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The FAA proposes to adopt a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) Model ARRIUS 2F and ARRIUS 2R engines. This proposed AD was prompted by a manufacturer investigation that revealed certain high-pressure (HP) turbine blades may contain non-compliant porosity rates due to a change in the manufacturing process. This proposed AD would require replacement of affected HP turbine blades, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.
Published
Mar 13, 2025
Comments Close
Apr 28, 2025
Citation
90 FR 11914
Agencies
2
Full text not available in our database.
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Docket No. FAA-2025-0341
Project Identifier MCAI-2024-00679-E
2120-AA64
14 CFR 39