STC SA5350SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 15, 1984
Applied
September 3, 1984
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A13

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-091.

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.

Umtrd .Starts of Bepartmcnt of Transportation —federal aoiation administration Supplemental l^pe Certificate SA5350SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 *>f ^a ClVll Air . si*a44 CJptajri ta 3A13 CESSNA 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M AND 182N Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-091, according to Bulletin No, 194, Revision 1, dated 9-27-84 and Master Drawing List No. 92104, Revision A, dated 9-27-84 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89116-1, dated 10-15-84 is required for Cessna Models 182H, 182J, 182K, 182L, 182M and 182N and/or later FAA Approved revisions of the above supplement.

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

r&St£ S&^n^ 9-Q3-84 10-15-84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (T,llfJ ' both. 47.

f*AfatM 8110-J(10-6«)

tinittd Srarts of Slmcrira Bepartment of ICranBportation -federal SDiarion administration Supplemental t:pe Certificate(Continuation £hcet) SA5350SW-D Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 89526, dated 10-15-84 is required for Cessna Models 182E, 182F and 182G 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' , ,i'.'-r<i!i,in (if this tertifecate is punishable by a Jim of not exceeding SlJMO, or irr:pwimrner:t nnt exceeding J years, nr />»/'' ' AA f riHM 81102-1 (1O-69) 'J hu cerlifx-.it! ma} be iran^'trttJ ir. ace •rd.irj.-t :i illi /•'.!/( -'/ / 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 9«6 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 · 9

MakeModelData sheet
Textron Aviation Inc.182E3A13
Textron Aviation Inc.182F3A13
Textron Aviation Inc.182G3A13
Textron Aviation Inc.182H3A13
Textron Aviation Inc.182J3A13
Textron Aviation Inc.182K3A13
Textron Aviation Inc.182L3A13
Textron Aviation Inc.182M3A13
Textron Aviation Inc.182N3A13