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2024-0031 : [Correction] Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment

Number 2024-0031
Issued by Europe  Europe
Issue date 2024-02-01
Effective date 2024-02-14
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 05
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
      • A319-151N
      • A319-153N
      • A319-171N
    • 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
      • A321-111
      • A321-112
      • A321-131
      • 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 This AD is republished to correct two typographical errors.
Correction Not applicable
Supersedure This AD supersedes EASA AD 2022-0085 dated 12 May 2022, EASA AD 2023-0008 dated 16 January 2023, and EASA AD 2023-0151 dated 25 July 2023.
Publication(s) and related information Airbus A318/A319/A320/A321 ALS Part 2 Revision 10 issue 02 dated 30 November 2023, or ALS Part 2 Revision 10 issue 03 dated 19 December 2023. The use of later approved variations or revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 23-145
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 14 December 2023 as PAD 23-145 for consultation until 11 January 2024. The Comment Response Document 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.