Safety Publications Tool

2025-0120 : Cabin Systems – Antenna Adapter Plate – Inspection

Number 2025-0120
Issued by Europe  Europe
Issue date 2025-05-26
Effective date 2025-06-09
EASA approval number
ATA Chapter 44
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
      • A320-251N
      • A320-252N
      • A320-253N
      • A320-271N
      • A320-272N
      • A320-273N
    • A321
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
      • A321-251N
      • A321-251NX
      • A321-252N
      • A321-252NX
      • A321-253N
      • A321-253NX
      • A321-253NY
      • A321-271N
      • A321-271NX
      • A321-271NY
      • A321-272N
      • A321-272NX
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-243
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
      • A330-841
      • A330-941
    • A350
      • A350-1041
      • A350-941
    • A380
      • A380-841
      • A380-842
      • A380-861
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2024-0199 dated 18 October 2024.
Publication(s) and related information Airbus SB A320-44-1102 original issue dated 22 December 2023. Airbus SB A320-44-1103 original issue dated 22 December 2023 or Revision 01 dated 29 April 2025. Airbus SB A330-44-3054 original issue dated 22 December 2023, Revision 01 dated 11 July 2024 or Revision 02 dated 26 March 2025. Airbus SB A350-44-P090 original issue dated 22 December 2023 or Revision 01 dated 31 March 2025. Airbus SB A380-44-8145 Revision 1 dated 22 April 2024, Revision 01 dated 22 April 2024 or Revision 02 dated 15 April 2025. Panasonic SB RDAA903008-01-44-00 Revision 1 dated 14 December 2023, Revision 2 dated 23 April 2024 or Revision 3 dated 07 April 2025. Panasonic SB RDAA903141-01-44-00 Revision 1 dated 18 December 2023 or Revision 02 dated 23 April 2024. Panasonic SB RDAA903194-01-44-00 Revision 1 dated 14 December 2023 or Revision 02 dated 03 May 2024. Panasonic SB RDAA903366-01-44-00 Revision 2 dated 21 December 2023, Revision 3 dated 03 May 2024 or Revision 04 dated 20 March 2025. Panasonic SB RDAA903465-01-44-00 Revision 1 dated 19 December 2023 or Revision 2 dated 23 April 2024. Panasonic SB RDAA903528-01-44-00 Revision 1 dated 19 December 2023 or Revision 02 dated 22 April 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. All interested persons may send their comments, referencing the AD Number, to the E-mail address specified in below Remark 3, prior to 23 June 2025. Only if any comment is received during the consultation period, a Comment Response Document will be published in the EASA Safety Publications Tool, in a compressed ('zipped') file, attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.

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