STC SA02220AK

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 4 Number: SA02220AK This certificate issued to:

Configuration 1:

Installation of Genesys Aerosystems, Inc. FlightLogic Electronic Flight Instrument System (EFIS) in accordance with Genesys Aerosystems, Inc., System Installation Manual Commuter and Large Aircraft, Document Number 150-045057, Revision M, dated August 13, 2014, 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: A27CE Make: Textron Aviation Inc.

Model: 501 Date of application: March 26, 2004 Date of issuance: July 31, 2004 Date reissued: January 11, 2010, February 26, 2020 Date amended: April 26, 2005; May 19, 2006;

October 31, 2011; September 6, 2022 By direction of the Administrator Signature:

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: SA02220AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02220AK

14 CFR 21.120)

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

(Continuation Sheet) Number: SA02220AK Date of application: March 26, 2004 Date of issuance: July 31, 2004 Date reissued: January 11, 2010; February 26, 2020 Date amended: April 26, 2005; May 19, 2006; October 31, 2011; September 6, 2022

Configuration 2:

Installation of Genesys Aerosystems, Inc. FlightLogic EFIS in accordance with Genesys Aerosystems, Inc., IDU-3 System Installation Manual Commuter and Large Aircraft

(7.0E and Higher), Document Number 64-000062, Revision E, dated August 13, 2014, 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, 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, Document Number 150-045006, Rev. G, dated February 26, 2020, or later FAA approved revision is a required for “Single-Side (2 to 3 Screen)” as part of this installation.

FAA approved Airplane Flight Manual Supplement, Document Number 150-045076, Rev D, dated February 26, 2020, or later FAA approved revision is a required for “Dual-Side (4 to 6 Screen)”, as part of this installation.

(Limitations and Conditions continued on page 4 of 4)

14 CFR 21.120)

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

(Continuation Sheet) Number: SA02220AK Date of application: March 26, 2004 Date of issuance: July 31, 2004 Date reissued: January 11, 2010; February 26, 2020 Date amended: April 26, 2005; May 19, 2006; October 31, 2011; September 6, 2022

3. For Configuration 2:

FAA approved Airplane Flight Manual Supplement, Document Number 13-220FMS-07E2, Rev. B, dated February 26, 2020, or later FAA approved revision is a required for “Single-Side (2 to 3 Screen)” as part of this installation.

FAA approved Airplane Flight Manual Supplement, Document Number 13-220FMS-07E4, Rev. B, dated February 26, 2020, or later FAA approved revision is a required for “Dual-Side (4 to 6 Screen)” as part of this installation.

4. For Configuration 3:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-220FMS-90A2, Revision A, dated June 30, 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 13-220FMS-90A4, Revision A, dated June 30, 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 Genesys Aerosystems, Inc. Document Number 150-045005, Rev. P, dated February 01, 2020, or later FAA accepted revision.

For Configuration 3 Instructions for Continued Airworthiness, refer to Genesys Aerosystems, Inc. Document Number 13-220011, Revision B, dated April 25, 2022 or later FAA accepted revision.