Safety Publications Tool
2021-0184R2 : Tail Rotor – Tail Gearbox Angular Clearance – Inspection
EASA approval number
EASA VTOL Department
/ Type Designation
SA 330 / AS 332 / EC 225
AS 332 L2
EC 225 LP
This AD revises EASA AD 2021-0184R1 dated 08 October 2021.
Publication(s) and related information
AH ASB AS332-64.00.46 original issue dated 30 June 2021. AH ASB EC225-64A011 original issue dated 30 June 2021. 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. The original issue of this AD was posted on 02 July 2021 as PAD 21-094 for consultation until 30 July 2021. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety 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. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
EASA_AD_2021_0184_R2.pdf (201 kb)
EASA_PAD_21_094.zip (2 mb)
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