Safety Publications Tool

2023-0167 : Landing Gear – Main Landing Gear Axles – Inspection

Number 2023-0167
Issued by Europe  Europe
Issue date 2023-08-30
Effective date 2023-09-13
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 32
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-223F
      • A330-243
      • A330-243F
      • A330-301
      • A330-302
      • A330-303
      • A330-323
      • A330-342
      • A330-343
      • A330-743L (BelugaXL)
      • A330-841
      • A330-941
    • A340
      • A340-312
      • A340-313
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A330-32-3305 original issue dated 22 May 2023. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 23-068
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 16 June 2023 as PAD 23-068 for consultation until 30 June 2023. 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.