| Number |
2010-0120 |
| Issued by |
 Europe |
| Issue date |
2010-06-21 |
| Effective date |
2010-07-05 |
| EASA approval number |
|
| ATA Chapter |
29 |
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 2009-0259 dated 10 December 2009.
|
| Publication(s) and related information |
Airbus AOT (All Operators Telex) No.A320-29A1150 original issue.
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD.
Hamilton Sundstrand Service Bulletin No. ERPS08M-29-8 original issue. |
| 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 Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|
