Number |
2024-0170 |
Issued by |
Europe |
Issue date |
2024-08-26 |
Effective date |
2024-09-09 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
57 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
-
A300F4-622R
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2017-0023 dated 10 February 2017.
|
Publication(s) and related information |
Airbus SB A300-57-6118 original issue dated 30 June 2015, or Revision 1 dated 31 January 2017, or Revision 2 dated 15 July 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
24-095 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 25 July 2024 as PAD 24-095 for consultation until 22 August 2024. 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.
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.
|