STC SA5217SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
May 8, 1986
Applied
September 6, 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 6, 2025.

What it approves

Installation of S-TEC System 60 two axis automatic flight guidance system, Model ST-226, 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.

Unitri gtatti Bepartment of transportation—federal atnation Administration Supplemental t:uje Certificate SA5217SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 n&£ A/n ^n^/ ^Mf>^* fTfd-t-ojT (T/ ^<7 'SM&Attvwrv&ritbrf*S&9*{ O s&^A* LlVl I Al T (jr^at no* iJiwaue/ —— •Ify^if'dei^^iCa^e'^yutmoef'- 3A21 CESSNA 210G, T210G, 210H, T210H, 210J AND T210J Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-226, with Optional Automatic Electric Trim System according to Bulletin No. 326, Revision 3, dated 5-02-86 and Master Drawing List No.

92238, Revision C, dated 5-02-86 with Optional Flight Director/Steering Horizon and/or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Cessna Models T210G, T210H and T210J when modified in accordance with STC SA2689SW (RAM Modification).

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

J<!*^^ JSdkttnt&Aa&r-^^Sb- & / 9-06-83 2L&,~*A~~t: 11-21-84, 8-05-85, 5-08-86, Revision 3 ^^yiu«-~»..- 10-07-83 QL&^t (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (TitU)

Tkit artificaU mmy kt /r«u/4n»rf in ttatouKt with FAR 21,47.

ttmtrd 3tatu of amcrira Bepartmcnt of fensportation— jpederal aoiation administration Supplemental IKgpe Certificate(Continuation &heet) SA5217SW-D, Revision 3 Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 89327, dated 10-07-83 is required for Cessna Models 210G, T210G, 210H, T210H, 210J and T210J and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplemental Flight Manual, P/N 89327-1, dated 8-05-85 is required for Cessna Models 210G, T210G, 210H, T210H, 210J, T210J and Models T210G, T210H and T210J when modified in accordance with STC SA2689SW (RAM Modification) 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.

.•I'd- alteration of this certificate is punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or both.

' AA FORM eiio-2-i (to-69) This certificate may be transferred in accordance with l:AU :.'/.-/.7 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 <7/> 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 · 6

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