Nolan. Posted December 25, 2006 Report Share Posted December 25, 2006 So apparently this is a loss of tail rotor effectiveness I dont even want to know the pucker factor on this Someone really want to go in depth to explain this annd i just realized the title makes no sense but im not a comp wizard so I wont (read: cant) change it http://www.helinews.com/video/CraneLTE2004.mov Quote Link to comment Share on other sites More sharing options...
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