STC SA01933WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

This certificate issued to: Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 SA01933WI Part 23* of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: See Approved Model List (AML) SA01933WI Multiple- AML STC Model: for approved aircraft makes and models Description of Type Design Change:

Hardware and software update for the Garmin G1000 Integrated Avionics System with GFC 700 Automatic Flight Control System Required Data: Garmin Master Drawing List (MDL) 005-01385-00, Revision 1, dated 10/29/2019 Later FAA-approved revisions to the data listed above are incorporated without amendment to this certificate

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

(2) If the holder agrees to permit another person to use this c ertificate 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 accordanc e with the Airplane Flight Manual Supplement (AFMS) identified on the Approved Model List.

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

Date of Application: May 2, 2019 Date Reissued:

Date of Issuance: October 29, 2019 Date Amended:

Signature

Title Paul Mast ODA STC Unit Administrator ODA-240087-CE

Possession of this Sup plemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Sup plemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01933WI 10/29/2019 Possession of this Sup plemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.

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

*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 Amdt. Section Amdt.

23.301 a 23-48 23.867 23-49 23.1365 a,b,d,e 23-49

23.303 Original 23.901 a, b(1) 23-51 23.1381 a,b Original

23.305 23-45 23.903 b(2) 23-51 23.1431 a,b,e 23-49

23.307 a Original 23.1301 23-20 23.1457 23-35

23.337 23-48 23.1303 a,b,d,e,f 23-49 23.1459 23-35

23.561 e 23-48 23.1307 23-49 23.1501 23-21

23.601 Original 23.1309 a(1)(3),b,c,d,e 23-49 (Note 2) 23.1523 23-34

23.603 23-23 23.1311 23-49 23.1525 23-45

23.605 a 23-23 23.1321 23-49 (Note 2) 23.1529 23-26

23.607 23-48 23.1322 23-43 23.1541 a,b 23-21

23.609 Original 23.1323 e 23-62 23.1543 b,c 23-50

23.611 23-48 23.1329 23-49 23.1545 a,b(4),d 23-50

23.613 a,b,c 23-45 23.1331 a,b(1) 23-43 23.1549 23-45 (Note 2)

23.627 Original 23.1335 23-20 23.1553 23-50 (Note 3)

23.671 a,b Original 23.1337 b(1) 23-51 (Note 1) 23.1555 a,b,e(2 ),d(1) 23-50 (Note 1)

23.771 a 23-14 23.1351 a,g 23-49 23.1581 a,b(1)(3),c,d,e,f 23-5 0

23.773 a(2) 23-45 23.1353 h 23-49 23.1583 e,h,m (Note 4)

23.777 a,b 23-51 23.1357 a,b,c,d 23-43 23.1585 a(1), j (Note 4)

23.853 a 23-49 23.1359 23-49 23.2515 a, b 23-64

23.863 a,b 23-34 23.2520 a, b 23-64

Note 1 – A compliance finding has been made showing the compensating design features and alternate methods of compliance found in FAA ELOS Memo ACE-08-09 for 14 CFR 23.1337 b(1) and

23.1555 d(1) have been maintained.

Note 2 - A compliance finding has been made showing the compensating design features and alternate methods of compliance found in FAA ELOS Memo ACE-08-10 for 14 CFR 23.1309 b(1)(2)(3),

23.1321 a, and 23.1549 have been maintained.

Note 3 - A compliance finding has been made showing the compensating design features and alternate methods of compliance found in FAA ELOS Memo ACE-08-21 for 14 CFR 23.1553 have been maintained.

Note 4 –A compliance finding has been made using Special Conditions 23-232-SC for 14 CFR 23.1583 e,h,m and 23.1585 a(1), j