STC SA01896WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificate issued to:

SA01896WI Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 Part of the Original Product – Type Certificate Number: Make:

Federal Aviation Regulations 23* Garmin G1000 Integrated Avionics System hardware and software updates including optional Flight Stream 510 Data Required:

(1) Master Drawing List (MDL) 005-01328-00, Revision 1, dated February 4, 2019

(2) Airplane Flight Manual Supplement (AFMS) 190-02450-02, Revision 1, dated February 4, 2019

(3) System Maintenance Manual (includes ICA) 190-02450-01, Revision 1, dated February 4, 2019 Later FAA-approved revisions to the data listed above are incorporated without amendment to this certificate Textron Aviation Inc.

510 A00014WI Limitations and Conditions:

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

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

(3) Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) identified above.

(continued on Page 3)

May 14, 2021 September 26, 2018 February 4, 2019 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

SA01896WI Limitations and Conditions (Cont.)

(4) 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.

*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:

Amdt.

23-49 23-49 23-43 23-20 23-49 23-49 23-43 23-49 23-49 Orig.

23-49 23-21 23-34 23-45 23-26 23-21 23-50 23-50 23-45 23-50 23-50 23-50 23-50 23-64 23-64 23-64

Amdt.

23-48 Orig.

23-45 Orig.

23-48 23-48 Orig.

23-23 23-23 23-48 Orig.

23-48 23-45 Orig Orig 23-14 23-45 23-51 23-49 23-34 23-20 23-49 23-49 23-49 23-49 23-49 23-43

Section

23.301(a)

23.303

23.305

23.307 (a)

23.337

23.561 (e)

23.601

23.603

23.605 (a)

23.607

23.609

23.611

23.613 (a)(b)(c)

23.627

23.671 (a)(b)

23.771 (a)

23.773 (a)(2)

23.777 (a)(b)

23.853 (a)

23.863 (a)(b)

23.1301 (a)(b)(c)(d)

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

23.1307

23.1309(a)(1)(3)(b)(c)(d)(e)

23.1311

23.1321

23.1322

May 14, 2021 Section

23.1323 (a)

23.1329

23.1331 (a)(b)(1)

23.1335

23.1351 (a)(g)

23.1353 (h)

23.1357 (a)(b)(c)(d)

23.1359

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

23.1381 (a)(b)

23.1431 (a)(b)(e)

23.1501

23.1523

23.1525

23.1529

23.1541 (a)(b)

23.1543 (b)(c)

23.1545 (a)(b)(4)(d)

23.1549

23.1555 (a)(b)(e)(2)

23.1581 (a)(b)(1)(3)(c)(d)(f)

23.1583 (e)(h)(m)

23.1585 (a)(1)(j)

23.2010 (a)(b)

23.2515 (a)(b)

23.2520 (a)(b)

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