STC SA01945WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01945WI This certificate issued to: Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Part 23* of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: See Approved Model List (AML) SA01945WI Model: for approved aircraft makes and models Multiple- AML STC Description of Type Design Change:

Hardware and software update for the Garmin G1000 Integrated Avionics System Required Data: Garmin Master Drawing List (MDL) 005-01474-00, Revision 1, dated June 10, 2020 Later FAA-approved revisions to the data listed above are incorporated without amendment to this certificate Limitations and Conditions:

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

(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) Aircraft modified by this STC must be operated in accordance with the Airplane Flight Manual Supplement (AFMS) identified on the Approved Model List.

(4) Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) on the Master Drawing List.

Date of Application: May 26, 2020 Date Reissued:

Date of Issuance: June 10, 2020 Date Amended:

By Direction of the Administrator Signature Title Paul Mast ODA STC Unit Administrator ODA-240087-CE

FAA Form 8110-2 (5/14) Page 1 of 3

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

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01945WI 6/10/2020 *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 remains unchanged from the original approval.

b. The certification basis for parts changed or affected by this change is:

Section Amdt. Section

23.143 (c) 23-50 23.1311

23.301 (a) 23-48 23.1321

23.303 Original 23.1322

23.305 23-45 23.1323 (a)(b)(c)

23.307 (a) Original 23.1325 (a) (b)(1)(2)(i) (e)

23.337 23-48 23.1327

23.561 (a) (b)(3) (e) 23-48 23.1329

23.601 Original 23.1331 (a) (b)(1)

23.603 23-23 23.1335

23.605 (a) 23-23 23.1337 (b)(c)

23.607 (a)(b) 23-48 23.1351 (a) (c)(4) (d)(1) (g)

23.609 Original 23.1353 (h)

23.611 23-48 23.1357 (a)(b)(c)(d)

23.613 (a)(b) 23-45 23.1359

23.627 Original 23.1365 (a)(b)(d)(e)

23.671 Original 23.1381 (a)(b)

23.681 (a) Original 23.1419 (a)

23.683 23-7 23.1431 (a)(b)(e)

23.685 (a)(c)(d) 23-17 23.1501

23.689 (a)(2)(3) (b) 23-7 23.1523

23.771 (a) 23-14 23.1525

23.773 (a)(2) 23-45 23.1529

23.777 (a)(b) 23-51 23.1545 (a)(b)

23.853 (a) 23-14 23.1549

23.867 23-7 23.1553

23.1301 23-20 23.1555 (a) (b) (e)(2)

23.1303 (a)(b)(c)(f) 23-49 23.1581 (a) (b)(1)(3) (c)(d)(f)

23.1305 (a)(1)(2)(3) (b)(2)(3)(i) 23-52 23.1583 (h)(m)

(4)(i) (5) 23.1585 (j)

23.1309 (a)(1)(2)(3) (b) 23-49 23.2515

(c)(1)(2)(i)(iii)(3) (e) 23.2520 Special Conditions (HIRF):

23-159-SC 23-172-SC 23-146-SC 23-173-SC 23-150-SC Amdt.

23-49 23-49 23-43 23-49 23-50 23-20 23-49 23-43 23-20 23-49 23-49 23-49 23-43 23-49 23-49 Original 23-43 23-49 23-21 23-34 23-45 23-26 23-50 23-45 23-50 23-50 23-50 23-50 23-50 23-64 23-64

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