STC SA02153LA-D PAGE 1

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02153LA-D This certificate issued to: Garmin International, Inc.

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

Original Product -- Type Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA02153LA-D for approved Model: aircraft models and applicable airworthiness regulations.

Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System in accordance with Master Drawing List, G600 PFD/MFD System AML STC, 005-C0313-00, Revision G, dated February 01, 2011, or later FAA approved revision; Airplane Flight Manual Supplement, G600 PFD/MFD System AML STC, 190-00601- 01, Revision E dated January 28, 2011, or later FAA approved revision; and G600 PFD/MFD System Instructions for Continued Airworthiness, 190-00601-00, Revision F dated December 16, 2010, or later FAA approved revision.

Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System in accordance with Master Drawing List, G500 PFD/MFD System AML STC, 005-C0313-10, Revision 1, dated April 01, 2015, or later FAA approved revision; Airplane Flight Manual Supplement, G500/G600 PFD/MFD System AML STC, 190- 00601-01, Revision K dated April 01, 2015, or later FAA approved revision; and G500/G600 PFD/MFD System Instructions for Continued Airworthiness, 190-00601-00, Revision L dated April 01, 2015, or later FAA approved revision.

Required data for TBM 700/850 RVSM group airworthiness approval are: the G600 data listed above; plus, Airplane Flight Manual Supplement TBM 700/850 G600 RVSM, 190-00601-34, Revision 2 dated December 13, 2013, or later approved revision.

(See Continuation Sheet on Page 3)

Date of Application: January 31, 2006 Date Reissued: September 15, 2009 Date of Issuance: July 25, 2008 Date Amended: February 02, 2011; October 26, 2012;

December 16, 2013; April 01, 2015; November 17, 2016; August 30, 2018 FEDERAL AVIATION By Direction of the Administrator Cink Frisk (Signature) TOMINSTRATO Erik Frisk, ODA STC Unit Administrator ODA-240087-CE, Garmin International, Inc.

(Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplement Type Certificate Number To (Name of Transferee) (Address of Transferee) (Number and street) (City, State and Zip code) From (Name of Grantor) (Print or type) (Address of Grantor) (Number and street) (City, State and Zip code) Extent of Authority (if licensing agreement):

Signature of Grantor (In Ink):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02153LA-D Ssued: July 25, 2008 Reissued: September 15, 2009 Amended: February 02, 2011, October 26, 2012, December 16, 2013, April 01, 2015, November 17, 2016;

August 30, 2018 Limitations and Conditions:

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

2. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the

4. Aircraft equipped with Garmin G1000/G950 Integrated Cockpit System are not eligible for this STC.

5. Aircraft equipped with Rockwell Collins ProLine 21 Integrated Avionics System are not eligible for this STC.

Certification Basis:

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

The certification basis for parts not changed or not affected by this change is shown on the attached AML.

b. The certification basis for parts changed or affected by this change is: No Amdt through 23-64.

Section Amdt Section Amdt

23.301(a)(b)(c) 23-48 23.1325(b)(1)(2) 23-50

23.303 Orig 23.1327(a) 23-20

23.305 23-45 23.1329(h) 23-49

23.307(a) Orig 23.1331(a)(b)(1) 23-43

23.337 23-48 23.1335 23-20

23.561(a)(b)(3) 23-48 23.1351 (a)(1)(2)(1) 23-49

23.601 Orig 23.1353(h) 23-49

23.603 23-23 23.1357(a)(b)(d) 23-43

23.605(a) 23-23 23.1359(c) 23-49

23.607(a)(b) 23-48 23.1365(a)(b)(d)(e) 23-49

23.609 Orig 23.1367 Orig

23.611 23-48 23.1381 (a)(b) Orig

23.613(a)(b) 23-45 23.1431(a)(b) 23-49

23.771(a) 23-14 23.1501 23-21

23.773(a)(2) 23-45 23.1523 23-34

23.777(a)(b) 23-51 23.1525 23-45

23.853(a) 23-62 23.1529 23-26

23.867 23-49 23.1541(a)(b) 23-21

23.1301 23-20 23.1543(b)(c) 23-50

23.1303(a) (b)(c)(d) (e)(f) 23-49 23.1545(a) (b)(c)(d) 23-50

23.1307 23-49 23.1555(a) (b)(e)(2) 23-50

23.1308(a)(b)(c) 23-57 23.1559(c) 23-50

23.1309(a)(1)(2)(3)(b)(c)(d)(e) 23-49 23.1581 (a) (b)(c)(t) 23-50

23.1311 23-49 23.1583(h)(m) 23-50

23.1321 (a)(c)(d)(e) 23-49 23.1585(j) 23-50

23.1322 23-43 23.2515 23-64

23.1323(a) 23-49 -END-