STC SA01818WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

This certificate issued to: Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 SA01818WI Part 23* of the Federal Aviation Regulations.

Multiple - AML STC Make:

Model: See Approved Model List (AML) SA01818WI for approved aircraft models and applicable airworthiness regulations

Installation of Garmin G5 Electronic Flight Instrument Data Required:

(1) Garmin Master Drawing List (MDL) 005-01112-01, Revision 1, dated July 22, 2016

(2) Garmin G5 STC Maintenance Manual including ICA190-01112-11, Revision 1, dated July 22, 2016

(3) Garmin G5 Airplane Flight Manual Supplement 190-01112-13, Revision 1, dated July 22, 2016 Later FAA-approved revisions to the data listed above are incorporated without amendment to this certificate Limitations and Conditions:

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

(2) The installation of the G5 requires the retention of the mechanical airspeed indicator, altimeter, and vertical speed indicator. The installation of the G5 in configurations not approved by this STC, such as an electronic standby instrument, requires separate airworthiness approval.

(3) For installations in aircraft approved for IFR operations:

(a) If the G5 is installed as the primary attitude indicator, the existing rate of turn indicator must be retained.

(b) If the G5 is installed as the rate of turn indicator, the existing primary attitude indicator must be retained.

(continued on Page 3)

Date of Application: May 5, 2016 Date of Issuance: July 22, 2016 Date Reissued:

Date Amended: Apr 28, 2017; Oct 18, 2017; Mar 15, 2019, Jul 19, 2019, Sep 28, 2021

Signature

Title Paul Mast ODA STC Unit Administrator ODA-240087-CE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 3 of 3 FAA Form 8110-2 (5/14)

Limitations and Conditions (Cont.)

(Continuation Sheet) Number: SA01818WI September 28, 2021

(4) For installations in aircraft approved for VFR-only operations, the G5 can be installed as the attitude indicator and rate of turn indicator without retention of either the existing attitude indicator or rate of turn indicator.

(5) Aircraft modified by this STC must be operated in accordance with the Airplane Flight Manual Supplement (AFMS) identified above.

(6) Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) identified above.

(7) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

(8) Unless a limitation is shown on the Approved Model List (AML), installations performed in accordance with MDL Revision 14 or later, or modified by Service Bulletin 1910, comply with 14 CFR 23.2515(a)(b) and 23.2520(a)(b), Amdt. 23-64, and are compatible with Garmin G3X and FIKI systems.

*Certification Basis Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change remains unchanged from the original approval.

b. The certification basis for parts changed or affected by this change is:* Section Amdt. Section Amdt.

23.251(a) 23-62 23.1323(a)(b)(c) 23-62

23.301(a) 23-48 23.1325(a)(b) 23-50

23.303 Orig. 23.1327(a)(1)(2) 23-20

23.305(a)(b) 23-45 23.1329(g)(h) 23-49

23.307(a) Orig. 23.1331(a)(b)(1)(c) 23-62

23.337(a)(b) 23-48 23.1351(a) 23-49

23.561(a)(b)(3)(e) 23-62 23.1353(h) 23-62

23.601 Orig. 23.1357(a)(b)(c)(d) 23-43

23.603 23-23 23.1359 23-49

23.605(a) 23-23 23.1365(a)(b)(d)(e) 23-49

23.607(b) 23-48 23.1381(a)(b) Orig.

23.613(a)(b) 23-45 23.1419(a)(c) 23-43

23.771(a) 23-14 23.1431(a)(b) 23-62

23.773(a)(2) 23-45 23.1529 23-26

23.777(a)(b) 23-62 23.1541 23-21

23.853(a) 23-62 23.1543(b) 23-50

23.867(a)(b) 23-49 23.1545(a)(b)(c) 23-62

23.1301 23-62 23.1555(a)(b) 23-62

23.1303(a)(b)(c)(f) 23-62 23.1581(a)(b)(d)(f) 23-50

23.1307 23-49 23.1585(a) 23-62

23.1309(a)(1)(2) 23-62 23.2010(a)(b) 23-64

23.1309(a)(b)(c)(d)(e) 23-49 23.2510 23-64

23.1311(a)(1)(2)(3)(6)(7)(b) 23-62 23.2515(a)(b) 23-64

23.1321(c)(d)(e) 23-49 23.2520(a)(b) 23-64

23.1322 23-43 23.2335 23-64 *Earlier amendments may apply to certain models; refer to the AML.