# STC SA01356WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Garmin International Inc, United States
- Description: Installation of the Garmin GFC 700 Automatic Flight Control System.
- Applied: September 30, 2005
- Status date: September 30, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/37/e0/37e0a588ae54d545361fa2e5fd81f60f57a28215a841345158bd9f416a33b9a3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8EF65294C8F8A3AA8625712B006AAB53.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01356WI

## ADs that name it (0)

None.

## Approved models (1)

- The Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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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## Every issue (1)

- September 30, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/37/e0/37e0a588ae54d545361fa2e5fd81f60f57a28215a841345158bd9f416a33b9a3)

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