| Number |
2011-0155R1 |
| Issued by |
Europe |
| Issue date |
2012-01-31 |
| Effective date |
2011-11-29 |
| 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 |
This AD revises EASA AD 2011-0155 dated 25 August 2011, which superseded EASA AD 2006-0203 dated 11 July 2006.
|
| Correction |
This AD has been republished to correct paragraph (2), referencing the effective date of the original issue of this AD.
|
| Supersedure |
None
|
| Publication(s) and related information |
AIRBUS A318/A319/A320/A321 FAL Document reference 95A.1931/05 issue 4, approved by EASA on 26 August 2010.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
11-050R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 11 May 2011 as PAD 11-050 for consultation until 08 June 2011 and republished as PAD 11-050R1 on 21 July 2011 and officially closed for comments on 04 August 2011. 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.
|