Vladinsky

Yes that makes a lot more sense. What happens right now, in flight, with FFB is that the trim tab moves and the pitching moment changes but the neutral position of the stick and control surface remain unaffected.

If this is true you have rigged the 3D model incorrectly, the trim tabs are connected to the left aileron, rudder and elevator and are not mechanically separated. Are you thinking of the servo tabs?

Easy to test, how long can you run full throttle before the 3 minutes remaining light turns on if you don't press the water injection on keybind?

Total travel, you can find this information in the 1979 NASA CR 3144, it has the same data for a couple other helicopters too.

Yes, that's right.

The UH-1H has a spring centering force of 1.21 lbs/inch in pitch and 0.79 lbs/inch in roll with a total cyclic travel of 13 inches in pitch and roll. The pedals have a spring centering force of 7.3 lbs/inch with a total travel of 6.5 inches. With force trim turned off or the force trim button depressed the springs are disengaged and the only resistance felt is the inertia and friction of the pushrods and hydraulic servos, which is negligible.

Only in MECH, which is likely not modeled.

For the Mirage 2000, pulling to the elastic stop with a force of 10kg commands 9G. To overcome the elastic stop requires roughly 25kg and pulling all the way back to the hard stop with a force of 40kg will command 11G.