Number |
2017-0246R1 |
Issued by |
Europe |
Issue date |
2018-04-06 |
Effective date |
2018-04-13 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
27 |
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
|
Revision |
This AD revises EASA AD 2017-0246 dated 11 December 2017.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A330-27-3222 original issue dated 16 February 2017.
Airbus SB A330-27-3223 original issue dated 06 June 2017.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
AOA Sensor P/N - Captain AOA Sensor P/N - First Officer AOA Sensor P/N - Standby
C16291AB or C16291AA C16291AB or C16291AA
C16291AB, C16291AA,
0861ED or 0861ED2
Note 4: For AOA Sensor P/N C16291AA, the DET and a functional heating test of each sensor must
be accomplished as required by paragraph (3) of EASA AD 2015-0134.
Credit:
(3) An aeroplane modified as required by paragraph (1) of this AD remains compliant with the
modification requirements of paragraph (1) of EASA AD 2015-0124 (any revision) for that
aeroplane.
Part Installation Prohibition:
(4) Do not install on an aeroplane any software or hardware of a version earlier than the one listed
in Table 1 of this AD, as required by paragraph (4.1) or (4.2) of this AD, as applicable.
(4.1) For Group 1 aeroplanes: After modification of the aeroplane as required by paragraph
(1) of this AD.
(4.2) For Group 2 aeroplanes: From 25 December 2017 [the effective date of the original issue
of this AD]. |
PAD number |
17-153 |
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 24 October 2017 as PAD 17-153 for consultation until 21 November 2017. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|