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2014-0275R1 : SUPERSEDED BY EASA AD 2015-0117

Number 2014-0275R1
Issued by Europe  Europe
Issue date 2015-01-19
Effective date 2015-01-19
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 This AD revises EASA AD 2014-0275 dated 19 December 2014.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus AOT A35N006-14 dated 10 December 2014. 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.
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 Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.