Number |
2010-0046R1 |
Issued by |
Europe |
Issue date |
2012-05-23 |
Effective date |
2012-06-06 |
EASA approval number |
|
ATA Chapter |
27 |
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 |
This AD revises EASA AD 2010-0046 dated 19 March 2010, which superseded EASA AD 2008-0149 dated 05 August 2008.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A320-27A1186 original issue, dated 23 June 2008.
Airbus SB A320-27A1186 Revision 05, dated 10 March 2010.
Goodrich SB 31075-27-21 Revision 2 dated 04 March 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The required actions and the risk allowance have granted the issuance of a Final AD with Request for Comments, postponing the public consultation process after publication.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|