You are not logged in
  Safety Publications Tool

2016-0108 : Landing Gear – Main Landing Gear Bogie Beam – Inspection / Repair / Modification

Number 2016-0108
Issued by Europe  Europe
Issue date 2016-06-08
Effective date 2016-06-22
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-223F
      • A330-243
      • A330-243F
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2014-0120R1 dated 31 August 2015.
Publication(s) and related information Airbus SB A330-32-3220 original issue dated 10 October 2008, or Revision 01 dated 05 October 2011, or Revision 02 dated 13 December 2012. Airbus SB A330-32-3248 original issue dated 05 October 2011, or Revision 01 dated 13 December 2012, or Revision 02 dated 16 April 2014, or Revision 03 dated 27 November 2015, or Revision 04 dated 05 January 2016. Airbus SB A330-32-3268 original issue dated 20 April 2015. Airbus SB A330-32-3275 original issue dated 23 December 2015. Airbus SB A340-32-4264 original issue dated 10 October 2008. Airbus SB A340-32-4286 original issue dated 05 October 2011, or Revision 01 dated 27 November 2015, or Revision 02 dated 05 January 2016. Airbus SB A340-32-4300 original issue dated 20 April 2015. Airbus SB A340-32-4305 original issue dated 23 December 2015. Messier Bugatti Dowty SB No. A33/34-32-306 original issue dated 21 December 2015. Messier Bugatti Dowty SB No. A33/34-32-305 original issue dated 13 April 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 16-025R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 18 February 2016 as PAD 16-025 for consultation until 17 March 2016 and republished on 27 April 2016 as PAD 16-025R1 for additional consultation until 11 May 2016. The Comment Response Documents can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.