STC SR09576RC

Number SR09576RC

This certificate, issued to Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062

Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H9EU Make: Airbus Helicopters Model: EC130B4

Description of the Type Design Change: Installation of Garmin G500H Flight Display System in accordance with Master Document List, G500H for Airbus (Eurocopter) EC130, 005-00763-08, Rev 1, dated 05/15/2014, or later FAA approved revision. Instructions for Continued Airworthiness for the Garmin G500H Installation in Eurocopter EC130, 190-01527-15, Rev 1, dated 04/22/2014, or later FAA approved revision and Rotorcraft Flight Manual Supplement for Eurocopter Model EC 130 B4 with Garmin G500H System, 190-01527-16, Rev 1, dated 05/15/2014, or later FAA approved revision are required.

Limitations and Conditions: This approval should not be extended to other rotorcraft of this model series unless the installer determines that the relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft. 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. A copy of this certificate, RFMS and ICA, must be maintained as part of the permanent records for the modified aircraft.

Date of application: May 12, 2010 Date reissued: August 9, 2012; March 7, 2013 Date of issuance: August 30, 2010 Date amended: May 15, 2014

(Signature)

ODA STC Unit Administrator, ODA-240087-CE (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of Transferee)

(Address of Transferee)

(Number and Street)

(City, State, and ZIP Code)

from (Name of Grantor) (Print or Type)

(Address of Grantor)

(Number and Street)

(City, State, and ZIP Code)

Signature of Grantor (In Ink):

U.S. GPO: 1987-763-289

Number SR09576RC Garmin International, Inc.

Issued: Date August 30, 2010 Reissued: Date August 9, 2012; March 7, 2013 Amended: Date May 15, 2014

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 this change is as follows:

a. The certification basis for parts not changed or not affected by this modification remains unchanged.

b. The certification basis for parts changed or affected by this modification is captured in the table below.

Section Amdt Section Amdt

27.301(a)(b)(c) 27-0 27-1322(b)(d) 27-11

27.303 27-0 27.1323(a)(b)(c) 27-13

27.305(a) 27-0 27.1325(a) 27-13

27.307(a) 27-26 27.1327(a)(b) 27-13

27.321(a)(b) 27-11 27.1351(a) 27-13

27.337(a)(b) 27-26 27.1357(a)(b)(c)(d) 27-13

27.561(b) 27-32 27.1365(a)(b) 27-0

27.601(a)(b) 27-0 27.1367(a)(b)(c) 27-0

27.603(a)(b)(c) 27-16 27.1381(a)(b) 27-0

27.605(a) 27-16 27.1501(a)(b) 27-14

27.609(a) 27-0 27.1523(a)(b)(c) 27-0

27.610(a)(b) 27-21 27.1525 27-21

27.611(a)(b) 27-0 27.1529 27-18

27.613(a)(b)(c)(d) 27-26 27.1541(a)(b) 27-0

27.771(a)(b)(c) 27-0 27.1543(b) 27-0

27.773(a)(b) 27-0 27.1545(a)(b) 27-16

27.777(a)(b) 27-0 27.1555(a) 27-21

27.1301(a)(b)(c)(d) 27-0 27.1559 27-21

27.1303(a)(b)(c) 27-0 27.1581(a)(b)(d) 27-14

27.1309(a)(c)(d) 27-21 27.1583(e) 27-16

27.1317(c) 27-42 27.1585(a) 27-21

27.1321(a)(c)(d) 27-13 -------- ---

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