STC SA01356WI

Supplemental type certificate · Garmin International Inc

Holder
Garmin International Inc · United States
Status
Current · Issued
Status date
September 30, 2005
Applied
September 30, 2005
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
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 the Garmin GFC 700 Automatic Flight Control 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.

1200 East 151st Street Olathe, KS 66062

Part 23 of the Federal Aviation Regulations.

Original Product--Type Certificate Number: 3A13 Make: Cessna Model: T182T

Description of Type Design Change: Installation of the Garmin GFC 700 Automatic Flight Control System in the Cessna T182T Aircraft in accordance with Garmin Master Drawing List 005-C0263-00, Revision 1, dated September 30, 2005, or later FAA approved revisions.

1. Required baseline for this STC is a Cessna T182T equipped with a G1000 Integrated Cockpit System, approved and installed per Cessna Aircraft Company ECR No. 50797.

2. The modified aircraft must be operated in accordance with the applicable Airplane Flight Manual Supplement (AFMS) identified on the Master Drawing List (MDL).

3. The modified aircraft must be maintained in accordance with the applicable Instructions for Continued Airworthiness (ICA) identified on the MDL.

4. Compatibility of this design change with previously approved modifications must be determined by the installer.

5. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: October 27, 2004

Date of issuance: September 30, 2005 Date reissued :

( Signature) Harvey E. Nero FAA Program Manager Wichita Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number SA01356WI Date of Issuance: September 30, 2005

* Certification Basis: With respect to the modifications of this STC, the applicant has complied with the original Certification Basis 14 CFR Part 23, effective February 1, 1965, including Amendments 23-1 through Amendments 23-55, and as amended by the Amendments stated as follows; and Special Condition 23-162-SC, Protection of Systems for High Intensity Radiated Fields (HIRF), effective April 8, 2005.

14 CFR Part Amendment 14 CFR Part Amendment §23.301(a) 23-48 §23.1301(a-d) 23-20 §23.303 - §23.1309(a-f) 23-49 §23.305(a)(b) 23-45 §23.1311(a)(b(c) 23-49 §23.307(a) - §23.1321(a)(c)(e) 23-49 §23.1322(a-e) 23-43 §23.395(a)(1) 23-7 §23.1325(b)(2) 23-50 §23.397(a)(b) 23-45 §23.1327(a)(b) 23-20 §23.1329(a-h) 23-49 §23.601 - §23.1335 23-20 §23.603(a)(b) 23-23 §23.1351(a)(g) 23-49 §23.605 23-23 §23.1353(h) 23-49 §23.607 23-48 §23.1357(a-d) 23-43 §23.609(a)(b) - §23.1359(a)(b)(c) 23-49 §23.611 23-48 §23.1365(a)(b)(d)(e)(f) 23-49 §23.613(a)(b)(c) 23-45 §23.1367(a)(b)(c)(d) - §23.625(a) 23-7 §23.1381(a)(b)(c) - §23.671(a) - §23.1431(a)(b)(e) 23-49 §23.677(a)(d) 23-49 §23.1525 23-45 §23.685(a-d) 23-17 §23.1529 23-26 §23.689(a-f) 23-7 §23.1541(b)(1)(c)(2) 23-21 §23.771(a) 23-14 §23.1555(a)(b) 23-50 §23.773(a)(2) 23-45 §23.1581(a)(b)(2) 23-50 §23.777(a)(b) 23-51 §23.1581(c)(d)(f) 23-50 §23.779(a) 23-51 §23.1583(h)(m) 23-50 §23.867(a)(b) 23-49 §23.1585(j) 23-50

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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 · 1

MakeModelData sheet
The Cessna Aircraft CompanyT182T3A13