Safety Publications Tool
2021-0175 : [Correction] Landing Gear – Main Landing Gear Sliding Tubes – Inspection
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD is republished to correct an error in Group 1 definition.
This AD supersedes EASA AD 2020-0258 dated 18 November 2020, including its Correction dated 19 November 2020.
Publication(s) and related information
Airbus SB A320-32-1461 original issue dated 11 April 2018. Airbus AOT A32N020-20 original issue dated 17 June 2020. Airbus AOT A32N022-20 original issue dated 15 October 2020, or Revision 01 dated 16 November 2020. Airbus AOT A32N023-21 original issue dated 05 May 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 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.
EASA_AD_2021_0175_C1.pdf (269 kb)
EASA_AD_2021_0175.zip (540 kb)
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