Number |
2010-0016R1 |
Issued by |
Europe |
Issue date |
2010-02-09 |
Effective date |
2010-02-10 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Section |
ATA Chapter |
34 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A330
-
A330-201
-
A330-202
-
A330-203
-
A330-223
-
A330-243
-
A330-301
-
A330-302
-
A330-303
-
A330-321
-
A330-322
-
A330-323
-
A330-341
-
A330-342
-
A330-343
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
-
A340-541
-
A340-542
-
A340-642
-
A340-643
|
Revision |
This AD revises EASA AD 2010-0016 dated 27 January 2010. This AD revision is issued to specify that the identification of the affected AoA probes is also possible in accordance with aeroplane maintenance records data analysis.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus Service Bulletin A330-34-3232 at original issue;
Airbus Service Bulletin A340-34-4239 at original issue;
Airbus Service Bulletin A340-34-5072 at original issue.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
Thales Service Bulletin C16291A-34-007 Revision 01 dated 03 December
2009. |
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@easa.europa.eu .
4. For any questions concerning the technical content of the
requirements in this AD, please contact: AIRBUS – Airworthiness
Office – EAL; E-mail: airworthiness.A330-A340@airbus.com .
|