TD please recheck G Limits of all aircraft in 4.10

[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.