| Number |
2018-0229 |
| Issued by |
 Europe |
| Issue date |
2018-10-23 |
| Effective date |
2018-11-06 |
| EASA approval number |
|
| ATA Chapter |
57 |
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
-
A300-600ST (Beluga)
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2017-0210 dated 24 October 2017.
|
| Publication(s) and related information |
Airbus SB A300-57-6049 Revision 08 dated 04 July 2017.
Airbus SB A300-57-6050 Revision 03 dated 31 May 2001.
Airbus SB A300-57-6069 original issue dated 08 June 2000, or Revision 01 dated 30 October 2003, or Revision 02 dated 22 December 2006.
Airbus SB A300-57-6086 Revision 05 dated 30 January 2012 and Revision 06 dated 04 July 2017.
Airbus SB A300-57-6113 original issue dated 25 April 2016.
Airbus SB A300-57-6119 original issue dated 25 April 2016.
Airbus SB A300-57-6121 original issue dated 31 August 2018.
Airbus SB A300-57-9016 original issue dated 13 June 2005.
Airbus SB A300-57-9001 Revision 01 dated 22 August 2017.
Airbus SB A300-57-9002 Revision 02 dated 22 August 2017.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
18-122R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 06 September 2018 as PAD 18-122, and republished as PAD 18-122R1 on 17 September 2018 for consultation until 04 October 2018. 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.
|
