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FAA AD on Raytheon Aircraft Company model 390 airplanes

Washington, Usa - To prevent failure of the rudder pedal arm assemblies caused by fatigue cracks

Airworthiness Directive Federal Register Information [Federal Register: September 15, 2005 (Volume 70, Number 178)] [Page 54472-54474] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21410; Directorate Identifier 2005-CE-31-AD; Amendment 39-14272; AD 2005-19-07] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 127042
Rome, Italy, 09/16/2005 15:27
AVIONEWS - World Aeronautical Press Agency

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