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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

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
Rome, Italy, 05/30/2003 11:48
AVIONEWS - World Aeronautical Press Agency

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