Number |
2014-0213R1 |
Issued by |
Europe |
Issue date |
2022-04-22 |
Effective date |
2022-04-29 |
EASA approval number |
|
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
Revision |
This AD revises EASA AD 2014-0213 dated 19 September 2014.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A380-53-8074 original issue dated 30 July 2014, or Revision 01 dated 05 February 2015, or Revision 02 dated 01 April 2020, or Revision 03 dated 09 September 2021.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
Airbus TD_G1_S4_04931_2013 Issue C dated 23 October 2013.
Airbus TD_G1_S4_05440_2013 Issue A dated 06 November 2013.
Airbus TD_G1_S4_05583_2013 issue A dated 21 November 2013. |
PAD number |
14-134 |
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 02 September 2014 as PAD 14-134 for consultation until 16 September 2014. 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.
|