First, while I have some engineering background with helos, I don't consider myself to be an expert in any shape or form ....
However, you might like to have a look at a relevant thread on PPRuNe (
www.pprune.org/rotorheads/477083-vne-lig...itude-reduction.html) which speaks to the topic. I would be very attentive to the posts by Shawn Coyle and Nick Lappos (these guys are real helo experts). Some of the others may, likewise, be experts but I don't know their individual stories so I am not able to comment.
The options in your cited question look to be a bit simplistic so perhaps it is a case of knowing what the particular examiner is looking for in the answer ?
Following the time-honoured "check each option before selecting your answer" ...
(a) option A - sounds OK to me
(b) option B - blade aerodynamics are pretty critical for helos. Weight and RRPM relate to lift which affects blade airflow. Don't like this one ..
(c) option C - show me a helo which doesn't have Vne varying as you climb ... don't like this one, either
(d) option D - I don't think do .. bin this one without any further thought
I think I might go with you .. option A sounds the best of the bunch.