Number |
2017-0215 |
Issued by |
Europe |
Issue date |
2017-10-24 |
Effective date |
2017-11-07 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
05 |
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
-
A320-251N
-
A320-271N
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
-
A321-251N
-
A321-253N
-
A321-271N
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2012-0008 dated 16 January 2012 and EASA AD 2014-0141 dated 04 June 2014.
|
Publication(s) and related information |
Airbus ALS Part 1 Revision 05 dated 06 April 2017, or Airbus ALS Part 1 Revision 05 issue 02 dated 19 April 2017.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD. |
PAD number |
16-134R1 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 September 2016 as PAD 16-134 for consultation until 17 October 2016, and republished on 26 June 2017 as PAD 16-134R1 for additional consultation until 24 July 2017. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|