| Number |
2020-0248 |
| Issued by |
 Europe |
| Issue date |
2020-11-17 |
| Effective date |
2020-11-25 |
| EASA approval number |
|
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
This AD has been republished to correct the Applicability by removing aeroplane models which are not associated with an affected aeroplane MSN.
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A340-27-5049 original issue dated 03 April 2010.
Airbus SB A340-28-5048 Revision 01 dated 28 April 2010.
Airbus SB A340-31-5043 original issue dated 02 February 2010, or Revision 01 dated 22 November 2010.
Airbus SB A340-32-5107 original issue dated 21 October 2011.
Airbus SB A340-53-4117 original issue 09 March 1999, or Revision 01 dated 15 February 2001.
Airbus SB A340-53-5038 original issue dated 10 August 2007.
Airbus SB A340-57-5023 original issue dated 25 June 2008, or Revision 01 dated 21 November 2008.
Airbus TD 70540014/005/2010 original issue dated 30 May 2014.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-145 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 23 September 2020 as PAD 20-145 for consultation until 21 October 2020. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.
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