STC SA02242SE

Number SA02242SE

This certificate, issued to Aerostar Aircraft Corporation 10555 Airport Drive Hayden Lake, ID 83835

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A17WE Make: Aerostar Model: PA-60-600 (Aerostar 600); PA-60-601 (Aerostar 601);

PA-60-601P (Aerostar 601P); PA-60-602P (Aerostar 602P);

PA-60-700P (Aerostar 700P)

Description of the Type Design Change: Fabrication of blended winglets in accordance with Aerostar Engineering Drawing List 275-DL, Revision NC, dated February 1, 2012, or later Federal Aviation Administration (FAA) approved revision. Installation in accordance with Aerostar Option 275 Winglet Installation Instructions Report 275-01, Revision NC, dated February 14, 2011, or later FAA-approved revision. This modification must be maintained in accordance with Aerostar Winglet Instructions for Continued Airworthiness (ICA) Report E-122 ICA, Revision B, dated February 13, 2012, and Aerostar Wing and Winglet Inspection Report E-123, Revision NC, dated July 3, 2012, or later FAA-accepted revisions.

Limitations and Conditions: Approval of this change in type design applies to the above listed aircraft only.

This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of the other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of the aircraft. A copy of this certificate, the Inspection Report, and ICA must be maintained as part of the permanent records for the modified aircraft.

Date of application: June 27, 2011 Date reissued:

Date of issuance: September 14, 2012 Date amended: March 12, 2013

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

Number SA02242SE

Aerostar Aircraft Corporation Issued: September 14, 2012 Reissued:

Amended: March 12, 2013

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.

Certification Basis:

The certification basis for this modification is based upon Title 14 Code of Federal Regulations (CFR) part 23 as specified in Type Certificate Data Sheet A17WE, except for areas changed or affected by the design change, for which the certification basis is 14 CFR part 23, effective February 1, 1965, including Amendments 23-1 through 23-59, with the following exceptions:

Section (§) Amendment § 23.29 23-0 § 23.305 23-0 § 23.1041 23-7 § 23.1043 23-21 § 23.1047 23-21 § 23.1401 23-0 § 23.1419 23-14 § 23.1521 23-0

- END -

FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES