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PAD 26-050 : Flight Controls – Elevator Aileron Computer – Replacement

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Number 26-050
Issued by Europe  Europe
Issue date 2026-04-16
EASA approval number
ATA Chapter 27
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
      • A319-151N
      • A319-153N
      • A319-171N
      • A319-173N
    • 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
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2025-0268-E dated 28 November 2025.
Publication(s) and related information Airbus AOT A27N022-25 Revision 00 (original issue) dated 28 November 2025, Revision 01 dated 28 November 2025 or Revision 02 dated 29 November 2025. Airbus FOT 999.0073/25 Revision 00 dated 29 November 2025, Revision 01 dated 30 November 2025 or Revision 02 dated 02 December 2026. Airbus Service Bulletin A320-27-1315 dated 17 December 2025 Airbus Service Bulletin A320-27-1316 dated 17 December 2025 Airbus Service Bulletin A320-27-1317 dated 17 December 2025 The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. This Proposed AD will be closed for consultation on 30 April 2026. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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