STC SA02197AK

14 CFR 21.120)

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

Number: SA02197AK This certificate issued to:

Installation of Hartzell HC-C2YR-1BF/F8477-4 Propeller, Hartzell C-3568-P Polished Spinner Assembly with A-2476-16 Spinner Mounting Kit, and if required, Hartzell Model C-1576 Damper Assembly in accordance with Burl’s Aircraft rebuild, LLC, Installation Instructions, Document Number 15AC80-I, dated August 21, 2002, or later FAA approved revision when aircraft is equipped with a Lycoming 0-360 Series engine in accordance with Supplemental Type Certificate No. SA302NW.

Compatibility of this design change with previously approved modifications must be determined by the installer. FAA Approved Flight Manual Supplement, Document Number 15AC80-AFM, dated September 24, 2002, or later FAA approved revision is a required part of this installation. For Instructions for Continued Airworthiness, refer to Burl’s Aircraft Rebuild, LLC, Instruction for Continued Airworthiness, Document No. 15AC80-ACA, dated August 21, 2002, or later FAA approved revision.

Burl’s Aircraft, LLC P.O. Box 671487 Chugiak, AK 99567-1487

Original Product Type Certificate Number: A-802

Make: AeroSedan, LLC Model: 15AC and S15AC

Date of application: February 04, 2002

Date of issuance: September 24, 2002 Date reissued: March 22, 2022

August A. Asay Title: Manager, Anchorage ACO Branch

Part 3 of the Civil Air Regulations.

14 CFR 21.120)

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

Number: SA02197AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02197AK