STC SR02647SE

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SR02647SE Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062 3 Federal Aviation Regulations 27 Airbus Helicopters H9EU AS 350 B2, AS 350 B3 Installation of a Garmin GFC 600H Flight Control System in accordance with Garmin Master Drawing List, 005-01095-00 Rev. 1 or later FAA-approved revision. Instructions for Continued Airworthiness are provided in the Maintenance Manual, 190-02081-03 Rev. 1 or later FAA-approved revision. Operating information is provided in the Rotorcraft Flight Manual Supplement, 190-02081-02 Rev. 1 or later FAA-approved revision.

(1) The installer must determine whether this design change is compatible with previously installed modifications.

(2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(3) A copy of this certificate, the approved RFMS, and the approved ICA must be maintained as part of the permanent records for the modified rotorcraft.

October 10, 2016 February 5, 2020

Erik Frisk ODA STC Unit Administrator ODA-240087-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47.

FAA Form 8110-2 (5/14) Page 3 of

3 SR02295LA Issued: February 5, 2020

Certification Basis:

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

Section

27.1 (b)

27.141 (a)(1)(2)(3)(b)(2)(c)

27.151 (a)(b)

27.161 (a)(b)

27.171

27.251

27.301 (a)(b)(c)

27.303

27.305 (a)

27.307 (a)(b)(2)(3)

27.337 (a)

27.395 (a)(b)(1)(2)(3)

27.397 (a)

27.561 (a)(b)(3)

27.601 (a)(b)

27.603 (a)(b)(c)

27.605 (a)

27.607 (a)(b)

27.609 (a)(b)

27.610 (a)(b)(1)(d)

Amdt.

27-37 27-21 27-21 27-21 Orig.

Orig.

Orig.

Orig.

Orig.

27-26 27-26 27-26 27-40 27-32 Orig.

27-16 27-16 27-4 Orig.

27-46

Section

27.611 (a)(b)(c)

27.613 (a)(b)(c)(d)

27.619 (a)(b)(1)

27.625 (a)

27.671 (a)(b)

27.674

27.675 (a)(b)(c)

27.681 (a)

27.683 (a)(b)(c)

27.685 (a)(b)(c)(e)(f)

27.771 (a)(b)(c)

27.773 (a)(1)(b)

27.777 (a)(b)

27.779 (a)

27.853 (a)

27.863 (a)(b)

27.865 (c)(5)(e)

27.1301 (a)(b)(c)(d)

27.1309 (a)

27.1316 (a)

27.1317 (a)(b)(c) Amdt.

Orig.

27-26 Orig.

27-35 Orig.

27-26 27-16 Orig.

Orig.

27-26 Orig.

27-50 Orig.

27-21 27-37 27-16 27-36 Orig.

27-46 27-46 27-42 Section

27.1321 (a)(c)(d)

27.1322 (a)(b)(c)(d)

27.1325 (a)

27.1329 (a)(b)(c)(d)(e)(f)

27.1351 (a)

27.1357 (a)(b)(c)(d)

27.1365 (a)(b)(c)

27.1367 (a)(b)(c)

27.1381 (a)(b)

27.1501 (a)(b)

27.1503 (a)(b)

27.1523 (a)(b)(c)

27.1525

27.1527

27.1529

27.1541 (a)(b)

27.1555 (a)(d)(2)

27.1581 (a)(b)(d)

27.1583 (e)(g)

27.1585 (a) Amdt.

27-13 27-11 27-13 27-35 27-13 27-13 27-35 Orig.

Orig.

27-14 Orig.

Orig.

27-21 27-14 27-18 Orig.

27-21 27-14 27-16 27-21 Special Conditions:

27-043-SC (System Safety)

----END---- SR02647SE