Number |
2016-0204 |
Issued by |
Europe |
Issue date |
2016-10-19 |
Effective date |
2016-10-27 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
92 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
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
|
Revision |
Not applicable
|
Correction |
This AD is republished to add two missing models to the applicability (the respective MSN were already listed in the original AD) and to correct the battery rod Part Number (P/N).
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A92N001-16 original issue dated 25 August 2016 or Revision 01 dated 10 October 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|