Safety Publications Tool
2018-0252-E : Tail Rotor – Tail Rotor Flight Control System – Inspection
EASA approval number
EASA Rotorcraft Section
/ Type Designation
LEONARDO S.p.A. HELICOPTERS
This AD supersedes EASA AD 2018-0250-E dated 19 November 2018.
Publication(s) and related information
Leonardo S.p.A. Emergency ASB 169-120 original issue dated 05 November 2018. Leonardo S.p.A. Emergency ASB 189-213 original issue dated 06 November 2018. Leonardo S.p.A. Emergency ASB 169-125 original issue dated 21 November 2018. Leonardo S.p.A. Emergency ASB 189-214 original issue dated 21 November 2018. Leonardo AW169 AMP DM 69-A-64-31-00-00A-31AB-A. Leonardo AW189 AMP DM 89-A-64-31-00-00A-31AA-A. UTAS SB 67-0006 original issue dated 21 November 2018. 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 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.
EASA_AD_2018_0252_E.pdf (512 kb)
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