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Thread: 20 degree cant on CH-53 and HH-60
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Old 27th Jul 2001, 18:03
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sling load
 
Join Date: May 2001
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Post 20 degree cant on CH-53 and HH-60
Nick,
In another post you mentioned the 20 degree cant on the CH-53 and the HH-60 assisting with increased lift and cog. In these aircraft, is tail rotor roll compensated in the main rotor shaft, or does the cant assist with this effect? It appears the tail rotor is mounted at approximately the same height as the rotor head. Would this be the reason why they are mounted that way?

Thanks
S L
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