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ADs [at] easa.europa [dot] eu
|
| Number |
26-125 |
| Issued by |
 Europe |
| Issue date |
2026-10-15 |
| EASA approval number |
|
| ATA Chapter |
36 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0280R1 dated 08 November 2024.
|
| Publication(s) and related information |
Airbus AOT A36R003-20 original issue dated 20 July 2020, or Revision 01 dated 24 November 2020.
Airbus SB A380-36-8086 original issue dated 17 September 2021.
Airbus SB A380-28-8074 original issue dated 30 April 2021.
Airbus SB A380-28-8075 original issue dated 30 April 2021.
Airbus SB A380-28-8076 original issue dated 30 April 2021.
Airbus SB A380-28-8077 original issue dated 30 April 2021.
Airbus SB A380-28-8078 original issue dated 30 April 2021.
Airbus SB A380-28-8079 original issue dated 30 April 2021.
Airbus SB A380-28-8080 original issue dated 30 April 2021.
Airbus SB A380-28-8081 original issue dated 30 April 2021.
Airbus SB A380-36-8089 original issue dated 07 July 2026.
Airbus SB A380-36-8090 original issue dated 07 July 2026.
Airbus SB A380-36-8091 original issue dated 07 July 2026.
Airbus SB A380-36-8092 original issue dated 07 July 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
This Proposed AD will be closed for consultation on 01 November 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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