STC SA02203AK

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 4

Number: SA02203AK This certificate issued to:

Configuration 1:

Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV), in accordance with Genesys Aerosystems, Inc., System Installation Instructions, Document Number 150-045264, Revision AH, dated August 13, 2014, and Installation Instructions addendum KFC-400 Autopilot Integration, Document 150-045400, Revision B, dated June 8, 2015 or later FAA approved revisions.

(Description of Type Design Change continued on Page 3)

Genesys Aerosystems, Inc.

4001 Old International Airport Road, Unit 10 Anchorage, Alaska 99502 Original Product Type Certificate Number: *

Make: * Model: * See attached FAA Approved Model List (AML) No. SA02203AK, Rev. G, dated June 1, 2018, or later FAA Approved revision, for a list of approved airplane models and applicable

Date of application: January 11, 2002

Date of issuance: March 26, 2003 Date reissued: January 11, 2010

Date amended: July 31, 2004; April 1, 2005;

October 31, 2006; December 21, 2007;

December 21, 2011; February 1, 2017; June 1, 2018;

July 6, 2022 By direction of the Administrator

August A. Asay Title: Manager, Anchorage ACO Branch

Part 23 of Federal Aviation Regulations.

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 4

Number: SA02203AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02203AK

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 4

(Continuation Sheet) Number: SA02203AK Date of application: January 11, 2002 Date of issuance: March 26, 2003 Date reissued: January 11, 2010 Date amended: July 31, 2004; April 1, 2005, October 31, 2006; December 21, 2007;

December 21, 2011; February 1, 2017; June 1, 2018; July 6, 2022

Configuration 2:

Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV), in accordance with Genesys Aerosystems, Inc., Integrated Display Unit (IDU-3) System Installation Instructions, Document Number 64-000061, Revision I, dated August 13, 2014, and Installation Instructions addendum KFC-400 Autopilot Integration, Document 150-045400, Revision B, dated June 8, 2015 or later FAA approved revisions.

Configuration 3:

Installation of Genesys Aerosystems, Inc. Electronic Flight Information System (EFIS), in accordance with Genesys Aerosystems IDU-450 Installation Manual 9.0A, Document number 64-000124-090A, Revision A, dated April 26, 2021, and IDU-450 Installation Manual Supplement for Small Part 23 Aircraft, Document 64-000128, Revision A, dated March 28, 2022, or later FAA approved revisions.

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

2. For Configuration 1:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 150-045262, Revision H, dated January 23, 2017 or later FAA approved revision, is a required part of this installation.

For airplanes equipped with KFC-400 Autopilot, FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, document 150-045262-K400, Revision E, dated January 23, 2017 or later FAA approved revision, is a required part of this installation.

(Limitations and Conditions continued on Page 4)

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 4 OF 4

(Continuation Sheet) Number: SA02203AK Date of application: January 11, 2002 Date of issuance: March 26, 2003 Date reissued: January 11, 2010 Date amended: July 31, 2004; April 1, 2005, October 31, 2006; December 21, 2007;

December 21, 2011; February 1, 2017; June 1, 2018; July 6, 2022

3. For Configuration 2:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-203FMS-070E, Revision B, dated January 23, 2017 or later FAA approved revision, is a required part of this installation.

For airplanes equipped with KFC-400 Autopilot, FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, document 13-203FMS-7EK4, Revision B, dated January 23, 2017 or later FAA approved revision, is a required part of this installation.

3. For Configuration 3:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-203FMS-090A, Revision A, dated June 30, 2022, or later FAA approved revision, is a required part of this installation.

For airplanes equipped with KFC-400 Autopilot, FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, document 13-203FMS-9AK4, Revision A, dated June 30, 2022, or later FAA approved revision, is a required part of this installation.

4. For Configuration 1 or Configuration 2 Instructions for Continued Airworthiness, refer to Document Number 150-045261, Revision AB, dated January 15, 2017 or later FAA approved revision. For Configuration 3 Instructions for Continued Airworthiness, refer to Document Number 13-203011, Revision A, dated December 13, 2021 or later FAA approved revision.