STC SA02015SE-D

Part 23* of the Federal Aviation Regulations.

Original Product--Type Certificate Number: *See attached Approved Model List (AML) No. SA02015SE-D Make: dated February 5, 2014 or later FAA-approved revision for list of Model: approved aircraft models and applicable airworthiness regulations.

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, 005-00570-13, Revision 13 dated February 5, 2014, or later FAA approved revision; Airplane Flight Manual Supplement, G500 PFD/MFD System AML STC, 190-01102-01, Revision 9 dated February 4, 2014, or later FAA approved revision; and G500 PFD/MFD System Instructions for Continued Airworthiness, 190-01102-00, Revision 5 dated December 11, 2012, or later FAA approved revision.

Later FAA-approved revisions to the data listed above are incorporated without further amendment to this STC.

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 other person written evidence of that permission.

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

Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Date of application: June 3, 2009

Date of issuance: July 30, 2009

Date amended: February 23, 2011, January 23, 2013, February 5, 2014

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

(Title)

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 granter) Print or type

(Address of granter) (Number and street)

(City, State and Zip code)

Signature of grantor (In Ink):

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA02015SE-D

Date of Issuance: July 30, 2009 Date Amended: February 23, 2011, January 23, 2013, February 5, 2014

*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(a)(b) 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(a)(b)(c) 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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