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2025-0030 : Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment

Number 2025-0030
Issued by Europe  Europe
Issue date 2025-02-10
Effective date 2025-02-24
EASA approval number
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
      • 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
      • A321-111
      • 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
      • A321-253NY
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes the EASA AD 2024-0031 dated 31 January 2024, including its Correction dated 01 February 2024, and EASA AD 2024-0208 dated 25 October 2024.
Publication(s) and related information Airbus A318/A319/A320/A321 ALS Part 2 Revision 11 dated 04 November 2024. The use of later approved revisions or variations of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 25-004
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 07 January 2025 as PAD 25-004 for consultation until 04 February 2025. 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.