Safety Publications Tool

2014-0049R2 : Wings – Movable Flap Track Fairing Number 3 and 4 Bracket Assemblies and Fasteners – Inspection / Replacement / Modification

Number 2014-0049R2
Issued by Europe  Europe
Issue date 2016-09-27
Effective date 2016-09-27
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A380
      • A380-841
      • A380-842
      • A380-861
Revision This AD revises EASA AD 2014-0049R1 dated 13 July 2016, the original issue of which superseded EASA AD 2011-0215 dated 04 November 2011.
Correction Not applicable
Supersedure This original issue of this AD superseded EASA AD 2011-0215 dated 04 November 2011.
Publication(s) and related information Airbus SB A380-57-8028 original issue dated 20 July 2011. Airbus SB A380-57-8030 original issue dated 20 July 2011. Airbus SB A380-57-8045 original issue dated 06 December 2013. Airbus SB A380-57-8059 original issue dated 31 January 2014. Airbus SB A380-57-8121 original issue dated 02 March 2016, or Revision 01 dated 15 August 2016. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. Airbus Technical Disposition TD/L57D13006165 issue A dated 13 February 2013. Airbus Technical Disposition TD/L57D13006366 issue A dated 13 February 2013.
PAD number 14-033
Remarks 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 07 February 2014 as PAD 14-033 for consultation until 21 February 2014. No comment were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.