Safety Publications Tool
2021-0222 : Fuselage – Main Gearbox Suspension Bar Attachment Fittings and Screws – Inspection
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
This AD supersedes EASA AD 2019-0295 dated 05 December 2019.
Publication(s) and related information
AH ASB AS332-53.02.05 original issue dated 18 April 2019, or Revision 1 dated 02 March 2020, or Revision 2 dated 19 August 2021. AH ASB AS332-53.02.07 original issue dated 21 October 2019, or Revision 1 dated 19 August 2021. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. This Proposed AD will be closed for consultation on 20 September 2021. 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 23 August 2021 as PAD 21-128 for consultation until 20 September 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_0222.pdf (198 kb)
EASA_PAD_21_128.zip (372 kb)
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