| Number |
2015-0021 |
| Issued by |
Europe |
| Issue date |
2015-02-13 |
| Effective date |
2015-02-27 |
| EASA approval number |
|
| ATA Chapter |
71 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A321
-
A321-111
-
A321-112
-
A321-211
-
A321-212
-
A321-213
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2013-0050 dated 05 March 2013.
|
| Publication(s) and related information |
Airbus AOT A71N001-12, Revision 01 dated 09 August 2012, or Revision 02 dated 27 February 2013.
Airbus SB A320-71-1060 dated 09 October 2014.
Goodrich Aerostructures SB RA32071-146, Revision 2 dated 26 July 2012.
Goodrich Aerostructures SB RA32071-160, original issue dated 18 September 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
15-001 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 09 January 2015 as PAD 15-001 for consultation until 06 February 2015. The Comment Response Document can be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|