Safety Publications Tool
2020-0086 : Tail Rotor – Hub Assembly – Inspection / Replacement
EASA approval number
EASA VTOL Department
/ Type Designation
SA 330 / AS 332 / EC 225
AS 332 C
AS 332 C1
AS 332 L
AS 332 L1
SA 330 J
This AD supersedes EASA AD 2019-0195 dated 13 August 2019.
Publication(s) and related information
AH ASB AS332-05.01.11 original issue dated 08 April 2020. AH ASB SA330-05.107 original issue dated 08 April 2020. The use of later approved revisions of the 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. 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 Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.
EASA_AD_2020_0086.pdf (514 kb)
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