I recently got some time in 2 different Piper Saratogas. My question involves the control breakout forces for pitch.
On both of those airplanes, it took approx 3-5 lbs of breakout force on the yoke to get the control moving both fore and aft. Not only that, once the control was moving, it would seem to bind during large control movements (on the ground!!), so the result was that it wouldn't move very smoothly. I actually had to use 2 hands on the yoke during landing, not because the airplane was mistrimmed, but to attempt to make small changes in pitch smoothly.
Is this common for Piper products?? If this happened on one airplane I would lean toward a control adjustment issue, but it happened on 2 independent aircraft.
Any comments/ideas??
On both of those airplanes, it took approx 3-5 lbs of breakout force on the yoke to get the control moving both fore and aft. Not only that, once the control was moving, it would seem to bind during large control movements (on the ground!!), so the result was that it wouldn't move very smoothly. I actually had to use 2 hands on the yoke during landing, not because the airplane was mistrimmed, but to attempt to make small changes in pitch smoothly.
Is this common for Piper products?? If this happened on one airplane I would lean toward a control adjustment issue, but it happened on 2 independent aircraft.
Any comments/ideas??