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FAA AD on Agusta model A109E helicopters

Washington, USA - To prevent failure of specified parts of the main transmission assembly and supports, the tail rotor assemblies, the main rotor control bolt, or the fuselage left-hand elevator, 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-06-AD; Amendment 39-12918; AD 2002-21-12] RIN 2120-AA64 Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2002-21-12 Agusta S.p.A.: Amendment 39-12918....

AVIONEWS - World Aeronautical Press Agency - 35086

AVIONEWS - World Aeronautical Press Agency