STC SA02153LA-D

Number SA02153LA-D

This certificate, issued to Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062

Part 23* of the Federal Aviation Regulations.

Original ProductType Certificate Number: *See attached Approved Model List (AML) NO. SA02153LA-D Make: dated October 26, 2012 or later FAA approved revision for list of Model: approved aircraft models and applicable airworthiness regulations.

Description of the Type Design Change: Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System in accordance with FAA approved Master Drawing List, G600 PFD/MFD System AML STC, 005-C0313-00, Revision “L”, dated October 26, 2012, or later FAA approved revision; and FAA approved Airplane Flight Manual Supplement, G600 PFD/MFD System AML STC, 190-00601-01, Revision “H” dated October 25, 2012, or later FAA approved revision.

1. Compatibility of this design chan ge 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 other person written evidence of that permission.

4. Aircraft equipped with Garmin G1000 Integrated Co ckpit System are not eligible for this STC.

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

6. Aircraft modified by this STC must be operat ed in accordance with the AFMS identified above.

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

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

(Signature) Michael Warren ODA STC Unit Administrator ODA-240087-CE Garmin International, Inc (Title)

Number SA02153LA-D

Date of Issuance: July 25, 2008 Date Amended: February 02, 2011 October 26, 2012

*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 is shown on the attached AML.

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

Regulations at the latest amendment: No Amdt through 23-61

Section Amdt Section Amdt

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

23.303 No Amdt 23.1327(a) 23-20

23.305 23-45 23.1329(h) 23-49

23.307(a) No Amdt 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)(i) 23-49

23.603 23-23 23.1353(h) 23-49

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

23.607(a)(b) 23-48 23.1359(c) 23-49

23.609 No Amdt 23.1365(a)(b)(d)(e) 23-49

23.611 23-48 23.1367 No Amdt

23.613(a)(b) 23-45 23.1381(a)(b) No Amdt

23.771(a) 23-14 23.1431(a)(b) 23-49

23.773(a)(2) 23-45 23.1501 23-21

23.777(a)(b) 23-51 23.1523 23-34

23.867 23-49 23.1525 23-45

23.1301 23-20 23.1529 23-26

23.1303(a)(b)(c)(d)(e)(f) 23-49 23.1541(a)(b) 23-21

23.1306 23-61 23.1543(b)(c) 23-50

23.1307 23-49 23.1545(a)(b)(c)(d) 23-50

23.1308(a)(b)(c) 23-57 23.1555(a)(b)(e)(2) 23-50

23.1309(a)(1)(2)(3)(b)(c)(d)(e) 23-49 23.1559(c) 23-50

23.1311 23-49 23.1581(a)(b)(c)(f) 23-50

23.1321(a)(c)(d)(e) 23-49 23.1583(h)(m) 23-50

23.1322 23-43 23.1585(j) 23-50

23.1323(a) 23-49

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