Apart from this bit
the Vne is just to control stress on the dynamic components and make sure components all reach their design lifetime.
if you exceed Vne, you have reduced the life on components - you have no idea by how much or what damage you may have done.
It is simple - don't exceed the limits but of you do, inadvertently, have the aircraft checked throughly.
Do you want to be the one flying when a pitch change rod or control horn gives up early in its life due to overstress?