STC ST04462CH

ST04462CH Anuvu IFC Corporation 1050 Oak Creek Drive Lombard, IL 60148 Part 25 the Federal Aviation complete certification basis A28NM Airbus SAS

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

2) The equipment for which these provisions are intended has not been certified. Additional FAA approval is required for the installation of this equipment and must be evaluated to assure satisfactory compliance with the applicable airworthiness standards. (continued on page 3) 12/15/2017 3/23/2021 10/3/2022 12/17/2025 6/5/2020 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division

4 Installation of Row 44 Broadband Antenna System Provisions in accordance with Row 44 Master Data Index Listing, Document No. RWO100-0001-00, Revision IR, dated May 4, 2020 or later FAA approved revision.

Regulations. See pages 3-4 for A319 Model -111, -112, -113, -114, -115, -131, 132, -132 A320 Model -211, -212, -214, -216, -231, -232, -233 A321 Model -111, -112, -211, -212, -231, -232

ST04462CH 12/17/25 4

ST04462CH 12/17/25 Limitations and Conditions (continued):

3) FAA Approved Airplane Flight Manual Supplement, Row 44 Document No. as listed, is required on board the modified aircraft:

a) A319 models: RWO220-0007-00, Revision -, approved June 5, 2020 or later FAA approved revision

b) A320 models: RWO220-0008-00, Revision -, approved June 5, 2020 or later FAA approved revision.

c) A321 models: RWO220-0009-00, Revision -, approved June 5, 2020 or later FAA approved revision.

4) FAA Approved Instructions for Continued Airworthiness Source Document RWO260-0007-00, Airworthiness Limitations,Section 2, Revision IR, dated May 4, 2020, approved June 5, 2020, or later FAA approved revision.

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.

Certification Basis

The certification basis for the changed Airbus A319, A320, & A321 Series aircraft as described in this certificate is as follows:

a. The type certification basis for the Airbus A319, A320, & A321 Series aircraft is shown on TCDS A28NM for parts not changed or not affected by this change.

(continued on page 4) 3 4 Add Page

ST04462CH 12/17/25 Certification Basis (continued):

b. The certification basis for the parts changed or affected by this change since the reference date of application, December 15, 2017, 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:

25.23(a),(b) Amdt 25-0; 23.29(a) Amdt 25-72; 25.251(b) Amdt 25-77; 25.301 Amdt 25-23;

25.303 Amdt 25-23; 25.305(a),(b),(e) Amdt 25-86; 25.307(a) Amdt 25-54; 25.321(a),(b) Amdt 25-23; 25.331(a) Amdt 25-91; 25.337(a)-(c) Amdt 25-23; 25.341(a) Amdt 25-72; 25.349(a) Amdt 25-91; 25.351(a) Amdt 25-91; 25.365(a),(c),(d),(e) Amdt 25-87; 25.561(a)-(d) Amdt 25-91; 25.571(a),(b) Amdt 25-86 ,(e)(1) Amdt 25-96; 25.581 Amdt 25-23; 25.601 Amdt 25-0;

25.603(a)-(c) Amdt 25-46; 25.605(a) Amdt 25-46; 25.607(a),(b) Amdt 25-23; 25.609(a),(b) Amdt 25-0; 25.611 Amdt 25-23; 25.613(a),(b) Amdt 25-112; 25-619(a)-(c) Amdt 25-23; 25-625

(a) Amdt 25-72; 25-629(a) Amdt 25-77; 25.841(a) Amdt 25-87; 25.901(c) Amdt 25-46; 25.903

(c) Amdt 25-100; 25.1401(b) Amdt 25-41; 25.1419(a) Amdt 25-72; 25.1529 Amdt 25-54

26.11(c) Amdt 26-0; 26.47 Amdt 26-1.

-----------------------------------------------------END------------------------------------------------------ 4 4 Add Page