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2009-0055R1 : Electrical Power – Engine Feeder Harness – Inspection & Nacelles/Pylons – GE CF6-80C2 Pylon Forward Pyramid – Inspection

Number 2009-0055R1
Issued by Europe  Europe
Issue date 2009-04-28
Effective date 2009-03-27
EASA approval number
ATA Chapter 24, 54
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300C4-605R variant F
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-204
      • A310-304
      • A310-308
Revision This AD revises and replaces EASA AD 2009-0055 dated 13 March 2009. This AD has been revised to clarify that modification of an aeroplane prior to the effective date of this AD, in accordance with the original issue of SB A310-54-2039 or SB A300-54-6038 or SB A300-54-9003, also terminates the repetitive inspection and reporting requirements of this AD.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2006-0155 dated 01 June 2006.
Publication(s) and related information AIRBUS Service Bulletins: A310-24-2100 original issue, A300-24-6097 original issue, A300-24-9010 original issue, A310-54-2039 revision 01, A300-54-6038 revision 01, A300-54-9003 revision 01 The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 09-010
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu