Number |
2014-0260 |
Issued by |
Europe |
Issue date |
2014-12-05 |
Effective date |
2014-12-19 |
EASA approval number |
|
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2011-0155R1 dated 31 January 2012.
|
Publication(s) and related information |
Airbus A318/A319/A320/A321 ALS Part 5 Rev.01, approved by EASA on 09 July 2014.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD. |
PAD number |
13-065R1 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 May 2013 as PAD 13-065 for consultation until 19 June 2013 and republished as PAD 13-065R1 on 29 October 2014 for consultation until 26 November 2014. The Comment Response Document can be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|