I am with an aircraft squadron and we have a conditional inspection for aircraft that pull an excessive amount of "G's". The inspection is to check significant parts of the aircraft that might crack or buckle under certain amounts of stress. There is an arguemt in the shop about going from a negative "G" (Forces pulling in one direction) to a positive "G" (Forces pulling in another direction). If the aircraft is flying and is pulling -2 G's then changes direction and pulls +3 G's... How many "G's" were pulled. Some say 5 G's and others say 3 G's. Can someone help us out and maybe provide a reference for this issue? Thanks!