TD please recheck G Limits of all aircraft in 4.10

[Letum]

Originally Posted by Ernst

I guess this behaviour is because TD code consider basically aircraft weight and does not account particularities of the construction of each aircraft.

This is not the case. If airframe strength was not considered, the zero would
be able to take nearly 3x the G of the F6, based on it's weight.

The strength of the airframe has certainly been considered. Directly or indirectly.

[Ernst]

Originally Posted by Letum

This is not the case. If airframe strength was not considered, the zero would
be able to take nearly 3x the G of the F6, based on it's weight.

The strength of the airframe has certainly been considered. Directly or indirectly.

Well, do not known. Only TD can answer. But i almost remenber they wrote that g limits were not especific for each design.