STC SA02282AK

Part * of the Civil Air Regulations.

Description of Type Design Change: Installation of Lycoming Engine Models IO-360-A1A, -A1B, -A1B6, -M1A, or -M1B; Hartzell propeller models HC-C2YR-1BF/F7666A()/F8477(), HC-C2YR-1N/NG8301(), or MT-Propeller Model MTV-15-() and associated modified powerplant components, in accordance with Master Data List, DSA 175-1, Rev. E, dated September 15, 2015, or later FAA approved revisions.

1. Compatibility of this modification with other FAA approved modifications, on the specific aircraft being altered, must be evaluated by the installer.

2. The aircraft must be equipped with Airplane Flight Manual Supplement/Supplemental Airplane Flight Manual, DSA 170-172-175-1301, Rev. B, dated December 14, 2015, or later FAA approved revision.

3. Maintained in accordance with Instructions for Continued Airworthiness, DSA-170-172-175 ICA, Rev. B, dated December 2, 2014, or later FAA accepted revision.

4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

5. Hartzell propeller model HC-C2YR-1N/NG8301() is approved on Lycoming engine models IO-360-A1B6, IO-360-M1A, and IO-360-M1B only.

6. This installation is compatible with Superior Air Parts Cold Air Induction System (CAIS) Supplemental Type Certificate No. SE02409AK.

Stoots Aviation David A. Stoots 3686 University Avenue So.

Fairbanks, Alaska 99709 Make: * Model: * Date of application: December 29, 2003

Date of issuance: December 12, 2006

Date reissued: September 3, 2008

Date amended: April 19, 2010; December 14, 2015

(Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

(Title) * Refer to FAA Approved Model List (AML) Number SA02282AK, Rev. A, dated December 14, 2015, for a list of approved airplane models and applicable airworthiness regulations.