STC SR02541AK

14 CFR 21.120)

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

Number: SR02541AK This certificate issued to:

Installation of Electronic Flight Instrument System (EFIS), avionics, and optional HeliSAS autopilot system in accordance with Genesys Aerosystems, Inc., Master Data List (MDL), UH-60 Avionics Upgrade, Document Number 19-H60010, Revision A, dated September 12, 2020, or later FAA approved revision.

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

2. 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.

Genesys Aerosystems, Inc.

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

Date of application: August 20, 2018

Date of issuance: October 19, 2020 Date reissued:

August A. Asay Title: Manager, Anchorage ACO Branch

Part 29 of Federal Aviation Regulations.

*See attached FAA Approved Model List (AML) No. SR02541AK, dated September 22, 2020, for a list of approved rotorcraft models.

14 CFR 21.120)

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

Number: SR02541AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR02541AK

To:

From:

14 CFR 21.120)

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

(Continuation Sheet) Number: SR02541AK

Limitations and Conditions: (continued)

3. For Instructions for Continued Airworthiness, refer to Approved Model list, or later FAA approved revision.

4. For Rotorcraft Flight Manual Supplement, refer to Approved Model List, or later FAA approved revision.

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 August 20, 2018, is based upon Part 29 and Part 29 Appendices B and E with specific amendments as below:

14 CFR Part 29 Amdt 14 CFR Part 29 Amdt

29.21(a) 24 29.1316 53

29.29 15 29.1317(a)(b)(c) 49

29.31 0 29.1321 21

29.251 0 29.1322 12

29.301 0 29.1323 44

29.303 0 29.1325 24

29.305 0 29.1327 0

29.307(a) 4 29.1329 42

29.321 0 29.1333 24

29.337 0 29.1335 14

29.561(a)(b) 0 29.1351(a)(b)(d) 42

29.601 0 29.1353(a)(b) 15

29.603 17 29.1357(a)(b)(c)(d)(e) 24

29.605(a) 17 29.1381 0

29.607 5 29.1431 0

29.609 0 29.1501 15

29.610 53 29.1503 0

29.611 0 29.1519 0

29.674 30 29.1525 24

29.681(b) 0 29.1529 20

29.683 0 29.1541 0

29.771(a)(b)(c)(d) 24 29.1543 0

29.773(a)(b) 57 29.1545 17

29.777(a) 0 29.1581 15

29.1301 0 29 Appx B I 21

29.1303(a)(b)(c) 24 29 Appx B VIII 40

29.1305 40 29 Appx B IX(a)(b) 21

29.1307(b)(e) 12 29 Appx E I 49

29.1309 53