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FAA AD on Turbomeca SA Arrius 2F turboshaft engines
Washington, Usa - To prevent reduced maximum available power during takeoff, landing, or an emergency, which could significantly affect helicopter performance, and result in loss of the helicopter
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Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-39-AD; Amendment 39-13169; AD 2003-11-10] RIN 2120-AA64 Airworthiness Directives; Turbomeca S.A. Arrius -2F Turboshaft Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-11-10 Turbomeca S.A.: Amendment...
AVIONEWS - World Aeronautical Press Agency - 46104
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency