STC SA01714WI

Part 23* of the Federal Aviation Regulations.

Original Product--Type Certificate Number: * See attached Approved Model List (AML) No.

SA01714WI dated May 1, 2013 or later FAA- approved revision for list of approved aircraft models and applicable airworthiness regulations.

Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.

Data Required:

(1) Garmin Master Drawing List (MDL) 005-00734-04, Revision 1, dated May 1, 2013 or later FAA-approved revision.

(2) Garmin Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual (AFMS), 190-00734-15, Revision 1, dated May 1, 2013 or later FAA-approved revision.

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

(2) Aircraft installations involving the Garmin transponder GTX 33/33D/330/330D models require the previous installation of an approved ADS-B position source. Refer to the design data specified in the Master Drawing List (MDL) listed above for specific hardware and software requirements.

(3) Aircraft installations involving the Garmin transponder GTX 335/335R/345/345R models without an optional internal GPS require the previous installation of an approved ADS-B position source. Refer to the design data specified in the Master Drawing List (MDL) listed above for specific hardware and software requirements.

Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Date of application: August 7, 2012

Date of issuance: May 1, 2013

Date amended: April 29, 2014, March 8, 2016

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

(Title)

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

Transfer the ownership of Supplement Type Certificate Number

To (Name 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 SA01714WI Date of issuance: May 1, 2013 Date Amended: April 29, 2014, March 8, 2016 Limitations and Conditions (continued):

(4) Aircraft with G950 or G1000 display systems are limited to Garmin transponder GTX 335R/345R models; see Table II of the attached AML. Refer to the design data specified in the Master Drawing List (MDL) listed above for specific hardware and software requirements.

(5) Aircraft modified by this STC must be operated in accordance with the Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual (AFMS) identified above.

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

(7) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

*Certification Basis Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the cert ification 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:

Section Amdt Section Amdt Section Amdt

23.301 a 23-48 23.773 a(2) 23-45 23.1357 a, b, c, d 23-43

23.303 Original 23.777 a, b 23-62 23.1359 c 23-49

23.305 23-45 23.853 a 23-62 23.1365 a, b, d, e 23-49

23.307 a Original 23.863 a, b 23-34 23.1367 a, b, c, d Original

23.337 23-48 23.1301 a, b, c 23-62 23.1431 a, b 23-62

23.561 b(3), e 23-62 23.1306 a, b 23-61 23.1501 a, b 23-21

23.601 Original 23.1307 23-49 23.1525 23-45

23.603 23-23 23.1308 a, b, c 23-57 23.1529 23-26

23.605 a 23-23 23.1309 a(1)(2),b, c, d 23-62 23.1555 a, b, e(2) 23-62

23.607 a, b 23-48 23.1310 23-62 23.1581 a, b, c, f 23-50

23.611 23-48 23.1311 a(2) 23-62 23.1583 h, m 23-62

23.613 a, b 23-45 23.1322 b, d, e 23-43 23.1585 j 23-62

23.627 Original 23.1351 a 23-49 ----- ----

23.771 a 23-14 23.1353 h 23-62 ----- ---- ------------------------------------------------END------------------------------------------------