Number |
2015-0119 |
Issued by |
Europe |
Issue date |
2016-01-12 |
Effective date |
2015-07-08 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
35 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A330
-
A330-201
-
A330-202
-
A330-203
-
A330-223
-
A330-223F
-
A330-243
-
A330-243F
-
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 was republished to correct a typographical error in the applicability.
|
Supersedure |
This AD supersedes EASA AD 2014-0277 dated 19 December 2014.
|
Publication(s) and related information |
Airbus AOT A35L007-14 original issue dated 18 December 2014, or Revision
01 dated 17 June 2015.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
B/E Aerospace SIL D1019-01 Revision 1 dated 03 January 2000, provides
instructions for the activation and the disposal of a removed generator. |
PAD number |
15-065 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 May 2015 as PAD 15-065 for consultation until
19 June 2015. 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.eu.
|