| Publication(s) and related information |
Airbus SB A380-57-8148 Revision 01 dated 06 February 2020.
Airbus SB A380-57-8269 original issue dated 06 February 2020.
Airbus RI R575-40267 original Issue (Issue A) dated 11 December 2017, or Issue B dated 28
November 2024.
Airbus RI R575-42389 original Issue (Issue A) dated 20 February 2025, or Issue B dated 04 March 2025.
Airbus RI R575-42397 original Issue (Issue A) dated 18 March 2025.
Airbus RI R575-58442 original Issue (Issue A) dated June 2016, or Issue B dated August 2017, or Issue C dated December 2017, or Issue D dated 26 November 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
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.
All interested persons may send their comments, referencing the AD Number, to the E-mail
address specified in below Remark 3, prior to 05 May 2025. Only if any comment is received
during the consultation period, a Comment Response Document will be published in the EASA
Safety Publications Tool, in a 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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