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Old 27th Jan 2006, 12:45
  #350 (permalink)  
semirigid rotor
 
Join Date: May 1999
Location: UK
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Just come back from harrassing innocent members of the public and the findings are as follows:

OAT +2, 135ft AMSL, wind 040/09, 2795Kg gross weight

4ft hover, without Cat A 58% Tq, with Cat A - 58% Tq

No discernable difference, Tq initially climbs when Cat A selected, but when everything has settled down, same figures on the VEMD. I didn't take the figures for N1 & TOT as they are not a limiting parameter.

Open to suggestions
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