Safety Publications Tool

2022-0026 : SUPERSEDED BY EASA AD 2023-0029

Number 2022-0026
Issued by Europe  Europe
Issue date 2022-02-16
Effective date 2022-03-02
EASA approval number
ATA Chapter 25
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
      • A320-271N
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
      • A321-251N
      • A321-253N
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2018-0255 dated 27 November 2018 and EASA AD 2019-0106 dated 15 May 2019.
Publication(s) and related information Airbus SB A320-25-1BF6 original issue dated 30 May 2017, or rev. 01 dated 27 December 2017. Airbus SB A320-25-1BHG original issue dated 03 July 2017. Airbus SB A320-25-1BK9 original issue dated 06 June 2018, or rev. 01 dated 02 April 2019, or rev. 02 dated 28 May 2020. Airbus SB A320-25-1BKK original issue dated 06 June 2018. Airbus SB A320-25-1BCB original issue dated 06 April 2016. Zodiac Galleys Europe SB 213510-25-001 rev. A dated 04 August 2017, or rev. B dated 23 April 2018, or rev. C dated 11 June 2018, or rev. D dated 15 August 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-128R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 31 August 2020 as PAD 20-128 for consultation until 28 September 2020, and republished as PAD 20-128R1 on 07 October 2020 for additional consultation until 04 November 2021. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the 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.