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FAA AD on Sikorsky Aircraft Corporation model S-92A helicopters (2007-17-05)

Washington, Usa - To prevent failure of a shaft and bearing assembly, loss of tail rotor pitch and yaw control, and subsequent loss of control of a helicopter

Airworthiness Directive Federal Register Information [Federal Register: (Volume 72, Number 161)] [Page 46553-46555] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-28971; Directorate Identifier 2007-SW-32-AD; Amendment 39-15163; AD 2007-17-05] RIN 2120-AA64 Airworthiness Directives; Sikorsky Aircraft...

fra/pec - 1078541
Rome, Italy, 08/30/2007 13:58
AVIONEWS - World Aeronautical Press Agency

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