Safety Publications Tool

2014-0173R1 : Exhaust – Thrust Reverser “J-Ring” at 6 and 12 o'clock Beam – Inspection / Replacement

Number 2014-0173R1
Issued by Europe  Europe
Issue date 2014-09-02
Effective date 2014-09-09
EASA approval number
ATA Chapter 78
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
Revision This AD revises EASA AD 2014-0173 dated 22 July 2014.
Correction Not applicable
Supersedure The original issue of this AD superseded EASA AD 2009-0056 dated 11 March 2009.
Publication(s) and related information Airbus SB A340-78-4029 at original issue dated 14 May 2003, or Revision 01 dated 31 March 2004. Airbus SB A340-78-4030 at original issue dated 14 April 2003, or Revision 01 dated 18 May 2004, or Revision 02 dated 21 March 2006, or Revision 03 dated 13 June 2007, or Revision 04 dated 06 February 2014. Airbus SB A340-78-4033 at original issue dated 13 June 2007 or Revision 01 dated 05 March 2008. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 14-083
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2.The original issue of this AD was posted on 21 May 2014 as PAD 14-083 for consultation until 18 June 2014. The Comment Response Document can be found at https://ad.easa.europa.eu/. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.