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FAA Emergency AD on Agusta model A-109E helicopters
Washington, USA - To prevent fatigue failure of the tail rotor blade and subsequent loss of control of the helicopter
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-SW-55-AD; AD 2002-25-51 Agusta S.p.A. (Agusta) Model A109E helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2002-25-51 AGUSTA S.p.A (Agusta): Docket No. 2002-SW-55-AD. Supersedes AD 2002-17-51, Amendment...
AVIONEWS - World Aeronautical Press Agency