Number |
2015-0117 |
Issued by |
Europe |
Issue date |
2015-08-07 |
Effective date |
2015-07-08 |
EASA approval number |
|
ATA Chapter |
35 |
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 re-published to correct a template error, removing the word ‘Proposed’ and replacing the acronym ‘PAD’ with ‘AD’.
|
Supersedure |
This AD supersedes EASA AD 2014-0275R1 dated 19 January 2015.
|
Publication(s) and related information |
Airbus AOT A35N006-14 dated 10 December 2014, or Revision 01 dated 17 June 2015.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator. |
PAD number |
15-062 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 May 2015 as PAD 15-062 for consultation until 19 June 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.
|