British FM killing the fun of the game for allied pilots.

[Kurfürst]

Originally Posted by 41Sqn_Banks

But this is nothing special about the Spitfire. Each aircraft has it's structural limits, exceeding these limits damages/destroys the aircraft. As you say the critical situations might be different for each aircraft.
The problem is not the Spitfire, the problem is that structural limits are not simulated.

Question.

One aircraft has a stick force gradient of 4 lbs/g, the other has a stick force gradient of 20lbs/g.

Question 1.
In which aircraft is it easier for the pilot to reach the actual break point of ca. 10-12 g?

Question 2.
Is it possible for the aircraft which has a stick force gradient of 4 lbs/g to actually reach that 10-12 g load at which the airframe is likely to break?