STC SA02571SE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 3 SA02571SE Federal Aviation Regulations23 See Approved Model List (AML) SA02571SE for approved aircraft models and applicable airworthiness standards.

Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Data required includes Garmin Master Drawing List (MDL) 005-00795-C2 Revision 1, dated November 17, 2017 or later FAA-approved revision; Garmin Airplane Flight Manual Supplement (AFMS) 190-01717-B2 Revision 1, dated November 17, 2017 or later FAA-approved revision; Additional Garmin AFMS for the Socata TBM 700/850 (to address RVSM aspects) 190-01717-B4 Revision 1, dated November 17, 2017 or later FAA-approved revision; Garmin Maintenance Manual (Includes Instructions for Continued Airworthiness (ICA)) 190-01717-B1 Revision 1, dated November 17, 2017 or later FAA-approved revision.

(1) The installer must determine whether this design change is compatible with previously installed modifications.

(2) 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.

(3) A copy of this certificate, the approved AFMS, and the approved ICA must be maintained as part of the permanent records for the modified aircraft.

(See Continuation Sheet on Page 3) August 5, 2015 November 17, 2017 Multiple - AML STC December 5, 2018; June 25, 2019; November 26, 2019; October 26, 2020; July 9, 2021; February 2, 2022; January 25, 2023; December 12, 2023 JR Brownell ODA STC Unit Administrator ODA-240087-CE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

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

3 SR02295LASA02571SE Amended: December 12, 2023 Limitations and Conditions (continued):

(4) Equivalent Level of Safety Findings have been made for the following regulations (also indicated below with an asterisk): 14 CFR 23.777(a), 23.1301(b), and 23.1555(a)(b) (documented in ELOS Memo ST12743SE-A-S-1).

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:

Section

23.301 (a)

23.303 (All)

23.305 (All)

23.307 (a)

23.337 (All)

23.561 (a)(b)(3)

23.601

23.603 (All)

23.605 (a)

23.607 (a)(b)

23.609 (All)

23.611 (All)

23.613 (a)(b)(c)

23.627

23.771 (a)

23.773 (a)(2)

23.777 (a)*(b)

23.853 (a)

23.863 (a)(b)

23.867 (a)(b)(c)

23.901 (a)(1)(2)(b)(1)(2)(e)

23.903 (b)(2)(c)

23.954 (a)(b)†

23.955 (a)(2)(3)(4)(b)(c)

23.963 (e)

23.993 (All) Amdt.

23-48 Original 23-45 Original 23-48 23-62 Original 23-23 23-23 23-48 Original 23-48 23-45 Original 23-14 23-45 23-62 23-62 23-34 23-49 23-53 23-62 23-7 23-51 23-51 23-43 Section

23.1153

23.1165 (d)(e)

23.1182

23.1183 (a)(b)

23.1301 (a)(b)*(c)

23.1303 (a)(b)(c)(d)(e)(f)

23.1305 (a)(1)(2)(3)(b)(2)

23.1307 (All)

23.1309 (a)(1)(2)(b)(c)(d)

23.1310 (a)

23.1311 (a)(b)

23.1321 (a)(b)(c)(d)(e)

23.1322 (All)

23.1323 (a)(b)(c)(e)

23.1325 (b)(1)(2)

23.1327 (a)(b)

23.1329 (h)

23.1331 (All)

23.1335

23.1337 (a)(b)(1)(c)

23.1351 (a)(b)(d)(e)

23.1353 (a)(b)(c)(d)(e)

23.1353 (h)

23.1357 (a)(b)(d) Amdt.

23-51 23-62 23-14 23-51 23-62 23-62 23-52 23-49 23-62 23-62 23-62 23-49 23-43 23-62 23-50 23-20 23-49 23-62 23-20 23-51 23-49 23-62 23-49 23-43 Section

23.1359 (a)(b)(c)

23.1361 (a)(b)(2)(3)

23.1365 (a)(b)(d)(e)

23.1367 (All)

23.1381 (a)(b)

23.1416 (b)(c)

23.1419 (a)(c)

23.1431 (a)(b)(e)

23.1501 (All)

23.1521 (a)(b)(c)

23.1523 (All)

23.1525 (All)

23.1529

23.1541 (a)(b)(c)

23.1543 (b)(c)

23.1545 (a)(b)(c)(d)

23.1549 (All)

23.1553 (All)

23.1555 (a)*(b)*(d)(3)(e)(2)

23.1559 (c)

23.1581 (a)(b)(c)(f)

23.1583 (b)(h)(m)

23.1585 (j)

23.2010 (a)(b)

23.2515 (a)(b)

23.2520 (a)(b) †14 CFR 23.954(a)(b) is applicable only to airplanes which have this regulation as part of their certification basis.

----END---- Amdt.

23-49 23-49 23-49 Original Original 23-23 23-43 23-62 23-21 23-50 23-34 23-45 23-26 23-21 23-50 23-62 23-45 23-50 23-62 23-62 23-50 23-62 23-62 23-64 23-64 23-64