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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

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
Rome, Italy, 08/03/2004 12:16
AVIONEWS - World Aeronautical Press Agency

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