Hi All,
Let me add to what Ted says.
Narrowing the lines at the handle to get the desired sensitivity is better than flying too sensitive, but it is a band-aid rather than the solution to the problem.
The sensitivity should be reduced by either lengthening the flap horn or making the bellcrank longer. I like both.
Why is the narrow line spacing bad? The control effort to deflect the flaps and elevator in a corner can be as much as several hundred ounce-inches of torque for a heavy ship with large surfaces. Converting to inch-pounds, that's anywhere between 5 and 15 inch-pounds of torque. That torque is developed with a difference in line tension, between the up and down lines, across the length of the bellcrank. Aha! Now let's do the ugly math.
The math ain't ugly because it's difficult, it's ugly because it highlights a problem: let's pick the middle figure of 10 inch-pounds. With a four-inch crank, that means you need a 2-1/2 pound difference in tension between the lines. Now, 2-1/2 pounds could be maybe one quarter of the total line tension (guessing 10 lbs). That means that one line might have 3-3/4 lbs and the other 6-1/4. That's almost 2:1.
One line will sag, both due to aerodynamic drag and due to G loading in the corner, twice as much as the other! When you neutralize the handle, the tension will almost equalize and then the mass of the saggy line will have to accelerate "forward" to match the other. This unwanted "tail" to every large input means that the controls feel like they are laggy and spongy.
Ideally, we would run long bellcranks, longer flap horns, and wide spacings at the handle for best control fidelity. What's more, this problem gets worse with lighter airplanes!
later,
Dean Pappas