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  Safety Publications Tool

2024-0188 : Landing Gear – Nose Landing Gear Shock Absorber – Functional Check

Number 2024-0188
Issued by Europe  Europe
Issue date 2024-09-27
Effective date 2024-10-04
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 32
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A350
      • A350-1041
      • A350-941
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus AOT A32P031-24 original issue dated 18 April 2024, Revision 01 dated 29 July 2024, or Revision 2 dated 28 August 2024, Revision 03 dated 26 September 2024. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
PAD number 24-107
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 29 August 2024 as PAD 24-107 for consultation until 12 September 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.