Can we safely assume that if we inadvertently over stress the airframe without any obvious signs of structural damage, we can then safely land and repair to reset that stress datum, like most other airframe damage within the sim? The last thing we need is to repair and remarm and then to find out that our airframe structure subsequently fails due to previous unseen collective damage.
What I'm asking is a) Are all over g stresses recorded within the sim to form some sort of cumulative airframe depreciation damage? b) Can we then repair and reset this value before continuing with any subsequent flights without switching aircraft. Although I do appreciate that switching AC is probably the most likely resolution in real life, should that pilot not be grounded for ruining a perfectly good bird. Although in the case of the sim, you do not have the luxury of a ground crew to analyse cockpit data or engineers to check the AF for structural damage.