STC ST04465CH

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

Number: ST04465CH

Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number: A28NM Make: Airbus Model: A320 Models -211, -212, -214, -216, -231, -232, -233

Date of Application: November 11, 2020 Date Reissued:

Date of Issuance: February 19, 2021 Date Amended:

Brenda L. Litchfield ODA Administrator Title: Envoy Aerospace, LLC ODA-831240-CE Astronics Armstrong Aerospace 804 S. Northpoint Blvd Waukegan, IL 60085

1) This STC is applicable to all serial numbers for this Make-Model.

2) The installer must determine whether this design change is compatible with previously approved modifications.

3) Incorporation of this design change results in Airplane Flight Manual Supplements, Doc. No. 0664- 09891-2407 and Doc. No. 0664-09906-2406, no longer being applicable to the aircraft. These documents are to be removed from the FAA approved Aircraft Flight Manual.

4) FAA Approved Instructions for Continued Airworthiness – Airworthiness Limitations, Section 2 of Astronics CSC Doc. No. DC113-9932-00, Revision -, approved February 19, 2021, or later FAA approved revision is a required part of this STC.

5) 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.

Removal of a 2Ku In-flight Entertainment and Connectivity (IFEC) System in accordance with Astronics Connectivity Systems & Certification (CSC) Master Data List, Doc. No. DC104-9932-00 Revision A, dated February 18, 2021, or later FAA approved revision.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of 3

Number: ST04465CH

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 3 of 3

(Continuation Sheet) Number: ST04465CH Date of Issuance: February 19, 2021 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 the Airbus A320 Models -211, -212, -214, -216, -231, -232, and -233 aircraft is as follows:

a. The type certification basis for the Airbus A320 Models -211, -212, -214, -216, -231, -232, and -233 aircraft is shown on TCDS A28NM for parts not changed or affected by the change.

b. This certification basis for parts changed or affected by the change since the reference date of application is based upon TCDS A28NM. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in Order 8110.48, the certification basis for this modification was determined to be:

Applicable regulations at the latest amendment 25-0 through 25-56 § 25.29(a)(b) § 25.301(a)(b) § 25.303 § 25.305(a)(b) § 25.307(a) § 25.365(a)(b)(d) § 25.561(a)(b)(c) § 25.571(a)(b) § 25.601 § 25.603(a)(b) § 25.605(a) § 25.609(a)(b) § 25.611 § 25.613(a)(b)(c)(d) § 25.619(a)(b)(c) § 25.625(a)(b)(c) § 25.853(a) § 25.1301(a)(b) § 25.1351(a) § 25.1359(d) § 25.1529

Applicable 14 CFR Part 26 regulations at the latest amendment 26-0 through 26-1 Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the latest amendment date of this STC, compliance has been found for the following regulations:

14 CFR § 26.11(c) [Amdt. No. 26-0]; § 26.47(c) [Amdt. No. 26-1].

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