Safety Publications Tool
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2012-0170R2 : SUPERSEDED BY EASA EMERGENCY AD 2016-0097-E
EASA approval number
EASA Rotorcraft Section
/ Type Designation
SA 365/366 / AS 365 / EC 155
SA 366 G1
This AD revises EASA AD 2012-0170R1, dated 18 October 2013.
Publication(s) and related information
Eurocopter AS365 ASB No. 05.00.54 Revision 4 dated 16 May 2011.Eurocopter AS365 ASB No. 05.00.61 Revision 2 dated 05 July 2012, or Revision 3 dated 25 June 2013, or Airbus Helicopters AS365 ASB No. 05.00.61 Revision 4 dated 08 April 2014. Eurocopter AS365 SB No. 65.00.17 Revision 1 dated 21 March 2011. Eurocopter SA366 ASB No. 05.37 Revision 4 dated 16 May 2011. Eurocopter SA366 ASB No. 05.41 Revision 2 dated 05 July 2012. Eurocopter SA366 SB No. 65.04 Revision 1 dated 21 March 2011. Eurocopter EC155 ASB No. 05A015 Revision 5 dated 25 July 2011. Eurocopter EC155 ASB No. 05A022 Revision 2 dated 04 July 2012, or Revision 3 dated 25 June 2013, or Airbus Helicopters EC155 ASB No. 05A022 dated 08 April 2014. Eurocopter EC155 SB No. 65-006 Revision 1 dated 21 March 2011. 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. Based on the required actions and the compliance time, EASA have decided to issue of a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
easa_ad_2012_0170_R2_superseded.pdf (555 kb)
easa_ad_2012_0170.zip (1 mb)
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