| Number |
2026-0036 |
| Issued by |
 Europe |
| Issue date |
2026-02-25 |
| Effective date |
2026-03-11 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0080 dated 26 March 2024.
|
| Publication(s) and related information |
Airbus A330-700L ALS Part 2, DT-ALI, Revision 02 dated 19 December 2025.
The use of later approved revisions of the above-mentioned document, or of variations to the above-mentioned document which include the content of above-mentioned document, is acceptable for compliance with the requirements of this AD. |
| PAD number |
26-012 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 23 January 2026 as PAD 26-012 for consultation until 20 February 2026. 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.
|
