Number |
2022-0094 |
Issued by |
Europe |
Issue date |
2022-05-25 |
Effective date |
2022-06-08 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
30, 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 2019-0251 dated 09 October 2019.
|
Publication(s) and related information |
Airbus A380 AFM TR 206 issue 1 dated 19 February 2019.
Airbus SB A380-36-8062 original issue dated 23 August 2019.
Airbus AOT A36R002-19 original issue dated 26 June 2019.
Airbus SB A380-36-8061 original issued dated 17 November 2021.
Airbus SB A380-30-8008 original issued dated 25 September 2020, or Revision 01 dated 27 September 2021.
Liebherr Aerospace Toulouse SAS (F1958) SB 6746-36-01 original issue dated 08 November 2021.
SAFRAN Aerotechnics (F0553) SB 733474-30-002 original issue dated 19 August 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
22-048 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 April 2022 as PAD 22-048 and closed for consultation on 24 May 2022. No comments were received during the consultation period.
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.
|