Safety Publications Tool
2017-0047 : Hydraulic Power – Module Plate Assembly – Inspection / Modification
EASA approval number
EASA Medium Rotorcraft Section
/ Type Designation
AIRBUS HELICOPTERS DEUTSCHLAND
MBB-BK 117 C-2 (EC145)
MBB-BK 117 C-2e (EC145)
MBB-BK 117 D-2 (H145)
MBB-BK 117 D-2m
This AD supersedes EASA AD 2015-0210R2, dated 02 December 2016.
Publication(s) and related information
Airbus Helicopters ASB MBB-BK117 C-2-29A-003 original issue dated 12 October 2015, or Revision 1 dated 14 October 2016, or Revision 2 dated 01 February 2017. Airbus Helicopters ASB MBB-BK117 D-2-29A-001 original issue dated 12 October 2015, or Revision 1 dated 14 October 2016, or Revision 2 dated 01 February 2017. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 08 February 2017 as PAD 17-020 for consultation until 08 March 2017. The Comment Response Document can be found at http://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.
EASA_AD_2017_0047.pdf (434 kb)
EASA_PAD_17_020.zip (1 mb)
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