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2016-0135 : Landing Gear – Main Landing Gear Hinge Pin – Inspection / Replacement

Number 2016-0135
Issued by Europe  Europe
Issue date 2016-07-08
Effective date 2016-07-22
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • ATR
    • ATR42
      • 200
      • 300
      • 320
      • 400
      • 500
    • ATR72
      • 101
      • 102
      • 201
      • 202
      • 211
      • 212
      • 212A
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2014-0074 dated 21 March 2014.
Publication(s) and related information Messier Bugatti Dowty SB 631-32-213, original issue, dated 16 December 2013, or Revision 1, dated 08 December 2014, or Revision 2, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-214, original issue, dated 13 January 2014, or Revision 1, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-215, original issue, dated 13 January 2014, or Revision 1, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-216, original issue, dated 30 October 2013, or Revision 1, dated 17 December 2013, or Revision 2, dated 08 December 2014, or Revision 3, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-219, original issue, dated 03 March 2014, or Revision 1, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-220, original issue, dated 03 March 2014 or Revision 1, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-224, original issue, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-231, original issue, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-232, original issue, dated 08 December 2014, or Revision 1, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-233, original issue, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-234, original issue, dated 15 March 2016. Messier Bugatti Dowty SB 631-32-235, original issue, dated 15 March 2016. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 16-077
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 24 May 2016 as PAD 16-077 for consultation until 21 June 2016. The Comment Response Document 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.