STC SP03675AT

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SP03675AT

This certificate issued to: B/E Aerospace 3110 Commerce Parkway Miramar, FL 33025

Part 29 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: H10EU Make: Eurocopter Aerospaciale Model: SA-365N1, AS-365N2, AS-65N3

Installation of a Honeywell Solid State Cockpit Voice Flight Data Recorder (SSCVFDR) into a Eurocopter SA-365N1, AS-365N2 and AS-365N3 Series Rotocraft and associated hardware in accordance with Master Drawing List 2-54965-001 Revision B dated February 4, 2009 or later FAA approved drawing revisions.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane

Date of Application: January 07, 2008 Date Reissued: March 02, 2015 Date of Issuance: March 06, 2009 Date Amended:

Signature

Title: Melvin D. Taylor, Manager Atlanta Aircraft Certification Office

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

Transfer the ownership of Supplemental Type Certificate Number: ST03675AT

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST03675AT

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

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. FAA Approved Airplane Flight Manual Supplement for the Honeywell Honeywell Solid State Cockpit Voice Flight Data Recorder (SSCVFDR), 2-54965-912, revision IR, dated March 6, 2009, or later FAA approved revision is a required part of this STC.

Instructions for Continued Airworthiness (ICA), EMTEQ Engineering Document No. 2-54965-903, Rev. IR, dated August 4, 2008, or later FAA accepted revision must be made available to the operator at the time of installation.

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 Eurocopter SA-365N1, AS-365N2 and AS-365N3 passenger to Freighter is as follows:

a. The type certification basis for Eurocopter SA-365N1, AS-365N2 and AS-365N3 Series Rotocraft is shown on TCDS H10EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, January 7, 2008 is based upon Part 29 as amended by Amendment 29-49. 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 modification was determined to be:

Regulations at the latest amendment 29-1 through 29-49

29.301, 29.303, 29.305, 29.307, 29.561, 29.601, 29.603, 29.607, 29.609, 29.610, 29.611, 29.613, 29.625,

29.683, 29.1301, 29.1309, 29.1322, 29.1351, 29.1357, 29.1359, 29.1431, 29.1457, 29.1459, 29.1529 Appendix F

Regulations at an intermediate amendment Appendix H

Regulations at the amendment level in TCDS H10EU Appendix G --------------------------END---------------------------