| Publication(s) and related information |
Airbus SB A380-57-8132 original issue dated 03 February 2017, or Revision 01 dated 10 October 2019.
Airbus SB A380-57-8133 original issue dated 03 February 2017, or Revision 01 dated 23 January 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Airbus SB A380-57-8145 original issue dated 22 July 2016, or Revision 01 dated 26 June 2017.
Airbus SB A380-57-8146 original issue dated 22 July 2016, or Revision 01 dated 26 June 2017. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 April 2021 as PAD 21-057 for consultation until 24 May 2021. 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.
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