| Number |
2024-0189 |
| Issued by |
 Europe |
| Issue date |
2024-10-01 |
| Effective date |
2024-10-15 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2022-0124 dated 28 June 2022.
|
| Publication(s) and related information |
Airbus A350 ALS Part 1 Revision 08, Issue 2 dated 01 August 2024.
The use of later approved revisions or variations of the above-mentioned document is acceptable
for compliance with the requirements of this AD. |
| PAD number |
24-101R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 15 August 2024 as PAD 24-101 for consultation until 12 September 2024 and republished on 16 September 2024 as PAD 24-101R1 for additional consultation until 30 September 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.
|
