Number |
2012-0083 |
Issued by |
Europe |
Issue date |
2012-05-16 |
Effective date |
2012-05-30 |
EASA approval number |
|
ATA Chapter |
35 |
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 2011-0167 dated 06 September 2011.
|
Publication(s) and related information |
Airbus SB A320-35A1047 original issue dated 29 March 2011.
B/E Aerospace SB 1XCXX-0100-35-005 original issue dated 14 March 2011 or Revision 01 dated 15 December 2011. B/E Aerospace SB 22CXX-0100-35-003 original issue dated 17 March 2011 or Revision 01 dated 20 December 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
12-018 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 23 February 2012 as PAD 12-018 for consultation until 22 March 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.eu.
|