STC SA02119SE PAGE 2

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title 3 SA02119SE Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Federal Aviation Regulations 23 Installation of Garmin GDL 88 ADS-B UAT Transceiver System in accordance with FAA approved Master Drawing List, 005-00645-02, Revision 1, dated December 28, 2012, or later FAA approved revision; Airplane Flight Manual Supplement, 190-01310-02, Revision 1 dated December 28, 2012, or later FAA approved revision; and Instructions for Continued Airworthiness, 190-01310-01, Revision 1 dated November 21, 2012, or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. A copy of this certificate and associated AML, plus AFMS and ICA 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 a product, the holder must give the other person written evidence of that permission.

(See Continuation Sheet 3) Michael Warren, ODA STC Unit Administrator ODA-240087-CE, Garmin International, Inc.

See Approved Model List (AML) SA02119SE for approved airplane models and applicable airworthiness regulations October 22, 2015 February 21, 2011 December 28, 2012 Multiple - AML STC

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of

3 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 are at the latest amendment: Orig. through 23-61 and are listed below.

23.301(a) Amdt 23-48; 23.303 No Amdt; 23.305 All Amdt 23-45; 23.307(a) No Amdt; 23.337 All Amdt 23-48;

23.561(b)(3)(e) Amdt 23-48; 23.601 No Amdt; 23.603 All Amdt 23-23; 23.605(a) Amdt 23-23; 23.607(a)(b) Amdt 23-48;

23.609 All No Amdt; 23.611 Amdt 23-48; 23.613(a)(b) Amdt 23-45; 23.627 No Amdt; 23.771(a) Amdt 23-14;

23.773(a)(2) Amdt 23-45; 23.777(a)(b) Amdt 23-51; 23.1301(a)(b)(c)(d) Amdt 23-20; 23.1306(b) Amdt 23-61;

23.1308(c) Amdt 23-57; 23.1309(a)(1)(2)(3)(b)(1)(2)(ii)(3)(4)(c)(1)(e) Amdt 23-49; 23.1321(e) Amdt 23-49;

23.1322 All Amdt 23-43; 23.1331(a)(b)(1) Amdt 23-43; 23.1351(a)(1)(2)(i) Amdt 23-49; 23.1353(h) Amdt 23-49;

23.1357(a)(b) Amdt 23-43; 23.1359(c) Amdt 23-49; 23.1365(a)(b)(d)(e) Amdt 23-49; 23.1367(a)(c)(d) No Amdt;

23.1381(a)(b) No Amdt; 23.1431(a)(b) Amdt 23-49; 23.1501(a)(b) Amdt 23-21; 23.1529 All Amdt 23-26;

23.1541(a)(2)(b) Amdt 23-21; 23.1555(a)(b)(e)(2) Amdt 23-50; 23.1581(a)(b)(c)(f) Amdt 23-50; 23.1583(h)(m) Amdt 23-50;

23.1585(j) Amdt 23-50

Note 1) For installations of this STC, as amended October 22, 2015 or later, the certification basis has been updated to include the regulations listed below. The added regulations are for changes associated with installation of Flight Stream 110/210 LRU.

23.853(a)(f) Amdt 23-62

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