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FAA AD on Agusta model A119 helicopters
Washington, USA - To prevent failure of the tail rotor blade and subsequent loss of control of the helicopter
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-46-AD; Amendment 39-12910; AD 2002-21-04] RIN 2120-AA64 Airworthiness Directives; Agusta S.p.A. Model A119 Helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2002-21-04 Agusta S.p.A.: Amendment 39-12910. Docket No. 2002-SW-46- AD. Supersedes Emergency AD 2002-17-52,...
AVIONEWS - World Aeronautical Press Agency