STC SR02230AK

FAA Form 8110-2(10-68) Page 1 of 3 Number SR02230AK T his Certificate issued to c ertifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part * of the * Regulations.

D escription of Type Design Change:

Installation of Genesys Aerosystems, Inc, FlightLogic Electronic Flight Instrument System (EFIS) per design documentation for selected configuration, as listed in Genesys Aerosystems, Inc., Master Data List (MDL) Document Number 17-000025, Revision L, dated May 15, 2020, or later FAA approved revisions.

L imitations and Conditions:

1. Installer must determine compatibility of this design change with previously approved modifications.

2. If the holder agrees to permit another person to us e this certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. Installation is not permitted in Instrument Flight Rules (IFR) certified rotorcraft.

Installation is limited to having Primary Flight Display (PFD) located above Multi-Function Display (MFD).

* See attached FAA Approved Model List (AML) No. SR02230AK, dated November 17, 2004, for a list of approved rotorcraft models and ap plicable airworthiness regulations.

Genesys Aerosystems, Inc.

4001 Old International Airport Drive, Unit #10 Anchorage, Alaska 99502 Date reissued: January 11, 2010 Date amended: December 21, 2007; March 28, 2008;

March 14, 2011; December 19, 2012; February 18, 2015; May 1, 2017; September 18, 2020 By direction of the Administrator

(S ignature) August A. Asay Manager, Anchorage ACO Branch

(Title) Date of application: July 17, 2003 Date of issuance: November 17, 2004

FAA Form 8110-2(10-68) Page 3 of 3 Number SR02230AK Date of issuance: November 17, 2004 L imitations and Conditions (continued):

4. Activation of Fuel Flow functions requires installation of separately approved fuel flow transducers.

5. O ptional autopilot integration is approved for SFIM PA85 autopilots installed in accordance with American Eurocopter Corporation STC numbers SH6002SW-D or SH7000SW-D.

6. R efer to MDL Document Number 17-000025, Revision L, dated May 15, 2020, or later FAA approved revision, for applicable Rotorcraft Flight Manual Supplement (RFMS) and Instructions for Continued A irworthiness (ICA).

Certification Basis:

The certification basis for installation of Genesys Aerosystems, Inc. FlightLogic EFIS in Eurocopter AS350 and AS355 series Rotorcraft is as follows:

R egulations at the latest amendment 27-0 through 27-47:

1 4 CFR §§ 27.301-27.307, 27.321, 27.337, 27.561, 27.601, 27.771, 27.773, 21.777, 21.1301, 27.1303,

27.1307 – 27.1329, 27.1351, 27.1357 – 27.1381, 27.1501, 27.1519, 27.1525, 27.1529 – 27.1545, 27.1581,

27.1583