STC SA02587AK

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3

Number: SA02587AK This certificate issued to:

Installation of Electronic Flight Information System (EFIS) and avionics in accordance with Genesys Aerosystems, Inc., Master Data List (MDL), PC-7 Avionics Upgrade, Document Number 13-PC7002, Revision A, dated September 4, 2024, or later FAA approved revision.

1. Compatibility of the design change with previously approved modifications must be determined by the installer.

(Limitations and Conditions continued on Page 3 of 3)

Genesys Aerosystems, Inc.

4001 Old International Airport Drive, Unit #10 Anchorage, AK 99502

Make: * Model: *See attached FAA Approved Model List (AML) No. SA02587AK, dated September 27, 2024, or later FAA approved revision, for a list of approved aircraft models.

Date of application: December 3, 2021

Date of issuance: September 27, 2024 Date reissued:

for Gregory S. DiLibero Title: Manager, West Certification Branch

Part 23 of Federal Aviation Regulation.

14 CFR 21.120)

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

Number: SA02587AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02587AK

14 CFR 21.120)

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

(Continuation Sheet) Date of application: December 3, 2021 Date of issuance: September 27, 2024 Date reissued:

Number: SA02587AK

Limitations and Conditions: (Continued from Page 1 of 3)

2. For Instructions for Continued Airworthiness, refer to Approved Model List.

3. For Rotorcraft Flight Manual Supplement, refer to Approved Model List.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the models listed on the AML is as follows:

a) The modification certification basis for parts changed or affected by this change since the reference application date December 3, 2021, is based upon Part 23 with specific amendments as below:

14 CFR Part 23 Amdt 14 CFR Part 23 Amdt

23.301 0 23.1308(a)(b)(c) 57

23.303 0 23.1309(a)(b)(c)(d) 62

23.305 0 23.1311(a)(b)(c) 62

23.307 0 23.1321(a)(c)(d)(e) 49

23.561(b)(e) 7 23.1322(a)(b)(c)(d)(e) 43

23.601 0 23.1323(a)(c) 49

23.603 0 23.1325(a)(b)(1)(2)(i) 49

23.605 0 23.1327(a)(b) 20

23.607 0 23.1331(a)(b) 43

23.609 0 23.1351(a)(1)(2)(i) 49

23.611 7 23.1353(h) 49

23.613 0 23.1357(a)(b)(c)(d) 43

23.619 7 23.1365(a)(b)(d)(e) 49

23.625(a) 7 23.1367(a)(b)(c)(d) 0

23.627 0 23.1381(a)(b)(c) 0

23.771(a) 14 23.1431(a)(b)(d)(e) 62

23.773(a)(2) 45 23.1501(a)(b) 21 23/777(a)(b) 62 23.1525 45

23.867(a)(b) 49 23.1529 26

23.1301(a)(b)(c) 62 23.1541(a)(b) 21

23.1303(a)(b)(c)(d)(e)(f) 49 23.1543(b)(c) 50

23.1305(a)(1)(2)(3)(c)(e) 52 23.1545(a)(b)(c)(d) 50

23.1306 61 23.1581(a)(b)(c)(d)(f) 50

23.1307 49 23.1585(j) 62