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2014-0280 : SUPERSEDED BY EASA AD 2015-0118

Number 2014-0280
Issued by Europe  Europe
Issue date 2014-12-19
Effective date 2014-12-24
EASA approval number
Contributor EASA Large Transport Aeroplanes
ATA Chapter 35
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
      • A300F4-622R
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus AOT A35W008-14 dated 18 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.