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FAA AD on Agusta SpA model A-109A and A-109A II helicopters (2008-24-06)
Washington, Usa - To prevent fatigue failure of a tail rotor blade (blade), loss of a tail rotor, and subsequent loss of control of the helicopter
Airworthiness Directive Federal Register Information Federal Register: [Page 71526-71527] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0834; Directorate Identifier 2007-SW-78-AD; Amendment 39-15746; AD 2008-24-06] RIN 2120-AA64 Airworthiness Directives; Agusta S.p.A. Model A109A and A109A II Helicopters...
fra/pec - 1097205
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency