Number |
2021-0051 |
Issued by |
Europe |
Issue date |
2021-02-26 |
Effective date |
2021-03-09 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
27 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
Revision |
Not applicable
|
Correction |
This AD is republished to correct an error in paragraph (2).
|
Supersedure |
This AD supersedes EASA AD 2019-0310R1 dated 20 April 2020.
|
Publication(s) and related information |
Airbus SB A380-27-8068 original issue dated 12 December 2019.
Airbus SB A380-27-8070 original issue dated 06 January 2021.
Airbus SB A380-31-8108 original issue dated 06 January 2021.
Airbus SB A380-31-8109 original issue dated 06 January 2021.
Airbus A380 MMEL MER, approved 03 December 2019.
Airbus A380 AFM TR 208 issue 1.0, approval date 03 December 2020.
Airbus FOT Ref. 999.0072/20 original issue dated 18 January 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
|
PAD number |
21-003 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 22 January 2021 as PAD 21-003 for consultation until 19 February 2021.
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.
|