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You are here: home->com_plt->H719->5.5.6.8.0.A.1

5680
A helicopter is loaded in such a manner that the CG is located aft of the aft allowable CG limit. Which is true about this situation?
A) In case of an autorotation, sufficient aft cyclic control may not be available to flare properly.
B) If the helicopter should pitchup due to gusty winds during high-speed flight, there may not be sufficient forward cyclic control available to lower the nose.
C) This condition would become more hazardous as fuel is consumed, if the main fuel tank is located aft of the rotor mast.

 

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