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FAA AD on Agusta SpA model A-109K2 helicopters
Usa - To detect a crack and prevent fatigue failure of the trunnion, loss of the tail rotor hub and blade assembly, and subsequent loss of control of the helicopter
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Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: August 2, 2004 (Volume 69, Number 147)] [Page 46096-46098] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-SW-14-AD; Amendment 39-13755; AD 2004-15-21] RIN 2120-AA64 Airworthiness...
fra/pec - 101128
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency