| Number |
2017-0204R1 |
| Issued by |
 Europe |
| Issue date |
2024-08-21 |
| Effective date |
2024-09-04 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-102
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
A300B4-220
-
A300B4-2C
-
A300C4-203
-
A300F4-203
|
| Revision |
This AD revises EASA AD 2017-0204 dated 12 October 2017.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2013-0248 dated on 14 October 2013.
|
| Publication(s) and related information |
Airbus A300 ALS Part 1 Revision 01 dated 05 September 2013 and Revision 02 dated 28 August 2017.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
17-121 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 31 August 2017 as PAD 17-121 for consultation until 28 September 2017. 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.
|
