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FAA AD on Rolls-Royce Corporation 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, - C20F, -C20J, -C20S, and -C20W turboprop and turboshaft engines

Washington, Usa - To minimize the risk of uncontained 1st stage turbine wheel fragments from causing damage to the aircraft or damage to the second engine on twin-engine installations, which could lead to loss of control and loss of the aircraft

Airworthiness Directive Federal Register Information [Federal Register: May 18, 2005 (Volume 70, Number 95)] [Page 28420-28423] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19648; Directorate Identifier 2004-NE-31-AD; Amendment 39-14090; AD 2005-10-13] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 120740

AVIONEWS - World Aeronautical Press Agency
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