Safety Publications Tool

2007-0242R1 : Wings - Outer Wings Structural Fatigue - Inspection/Modification

Number 2007-0242R1
Issued by Europe  Europe
Issue date 2017-05-08
Effective date 2017-05-22
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision This AD revises EASA AD 2007-0242 dated 04 September 2007.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A310-57-2002 Revision 02 dated 04 January 1996, or Revision 03 dated 28 November 2006. Airbus A310-57-2003 original issue dated 20 August 1986, or Revision 01 dated 10 September 1986, or Revision 02 dated 21 October 1986, or Revision 03 dated 16 October 2006. Airbus A310-57-2005 original issue dated 28 March 1985, or Revision 01 dated 17 June 1985, or Revision 02 dated 11 October 1985, or Revision 03 dated 02 October 2006. Airbus A310-57-2006 Revision 03 dated 02 May 2006, or Revision 04 dated 21 May 2007. Airbus A310-57-2032 Revision 03 dated 04 January 1996, or Revision 04 dated 01 December 2006. Airbus A310-57-2046 Revision 07 dated 02 April 1999, or Revision 08 dated 01 December 2006. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 07-131
Remarks 1. If requested and appropriately substantiated, EASA can accept Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 06 August 2007 as PAD 07-131 for consultation until 03 September 2007. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the AD Focal Point -Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.