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2007-0297R1 : Fuselage - Rear/Aft Pressure Bulkhead Attachment Angles - Modification and Inspection Program

Number 2007-0297R1
Issued by Europe  Europe
Issue date 2008-09-17
Effective date 2007-12-24
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300-600
      • A300B4-620
      • A300C4-620
    • A310
      • A310-203
      • A310-222
Revision This AD revises EASA AD 2007-0297 dated 10 December 2007. This AD has been revised to remove an inappropriate reference regarding the normal inspection program from the Compliance section, Note 3.
Correction N/A
Supersedure This AD replaces EASA AD 2007-0297 dated 10 December 2007. The original issue of this AD superseded EASA AD 2007-0157 dated 04 June 2007.
Publication(s) and related information Airbus Service Bulletins: A300-53-6005 original issue, Revision 01, 02, 03 or 04 A300-53-6006 original issue, Revision 01, 02 or 03 A310-53-2024 original issue, Revision 01, 02, 03, 04 or 05 A310-53-2025 original issue, Revision 01, 02, 03, 04, 05 or 06 The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 07-211
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu