| Number |
2011-0167 |
| Issued by |
Europe |
| Issue date |
2011-09-06 |
| Effective date |
2011-09-20 |
| EASA approval number |
|
| ATA Chapter |
35 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
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 |
None
|
| Publication(s) and related information |
Airbus SB A320-35A1047 original issue dated 29 March 2011.
B/E Aerospace SB 1XCXX-0100-35-005 dated 14 March 2011.
B/E Aerospace SB 22CXX-0100-35-003 dated 17 March 2011.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
11-075 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 21 July 2011 as PAD 11-075 for consultation until
18 August 2011. The Comment Response Documents 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.
|