| Number |
2020-0051 |
| Issued by |
 Europe |
| Issue date |
2020-03-11 |
| Effective date |
2020-03-25 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
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 2016-0249 dated 14 December 2016, including its correction dated 10 January 2017.
|
| Publication(s) and related information |
Airbus SB A300-53-6125 original issue dated 08 November 2000, or Revision 01 dated 13 June 2003, or Revision 02 dated 25 February 2005, or Revision 03 dated 13 September 2011, or Revision 04 dated 17 March 2015.
Airbus SB A300-53-6178 original issue dated 17 March 2015, or Revision 01 dated 20 September 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-028 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 06 February 2020 as PAD 20-028 for consultation until 05 March 2020. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs@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.
|
