# STC ST04624NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Aeroconseil, France - Description: Installation of the GEE ARINC 791 Ku Band Satellite Communication Antenna - Applied: May 15, 2020 - Status date: March 11, 2022 - Product: Aircraft, Large Airplane - Certification basis: Part 3, Part 21, Part 25 - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) - Certificate PDF: https://openairdocs.org/files/sha256/60/ff/60ffa70b8416d549d3d956faa5fdf26c275d27fc155000cf1ac7924c11ae2dc0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7C2533FC005AFDEC8625880600424F04.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST04624NY ## ADs that name it (0) None. ## Approved models (21) - Airbus SAS A319-111 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-112 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-113 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-115 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-131 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-132 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A319-133 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-211 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-212 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-214 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-216 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-231 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-232 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A320-233 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-111 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-112 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-131 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-211 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-213 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-231 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) - Airbus SAS A321-232 ([TCDS A28NM](https://openairdocs.org/tcds/A28NM)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. **IMPORT ST04624NY** AEROCONSEIL 7 BOULEVARD HENRI ZIEGLER BLAGNAC CEDEX FRANCE 31700 Part 25 Title 14 Code of Federal Regulations A28NM Airbus SAS A318 Model -111, A318 Model -112, A319 Model -111, A319 Model -112, A319 Model -113, A319 Model -114, A319 Model -115, A319 Model -131, A319 Model -132, A319 Model -133; A320 Model -211, A320 Model -212, A320 Model -214, A320 Model -216, A320 Model -231, A320 Model -232, A320 Model -233, A321 Model -111, A321 Model -112, A321 Model -131, A321 Model -211, A321 Model -212, A321 Model -213, A321 Model -231, A321 Model -232 1. Installation of the GEE ARINC 791 Ku Band Satellite Communication Antenna Provisions in accordance with Aeroconseil Master Data List 0874-01-A-MDL-R01 (Revision R01) dated August 02, 2019, or later EASA approved revisions. 2. Maintenance must be in accordance with Aeroconseil Instructions for Continued Airworthiness (ICA) as follows: (See Description of Type Design Change Continued on Page 3 of 4) 1. This STC must be installed in conjunction with STC ST04630NY. (See Limitations and Conditions Continued on Page 3 of 4) May 15, 2020 April 22, 2021 March 11, 2022 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4 **IMPORT ST04624NY 4** IMPORT ST04624NY Date Amended: March 11, 2022 Description of Type Design Change (continued): a. For Model A319/A320/A321, ICA No. 0874-01-A-ICA-R01 (Revision 01) dated October 5, 2018, or later accepted EASA revisions. b. For Model A318, ICA No. 0874-01-A-ICA-F03-R02 (Revision 02) dated October 21, 2021, or later EASA accepted revisions. 3. Operation must be in accordance with Aeroconseil Aircraft Flight Manual Supplement 0874-01-A-AFMS-R00 (Revision R00) dated July 10, 2019, or later EASA approved revisions. 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission. 4. This modification is compatible with Extended Service Goal, as described in Section 3.2 of Aeroconseil ICA No. 0874-01-A-ICA-R01. 5. Models already fitted with ARINC 791 provisions for the installation of a dorsal large Satellite Communication Antenna between frames FR58 and FR63 are excluded. 6. Maintenance must be in accordance with the EASA approved "Airworthiness Limitations" section of the Aeroconseil ICAs referenced in item 2 under the description of type design change section of this STC. 7. Operation must be in accordance with the "Limitations and Specific Conditions" section of the Aeroconseil Aircraft Flight Manual referenced in item 3 under the description of type design change section of this STC. 8. This STC is applicable to all serial numbers for this Make-Model. 9. This approval is limited to only the installation of equipment provisions. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards. See Certification Basis on page 4 of 4 3 4 IMPORT ST04624NY Date Amended: March 11, 2022 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 Model A318/A319/A320/A321 is as follows: a. The type certified basis for parts not changed or not affected by the change is shown on TCDS A28NM. b. The modification certification basis for parts changed or affected by the change is shown on TCDS A28NM including 14 CFR part 25 as amended by Amendment 25-59 with the following exceptions: i. Regulations at Amendment 25-123: 14 CFR ยงยง 25.1, 25.23, 25.29, 25.121, 25.301 25.303, 25.305, 25.307, 25.321, 25.337, 25.365, 25.561, 25.571, 25.581, 25.601, 25.603, 25.605, 25.607, 25.609, 25.611, 25.613, 25.619, 25.625, 25.629, 25.631, 25.843, 25.899, 25.1301, 25.1401, 25.1419, 25.1501, 25.1529, 25.1541, 25.1587. ii. F-1 ELOS For 25.251 Vibe & Buffet Flight Test a. For Airbus A319/A320/A321: ELOS Memo ST09168NY-T-F-1 dated November 6, 2020. b. For Airbus A318: ELOS Memo SA09776NY-T-F-1 dated February 4, 2022. ----------END---------- 4 4 ## Every issue (2) - March 11, 2022: Amended, Current. [certificate](https://openairdocs.org/files/sha256/60/ff/60ffa70b8416d549d3d956faa5fdf26c275d27fc155000cf1ac7924c11ae2dc0) - April 22, 2021: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ce/70/ce70b8eb6a2cb9ec8954e83a893ccf3cc505e98bbcb1b95ab8d9d0b4ac9a3a38) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.