Number |
2024-0095 |
Issued by |
Europe |
Issue date |
2024-04-30 |
Effective date |
2024-05-14 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS DEFENCE & SPACE S.A.
-
EASA STC 10029272
-
EASA STC 10034690
-
EASA STC 10035945
-
EASA STC 10063084
-
EASA STC 10064192
-
STC EASA.A.S.02790
-
AIRBUS S.A.S.
-
A330
-
A330-202
-
A330-203
-
A330-243
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
ADS SB A330MRTT-53-0048 original issue dated 21 January 2022, or Revision 01 dated 29 January 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
Airbus SB A330-53-3303 original issue dated 12 July 2021, or Revision 01 dated 24 September 2021, or Revision 02 dated 07 June 2023.
Airbus SB A330-53-3275 original issue dated 08 September 2017, or Revision 01 dated 20 December 2018, or Revision 02 dated 28 April 2021. |
PAD number |
24-037 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 27 March 2024 as PAD 24-037 for consultation until 24 April 2024.
No comments were received during the consultation period.
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.
|