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leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2019-24-01
leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2020-01-15
2017-0189 : Time Limits / Maintenance Checks – Main Gearbox Suspension Bar Pins / Fittings – Re-calculation of Life Limits / Replacement
EASA approval number
EASA Rotorcraft Section
/ Type Designation
SA 330 / AS 332 / EC 225
AS 332 L2
EC 225 LP
This AD supersedes EASA AD 2017-0133 dated 27 July 2017.
Publication(s) and related information
AH AS332 Emergency ASB 01.00.86 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017. AH EC225 Emergency ASB 04A013 original issue dated 27 July 2017, or Revision 1 dated 25 August 2017. AH AS332 L2 ALS Revision 004 dated 18 July 2016. AH EC 225 LP ALS Revision 008 dated 13 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. Based on the required actions and the compliance time, EASA have decided to issue 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 EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
EASA_AD_2017_0189.pdf (355 kb)
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