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FAA AD on Sikorsky Aircraft Corporation model S-92A helicopters
Washington, Usa - To prevent fatigue failure of the tail gear box output housing, loss of tail rotor drive, and subsequent loss of control of the helicopter
Airworthiness Directive Federal Register Information [Federal Register: June 23, 2005 (Volume 70, Number 120)] [Page 36333-36334] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21588; Directorate Identifier 2005-SW-24-AD; Amendment 39-14150; AD 2005-13-13] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 122715
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency