>Some interesting comments here. I do not have any known
>exerience with flying with props that do not have the same
>pitch on both blades. I cannot think of any reason why
>there might be some advantage in doing so. I believe that
>there would be an unequal load on the crankshaft and the
>bearings. I would not think that could be good for the
>engine.
>
>My following comments are a bit off topic, but I think
>appropriate to mention here.
>
>In other forums and other threads, I have read where
>individuals have have found it necessary to reshape both
>blades so that both would have the same pitch. I think that
>most machines and production processes will result in both
>blades being very close to the same shape and pitch. What
>can happen is that the back face of the propeller hub might
>not be true. The hub back face would not have to be slanted
>very much to make a 0.5 to a full one inch difference in the
>measured pitch from one blade to the other. Instead of
>reshaping the blades, all that would be necessary is to
>"true-up" the hub back face (and front face) so that the
>measured pitch is the same from one blade to the other. It
>might also be necessary to re-drill the hole to be
>perpendicular to the now trued-up rear and front faces of
>the prop.
This is always the first thing to check. A tilted hub adds a constant angle to one blade and subtracts a constant angle from the other blade. The net result is that the measured pitch diverges towards the tips. 1/2 a degree of hub tilt means a bigger and bigger "error" in pitch as you get further from the hub.
If it *doesn't" diverge, and the blades are reasonably the same measured amount off on either side (like 5" all the way on one side, and 5.2 on the other) then it's not the hub.