| Number |
2021-0280R1 |
| Issued by |
 Europe |
| Issue date |
2024-11-08 |
| Effective date |
2024-11-08 |
| EASA approval number |
|
| ATA Chapter |
36 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
| Revision |
This AD revises EASA AD 2021-0280 dated 17 December 2021.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2020-0286 dated 18 December 2020.
|
| 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.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-171 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 23 November 2021 as PAD 21-171 for consultation until 07 December 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.
|
