5237SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
August 6, 1985
Applied
November 2, 1983
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 5, 2025.

What it approves

Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-033.

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.

Hratrfl States of awrica

•Department of tonsportation—JWeral Stoiation administration Supplemental l^pe Certificate <suvrn&€V' SA5237SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 n&t *n *n .<mce& -foe jtvt*uxn*£r>jineaA'A*t&u4r«tnen& ^f iXioW ••> M^nt L 1 V 1 I Air f sffttitftf-fiCnA .

3 A 2 1 CESSNA 210G, T2106, 210H, T210H, 210J, T210J, 210K AND T210K ^Z^eAertAAm d^/yJu-z *A&a-rt 'GlAa-nM •' Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-033, according to Bulletin No, 136, Revision 2, dated 6-18-85 and Master Drawing List No. 9238, Revision B, dated 6-18-85 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Models T210G, T210H, T210J and T210K when modified per STC SA2689SW (RAM Modification), (See Continuation Sheet, Page 2, a part of this STC,) J!/^ ^e<r<m4#^^ SZarnini&traS-irr-jf^e 11-2-83 <U**e**u~J: 8-06-85, Revision 1 11-11-83 (Signature I Id W. "-1Harold w. Holdeman DAS Staff Coordinator, DAS 5 SW (Titlt)

i certificate may be l-staftrrtd in accordance with FAR 21.47.

FAA font iMO-J (10-«l)

ttnitrd &tatts of amenta Bepartment of ^Transportation -federal auiation administration Supplemental HTgpe Certificate(Continuation &heet) SA5237SW-D, Revision 1 Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 8940-2, dated 8-06-85 is required for Cessna Models 210K and 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 89370-1, dated 8-06-85 is required for Cessna Models 210G, T210G, 210H, T210H, 2100, T210J and Models T210G, T210H and T210J when modified per STC SA2689SW (RAM Modification) and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 8940-1, dated 11-11-83 is required for Cessna Models 210K and T210K and/or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 89370, dated 11-11-83 is required for Cessna Models 2106, T210G, 210H, T210H, 210J and T210J and/or later FAA Approved revisions of the above supplement.

6. Compatability of this modification with other previously approved modifv cations must be determined by the installer, iitum of this certificate is punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or hnih f ORM Biio-2-1 tio-69) This certificate may be transjentd in accordance with i'AR -7.7" PAGE 2 OF 2 S

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <7P cade) 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 · 8

MakeModelData sheet
Cessna Aircraft Company210G3A21
Cessna Aircraft Company210H3A21
Cessna Aircraft Company210J3A21
Cessna Aircraft Company210K3A21
Cessna Aircraft CompanyT210G3A21
Cessna Aircraft CompanyT210H3A21
Cessna Aircraft CompanyT210J3A21
Cessna Aircraft CompanyT210K3A21