| Number |
2021-0017 |
| Issued by |
 Europe |
| Issue date |
2021-01-14 |
| Effective date |
2021-01-28 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS
-
A340
-
A340-211
-
A340-213
-
A340-311
-
A340-312
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD 98-026-079(B) dated 28 January 1998.
|
| Publication(s) and related information |
Airbus SB A340-53-4053 original issue dated 14 May 1996, or Revision 01 dated 13 August 1997, or Revision 02 dated 11 September 1998.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
|
| PAD number |
20-196 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 14 December 2020 as PAD 20-196 for consultation until 11 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.
|
