Safety Publications Tool
The 5th EASA Airworthiness Directives (AD) Workshop will be held on 28 November 2017 in Cologne. The event is addressed to all interested stakeholders such as operators, CAMO, maintenance organisations, design approval holders, who want to have a better understanding of EASA processes related to safety publications. More information and online registration are available
2017-0121 : Time Limits / Maintenance Checks – Airworthiness Limitation Section – Amendment / Implementation
EASA approval number
EASA Propulsion Section
/ Type Designation
SAFRAN HELICOPTER ENGINES
This AD supersedes EASA AD 2015-0177 dated 25 August 2015.
Publication(s) and related information
TURBOMECA ARRIEL 2C MM, Section 05-10, EASA approval date 23 September 2016. TURBOMECA ARRIEL 2C1 MM, Section 05-10, EASA approval date 23 September 2016. TURBOMECA ARRIEL 2C2 MM, Section 05-10, EASA approval date 23 September 2016. TURBOMECA ARRIEL 2S1 MM, Section 05-10, EASA approval date 23 September 2016. TURBOMECA ARRIEL 2S2 MM, Section 05-10, EASA approval date 23 September 2016. The use of later approved revisions of these 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. This AD was posted on 29 May 2017 as PAD 17-065 for consultation until 26 June 2017. 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.
EASA_AD_2017_0121.pdf (498 kb)
EASA_PAD_17_065.zip (797 kb)
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the EASA AD team
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