Number |
2012-0118 |
Issued by |
Europe |
Issue date |
2012-07-04 |
Effective date |
2012-07-18 |
EASA approval number |
|
ATA Chapter |
53 |
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 2007-0161 dated 11 June 2007.
|
Publication(s) and related information |
Airbus SB A320-53-1195 Revision 03, dated 08 November 2011.
Airbus SB A320-53-1196 Revision 02, dated 08 November 2011.
Airbus A318/A319/A320/A321 ALI document reference AI/SE-M4/95A.0252/96 issue 11, approved by EASA on 09 November 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
12-039 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 30 April 2012 as PAD 12-039 for consultation until 28 May 2012. 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[dot]eu.
|