| Number |
2007-0218R2 |
| Issued by |
Europe |
| Issue date |
2014-10-10 |
| Effective date |
2014-10-10 |
| EASA approval number |
|
| ATA Chapter |
28 |
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 2007-0218R1 dated 28 February 2011. The original issue of this AD superseded EASA AD 2006-0222 dated 20 July 2006.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A320-28-1159 original issue dated 08 January 2007.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Airbus AFM TR 4.03.00/28 issue 02. |
| PAD number |
07-093 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 13 June 2007 as PAD 07-093 for consultation until 04 July 2007. 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.
|