whopper chopper

Yes, the mast bump also occurs on dcs However, the effects of low-g conditions are not implemented For example, right rolling and rotor unloading

Semi-rigid rotor system helicopters (such as UH-1H) can cause low-g mast bumping due to the abrupt cyclic push over, but it can't be reproduced in DCS no matter how hard you try. I think this is a big part of the flight model implementation, so where should I contact to suggest this?