Number |
2021-0028 |
Issued by |
Europe |
Issue date |
2021-01-21 |
Effective date |
2021-02-04 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
57 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD 2000-157-145(B) dated 05 April 2000.
|
Publication(s) and related information |
Airbus SB A340-57-4068 original issue dated 12 August 1999, or Revision 01 dated 06 December 1999, or Revision 02 dated 16 May 2000.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 21 December 2020 as PAD 20-206 for consultation until 18 January 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.
|