Safety Publications Tool
2021-0215-E : Tail Rotor – Pitch Rod – Inspection
EASA approval number
EASA VTOL Department
/ Type Designation
Publication(s) and related information
AH EC175 Emergency ASB EC175-05A37 original issue dated 20 September 2021. The use of later approved revisions of the above-mentioned document 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 results of the safety assessment have indicated the need for immediate publication and notification, without the full consultation process. 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_0215_E.pdf (195 kb)
For help on using this tool, please refer to
the help section
For any inquiry regarding ADs, please contact
the EASA AD team
To report any bug, broken link or problem with this application, please contact the
Disclaimer & copyright notice
- 2021 ©