STC SA03065CH-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the ST C holder.

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

Number: SA03065CH-D This certificate issued to: A/C Systems LLC 2282 Airport Road Hangar 2 Selmer, TN 38375

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: 3A16 Make: Hawker Beechcraft Corporation Model: G58, 58, 58A, D55, D55A, E55, E55A.

Installation of an A/C Systems Air Conditioning System in accordance with Standard Aero Master Da ta List 1021376, Revision (I), dated April 20, 2012 or later FAA approved revision.

1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

2. FAA Approved Airplane Flight Manual Supplement document number FTA-010-6, Rev (IR) dated April 23, 2012, or later FAA approved revision is a required part of this modification.

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

-- Continued on Page 3

Date of Application: December 21, 2011 Date Reissued: October 08, 2012, May 12, 2020 Date of Issuance: April 23, 2012 Date Amended:

Signature Title (for) Christina M. Underwood Manager, Atlanta ACO Branch

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

Transfer the ownership of Supplemental Type Certificate Number: SA03065CH-D

To (Name and address of transferee)

From (Name and address of grantor)

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

Number: SA0306CH-D Date of Issuance: April 23, 2012 Date Reissued: October 08, 2012, May 12, 2020

Certification Basis:

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Hawker Beechcraft Corporation G58, 58, 58A, D55, D55A, E55, E55A Installation of an A/C Systems Air Conditioning System is as follows:

a. The type certification basis for Hawker Beechcraft Corporation G58, 58, 58A, D55, D55A, E55, E55A is shown on TCDS 3A16 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, December 21, 2011, is based upon TCDS 3A16. 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 amendment level Original thru 23-21

23.1(a, b)(Original), 23.45(a-d)(23-21), 23.51(a, b)(23-21), 23.65(a)(23-21), 23.77(a)(23-21), 23.301(a-c)(Original),

23.303(Original), 23.305(a, b)(Original), 23.307(a)(Original), 23.561(a-e)(Original), 23.601(Original), 23.603(a,

b)(Original), 23.605(Original), 23.607(Original), 23.609(a, b)(Original), 23.611(Original), 23.613(a -c)(Original), 23.619(a-

23.777(a-b)(Original), 23.831(Original), 23.901(a, b)(Original), 23.1041(Original), 23.1043(a -d)(Original), 23.1047(a,

b)(Original), 23.1163(a, b)(Original), 23.1183(a, b)(Original), 23.1191(a -h)(Original), 23.1301(a1, a2, a4, b)(Original),

23.1309(a, b)(23-14), 23.1351(a1)(Original), 23.1357(a, d)(Original), 23.1365(a, b)(Original), 23.1431(Original),

23.1501(a, b)(Original), 23.1519(Original), 23.1529(a-k)(23-8), 23.1541(a-c)(Original), 23.1555(a)(Original),

23.1585(a)(Original)

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