Number |
2009-0260 |
Issued by |
Europe |
Issue date |
2009-12-14 |
Effective date |
2009-12-24 |
EASA approval number |
|
ATA Chapter |
29 |
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 |
Not applicable
|
Correction |
This AD has been republished to correct some editorial errors.
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A330-29A3110 at original issue.
Airbus AOT A340-29A4085 at original issue.
Airbus AOT A340-500/600-29A5015 at original issue.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
Hamilton Sundstrand SB ERPS06G-29-6.
Hamilton Sundstrand SB ERPS33G-29-1. |
PAD number |
09-122 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 October 2009 as PAD 09-122 for consultation
until 04 November. The Comment Response Document can be found at https://ad.easa.europa.eu/.
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: A330-A340@airbus.com.
|