STC SA02658SE

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 SA02658SE Federal Aviation Regulations23 See Approved Model List (AML) SA02658SE for approved aircraft models and applicable airworthiness standards.

Installation of Garmin GI 275 Multi-Function Display System. Data required includes Garmin Master Drawing List (MDL) 005-01208-41 Revision 1, dated January 13, 2020 or later FAA-approved revision; Garmin Airplane Flight Manual Supplement (AFMS) 190-02246-12 Revision 1, dated January 13, 2020 or later FAA-approved revision; Garmin Maintenance Manual (Includes Instructions for Continued Airworthiness (ICA)) 190-02246-11 Revision 1, dated January 13, 2020 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 and AML, 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) March 29, 2018 January 13, 2020 Multiple - AML STC June 14, 2021; January 18, 2023; June 23, 2023;

February 2, 2024 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 SR02295LASA02658SE Amended February 2, 2024 Limitations and Conditions (continued):

(4) The aircraft's magnetic compass must be retained for all GI 275 installations.

(5) All aircraft listed on the AML meet the requirements for airplane certification levels 1 through 4 and airplane performance levels low speed and high speed.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48A, 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 at amendment Original through 23-64.

Section

23.301 (a)

23.303

23.305 (a)(b)

23.307 (a)

23.337 (a)(b)(c)

23.561 (a)(b)(3)

23.601

23.603 (a)(b)

23.605 (a)

23.607 (a)(b)(c)

23.609 (a)(b)

23.611

23.613 (a)(b)(c)

23.627

23.771 (a)

23.773 (a)(2)

23.777 (a)(b)

23.853 (a)(d)(3)(v)

23.863 (a)(b)

23.901 (a)(b)(e)

23.903 (c)

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

23.963 (e)

23.993 (a)(b)(c)(d)(e)

23.1182 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 23-63 23-62 23-62 23-34 23-53 23-62 23-51 23-51 23-43 23-14 Section

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)

(3)(i)(iii)(4)(i)(5)(6)

23.1307

23.1309 (a)(b)(c)(d)

23.1310 (a)

23.1311 (a)(b)

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

23.1322 (a)(b)(c)(d)(e)

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

23.1325 (a)(b)(1)(2)

23.1327 (a)(b)

23.1329 (h)

23.1331 (a)

23.1335

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

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

23.1353 (a)(b)(c)(d)(h)

23.1357 (a)(b)(d)

23.1359 (a)(b)(c)

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

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

23.1367 (a)(b)(c)(d) Amdt.

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 23-43 23-49 23-49 23-49 Original Section

23.1381 (a)(b)

23.1419 (a)(c)

23.1431 (a)(b)

23.1501 (a)(b)

23.1521 (a)(b)(1)(2)(4)(c)(1)

23.1523 (a)(b)(c)

23.1525

23.1529

23.1541 (a)(b)(c)

23.1543 (b)(c)

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

23.1549 (a)(b)(c)(d)

23.1553

23.1555 (a)(d)(1)(3)

23.1559 (c)

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

23.1583 (h)(m)

23.1585 (j)

23.2000

23.2005

23.2010 (a)(b)

23.2335

23.2430 (a)(2)

23.2515 (a)(b)

23.2520 (a)(b) ----END---- Amdt.

Original 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 23-64 23-64 23-64 23-64