Number |
2016-0114 |
Issued by |
Europe |
Issue date |
2016-06-23 |
Effective date |
2016-06-29 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
28 |
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 |
This AD is republished to remove a misleading adjective in paragraph (5) or the Required Action(s) and Compliance Time(s).
|
Supersedure |
This AD supersedes EASA AD 2014-0234R1, dated 11 December 2014.
|
Publication(s) and related information |
Airbus SB A320-28-1221 Revision 2, dated 11 January 2016. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
ZODIAC Aerotechnics SB 786073-28-002, original issue, dated 13 June 2014. |
PAD number |
16-061 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 04 May 2016 as PAD 16-061 for consultation until 01 June 2016. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|