i want to ask this time as to "what are the areas of an aircraft that feels or suffers the most from G forces?". i am asking this in terms of structural design and physical limits of the pilot(the position and seat angle) and the plane. please try not to limit the airplane model to simple light-aircraft,try to expand it near to military Aviation and other else.
if possible, please try not to use high-falutin words since i'm having a hard time with words in English.
If you can not understand this clearly, i am sorry for my poor English and Grammar, and also i want to elaborate more, but i can't translate it properly at the moment.