Publication(s) and related information |
Airbus A380 MMEL Revision of January 2021, EASA approval date 11 January 2021.
Airbus SB A380-28-8050 original issue dated 10 September 2015, or Revision 01 dated 09 January 2017, or Revision 02 dated 20 December 2017.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
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Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 27 July 2021 as PAD 21-108 for consultation until 24 August 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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