STC ST04633CH

Number: ST04633CH

Part 25 of the Federal Aviation Regulations.

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

Date of Application: August 30, 2024 Date Reissued: December 26, 2024 Date of Issuance: December 20, 2024 Date Amended:

Brenda L. Litchfield ODA Administrator Title: Envoy Aerospace, LLC ODA-831240-CE Astronics Connectivity Systems and Certification Corp.

804 S. Northpoint Blvd Waukegan, IL 60085 Installation of Safran RAVE Wireless In-Flight Entertainment (IFE) System in accordance with Astronics Connectivity Systems and Certification Corp. Master Data List, Doc. No. DC104-142002-00, Revision A, dated December 17, 2024, or later FAA-approved revisions.

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) FAA Approved Airplane Flight Manual Supplement, Astronics Connectivity Systems and Certification Corp.

Doc. No. DC303-142002-00, Revision -, approved December 20, 2024, or later FAA approved revision is required on board the modified aircraft.

4) 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.

5) This modification requires that the aircraft be shown to be electromagnetically compatible with transmitting portable electronic devices that utilize wireless data technologies.

Number: ST04633CH

(Continuation Sheet) Number: ST04633CH Date Reissued: December 26, 2024 Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for the Airbus A320 Model-211, A320 Model-212, A320 Model-214, A320 Model-216, A320 Model-231, A320 Model-232, A320 Model-233 aircraft is as follows:

a. The type certification basis for the Aircraft A320 Model-211, A320 Model-212, A320 Model-214, A320 Model-216, A320 Model-231, A320 Model-232, A320 Model-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 14 CFR Part 25 as amended by Amendment 25-56 as follows:

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)(c) § 25.307(a) § 25.561(a)(b)(c) § 25.571(a)(b) § 25.601 § 25.603(a)(b)(c) § 25.605(a) § 25.607(a)(b)(c) § 25.609(a) § 25.611 § 25.613(a)(b) § 25.619(a)(b)(c) § 25.625(a) § 25.787(a) § 25.789(a) § 25.1301(a)(b)(c)(d) § 25.1307(c) § 25.1309(a)(b)(d)(g) § 25.1351(a) § 25.1353(a)(b) § 25.1357(a)(c) § 25.1431(a)(c) § 25.1501(a)(b) § 25.1529 § 25.1541(a)(b) § 25.1581(a)(b)(d) § 25.1585(a)

Applicable 14 CFR Part 25 regulations at other amendment levels § 25.853(a) [Amdt 25-116]; § 25.869(a)(4) [Amdt 25-113]; § 25.981(a) [Amdt 25-102].

Applicable 14 CFR Part 26 regulations at the latest amendment 26-0 through 26-7 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. 26-7]; § 26.47(c) [Amdt. No. 26-7].

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