Number |
2017-0203 |
Issued by |
Europe |
Issue date |
2017-10-12 |
Effective date |
2017-10-26 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-601
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
-
A300F4-622R
-
A300-600ST (Beluga)
-
A310
-
A310-203
-
A310-203C
-
A310-204
-
A310-221
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2013-0072 dated 20 March 2013, including its correction dated 15 January 2015.
|
Publication(s) and related information |
Airbus A300-600 ALS Part 3 original issue dated 18 April 2012 and Revision 01 dated 28 August 2017.
Airbus A310 ALS Part 3 original issue dated 30 November 2012 and Revision 01 dated 28 August 2017.
The use of later approved variations or revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
17-120 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 31 August 2017 as PAD 17-120 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.
|