| Number |
2020-0239 |
| Issued by |
 Europe |
| Issue date |
2020-11-04 |
| Effective date |
2020-11-18 |
| EASA approval number |
|
| ATA Chapter |
55 |
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 2018-0116 dated 29 May 2018.
|
| Publication(s) and related information |
Airbus SB A380-55-8002 original issue, dated 13 May 2015, or Revision 01 dated 01 December 2016, or Revision 02 dated 20 April 2018, or Revision 03 dated 24 August 2020.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-156 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 05 October 2020 as PAD 20-156 for consultation until 02 November 2020. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.
|
