Number |
2013-0288 |
Issued by |
Europe |
Issue date |
2013-12-06 |
Effective date |
2013-12-20 |
EASA approval number |
|
Contributor |
EASA Large Aeroplane Section |
ATA Chapter |
32 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2011-0069R1 dated 11 April 2012, and EASA Emergency AD 2013-0132-E dated 25 June 2013.
|
Publication(s) and related information |
Airbus AOT A320-32A1390 original issue dated 10 February 2011; SB A320-32-1390 Revision 01 dated 21 September 2011, or Revision 02 dated 23 October 2013; AOT A32N001-13 original issue dated 24 June 2013; SB A320-32-1409 original issue dated 19 March 2013; and SB A320-32-1407 original issue dated 14 May 2013. GE SB 114122-32-105 original issue dated 17 January 2013. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
13-125R2 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 21 August 2013 as PAD 13-125 for consultation until 18 September 2013, republished on 25 September 2013 as PAD 13-125R1 for consultation until 09 October 2013, and republished on 13 November 2013 as PAD 13-125R2 for consultation until 27 November 2013 . 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[dot]eu.
|