STC SR02482AK

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 4

Number: SR02482AK This certificate issued to:

Installation of avionics and stability augmentation system for certification of Single Pilot Instrument Flight Rules (SPIFR) Operations in accordance with Genesys Aerosystems, Inc., Master Data List (MDL), MBB-BK 117 C-2(e) Avionics Upgrade, Document Number 19-145001, Revision F, dated June 16, 2020, or later FAA approved revision.

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

2. For Instructions for Continued Airworthiness, refer to Document Number 19-145014, Revision D, dated February 20, 2020, or later FAA accepted revision.

Genesys Aerosystems, Inc.

4001 Old International Airport Drive, Unit #10 Anchorage, Alaska, 99502 Original Product Type Certificate Number: H13EU

Make: Airbus Helicopters Deutschland GmbH (AHD) Model: MBB-BK 117 C-2

Date of application: April 14, 2016

Date of issuance: February 13, 2017 Date reissued:

Date amended: February 14, 2019; October 27, 2020 By direction of the Administrator

August A. Asay Title: Manager, Anchorage ACO Branch

Part 23 of Federal Aviation Regulations.

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 4

Number: SR02482AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR02482AK

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 4

(Continuation Sheet 1) Date of issuance: February 13, 2017 Date amended: October 27, 2020 Number: SR02482AK

3. For Rotorcraft Flight Manual Supplement, refer to Document Number 19-145027, Revision B, dated October 22, 2020, or later FAA approved revision.

4. This type design change applies to MBB-BK 117 C-2 starting at serial number 9601, designated MBB-BK 117 C-2(e).

5. Installation of HeliSAS Autopilot System per STC SR11337SC is a required part of this installation.

6. 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.

7. Maximum instrument approach angle is 6 degrees following the operational limitations defined in the Rotorcraft Flight Manual Supplement.

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 Airbus Helicopters Deutschland GmbH MBB-BK117 C-2(e) (EC145e) is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown in TCDS H13EU.

b. The modification certification basis for parts changed or affected by this change since the reference application date February 16, 2017, is based upon Part 29 and Part 29 Appendix B with specific amendments as below:

14 CFR Part 29 Amdt 14 CFR Part 29 Amdt

29.301 0 29.1325 24

29.303 0 29.1327 0

29.305 0 29.1329(f) 42

29.307(a) 30 29.1331 24

29.321 0 29.1333 24

29.337 30 29.1351(a)(b)(d) 42

29.561(a)(b) 38 29.1357(a)(b)(c)(d) 24

29.601 0 29.1381 0

29.603 17 29.1431 0

29.605(a) 17 29.1501 15

29.607 5 29.1525 24

29.609 0 29.1529 20

29.610 53 29.1541 0

14 CFR 21.120)

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 4 OF 4

(Continuation Sheet 2) Date of issuance: February 13, 2017 Date amended: October 27, 2020 Number: SR02482AK

14 CFR Part 29 Amdt 14 CFR Part 29 Amdt

29.771 24 29.1543(b) 0

29.773 3 29.1545 17

29.777 0 29.1555(a) 24

29.853(a) 23 29.1559 24

29.1301 0 29.1581 15

29.1303 24 29.1583(e) 24

29.1307(c)(d)(e) 12 29 App B I 21

29.1309 53 29 App B VIII 40

29.1316 53 29 App B IX 21

29.1317 (a)(b)(c) 49

29.1321 21

29.1322 12

29.1323 44