STC SR02123SE

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

Part of the

Signature

Title 3 SR02123SE Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Federal Aviation Regulations 27 Installation of Garmin GDL 84H/88H ADS-B UAT Transceiver System in accordance with Garmin Master Drawing List GDL 84H/88H Part 27 AML STC, 005-00645-H2, Revision 1, dated July 29, 2015, or later FAA approved revision. Garmin Rotorcraft Flight Manual Supplements are: Garmin GDL 84H/88H Bell 206B, 190-01310-J1, Revision 1 dated July 29, 2015, or Garmin GDL 84H/88H Bell 206L, L-1, 190-01310-J2, Revision 1 dated July 29, 2015, or Garmin GDL 84H/88H Bell 206L-3, L-4, 190-01310-J4 Revision 1 dated July 29, 2015, or Garmin GDL 88H/88DH Bell 407, 190-01310-J3, Revision 1 dated July 29, 2015, or later FAA approved revisions. (See Continuation Sheet 3)

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

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 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) SR02123SE for approved rotorcraft models and applicable airworthiness regulations October 1, 2014 July 29, 2015 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 Description of Type Design Change (continued):

Instructions for Continued Airworthiness is: GDL 84H/88H Part 27 AML STC Maintenance Manual Contains Instructions for Continued Airworthiness, 190-01310-J0, Revision 1 dated July 29, 2015, or later FAA approved revision.

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 27-47 and are listed below.

27.1(b) Amdt 27-37; 27.301 All Amdt Orig; 27.303 Amdt Orig; 27.305 All Amdt Orig; 27.307(a) Amdt 27-26;

27.337 All Amdt 27-26; 27.561(a)(b)(3) Amdt 27-32; 27.601 All Amdt Orig; 27.603 All Amdt 27-16; 27.605(a) Amdt 27-16;

27.607 All Amdt 27-4; 27.609 All Amdt Orig; 27.610(a)(b)(c)(d) Amdt 27-46; 27.611(a)(b) Amdt Orig;

27.613(a)(b)(c)(d) Amdt 27-26; 27.771(a) Amdt Orig; 27.773(a)(1)(b) Amdt Orig; 27.777(a)(b) Amdt Orig;

27.1301 All Amdt Orig; 27.1309(a)(c) Amdt 27-46; 27.1316 All Amdt 27-46; 27.1317(a)(b)(c) Amdt 27-42;

27.1321(d) Amdt 27-13; 27.1322 All Amdt 27-11; 27.1351(a) Amdt 27-13; 27.1357(a) Amdt 27-13; 27.1365 All Amdt 27-35;

27.1367 All Amdt Orig; 27.1501 All Amdt 27-14; 27.1523 All Amdt Orig; 27.1525 Amdt 27-21; 27.1529 Amdt 27-18;

27.1541 All Amdt Orig; 27.1555(a) Amdt 27-21; 27.1559 Amdt 27-21; 27.1581(a)(b)(d) Amdt 27-14;

27.1583(e) Amdt 27-16; 27.1585(a) Amdt 27-21; B27.1 Appendix B Section VIII* Amdt 27-46

*Note: For the equipment installed under this STC, Part 27 Appendix B, B27.1 Section VIII invokes 29.1431 for Helicopter Instrument Flight

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