STC SA02254AK

14 CFR 21.120)

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

Number: SA02254AK This certificate issued to:

Configuration 1:

Installation of “Single Screen”, “2 or 3 Screen”, “Dual Screen”, or “4 or 6 screen”, FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations, in accordance with Chelton Flight Systems, Inc., System Installation Manual Commuter and Large Aircraft, Document Number 150-045057, Revision M, dated August 13, 2014 or later FAA approved revision.

(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. SA02254AK, dated October 17, 2008 or later FAA approved revision, for a list of approved airplane models and applicable airworthiness regulations

Date of application: October 8, 2004

Date of issuance: September 21, 2005 Date reissued: January 11, 2010

Date amended: May 3, 2006; October 17, 2008;

November 6, 2011; May 1, 2017; June 16, 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: SA02254AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02254AK

14 CFR 21.120)

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

(Continuation Sheet) Number: SA02254AK Date of application: October 8, 2004 Date of issuance: September 21, 2005 Date reissued: January 11, 2010 Date amended: May 3, 2006; October 17, 2008; November 6, 2011;

May 1, 2017; June 16, 2022

Configuration 2:

Installation of “Single Screen”, “2 or 3 Screen”, “Dual Screen”, or “4 or 6 screen”, FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations, in accordance with Chelton Flight Systems, Inc., System Installation Manual Commuter and Large Aircraft, Document Number 64-000062, Revision E, dated August 13, 2014 or later FAA approved revision.

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, or later FAA approved revision.

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 150-045054, Revision E, dated May 1, 2017, or later FAA approved revision is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 150-045084, Revision D, dated May 1, 2017, or later FAA approved revision is required for “Dual Screen” or “4 or 6 Screen” installations as 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: SA02254AK Date of application: October 8, 2004 Date of issuance: September 21, 2005 Date reissued: January 11, 2010 Date amended: May 3, 2006; October 17, 2008; November 6, 2011;

May 1, 2017; June 16, 2022

3. For Configuration 2:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-07E2, Revision B, dated May 1, 2017 or later FAA approved revision is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-07E4, Revision B, dated May 1, 2017, or later FAA approved revision is required for “Dual Screen” or “4 or 6 Screen” installations as part of this installation.

4. For Configuration 3:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-90A2, Revision A, dated March 31, 2022 or later FAA approved revision, is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-90A4, Revision A, dated March 31, 2022 or later FAA approved revision, is required for “Dual Screen” or “4 or 6 Screen” installations as part of this installation.

5. For Configuration 1 or Configuration 2 Instructions for Continued Airworthiness, refer to Document Number 150-045055, Revision M, dated January 15, 2017, or later FAA approved revision. For Configuration 3 Instructions for Continued Airworthiness, refer to Document Number 13-254011, Revision A, dated November 11, 2021 or later FAA approved revision.