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2018-0172 : Main Rotor Blade Attachment Pin – Inspection
EASA approval number
EASA Heavy Rotorcraft Section
/ Type Designation
SA 330 / AS 332 / EC 225
AS 332 L2
EC 225 LP
This AD supersedes EASA AD 2015-0016 dated 30 January 2015.
Publication(s) and related information
Airbus Helicopters ASB EC225-05A040 original issue dated 22 December 2014, or Revision 1 dated 26 April 2018, or Revision 2 dated 26 June 2018. Airbus Helicopters ASB AS332-05.00.99 dated 22 December 2014, or Revision 1 dated 26 April 2018, or Revision 2 dated 26 June 2018. The use of later approved revisions of above-mentioned 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 29 June 2018 as PAD 18-089 for consultation until 27 July 2018. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 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_2018_0172.pdf (507 kb)
EASA_PAD_18_089.zip (2 mb)
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