| Number |
2022-0190 |
| Issued by |
 Europe |
| Issue date |
2022-09-14 |
| Effective date |
2022-09-28 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
54 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A330
-
A330-223
-
A330-321
-
A330-322
-
A330-323
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD F-2004-028R2 (EASA approval 2005-6373) dated 26 October 2005.
|
| Publication(s) and related information |
Airbus SB A330-54-3021 original issue dated 04 February 2004, Revision 01 dated 16 June 2004 and
Revision 02 dated 28 January 2008.
Airbus SB A330-54-3022 original issue dated 25 May 2005 and Revision 01 dated 09 January 2008.
Airbus SB A330-54-3050 original issue dated 08 November 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
22-105 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 01 August 2022 as PAD 22-105 for consultation until 29 August 2022.
The Comment Response Documents 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.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on
a product, part or appliance not affected by this AD, can be reported to the EU aviation safety
reporting system. This may include reporting on the same or similar components, other than
those covered by the design to which this AD applies, if the same unsafe condition can exist or
may develop on an aircraft with those components installed. Such components may be
installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate
(STC) or other modification.
|
