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5681
A helicopter is loaded in such a manner that the CG is located forward of the allowable CG limit. Which is true about this situation?
| | A) In case of engine failure and the resulting autorotation, sufficient cyclic control may not be available to flare properly to land. |
| | B) Should the aircraft pitchup during cruise flight due to gusty winds, there may not be enough forward cyclic control available to lower the nose. |
| | C) This condition would become less hazardous as fuel is consumed if the fuel tank is located aft of the rotor mast. |
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