OK, I think I understand what you are saying, and I can academically agree with your statements--and will conceed that you definitely know more about the issue at hand than I do. So, I have a question.

I can see where torque would cause an unwanted effect along the roll axis, and not the yaw axis. So, would right thrust still not help that issue? What I mean is, with the engine 180 degrees in relationship to the logitudinal axis of the fusealage, the torque reaction would be directed along the entire length of the fusealage--running from firewall out through the tail, in a straight line. Therefore, the roll reaction to the torque would be having an effect along the entire logitudinal axis.

Whereas, with right thrust built in, the axis of torque reaction would be re-directed to go not through the centerline of the aircraft, but rather to exit the aircraft somewhere along the left side of the fusealage--again, around the CofG. Would this not reduce the rolling effect of the the torque reaction?

I may be all wrong, and can accept any correction in my assumptions.

Also, since we have officially turned this thread into the perverbial "can of worms" , could you please post some mathmatical concepts explaing the P factor and what it means, and what it does to aircraft? I am now interested in this conversation. I believe we have gotten this thread back to a civilized coversation, so let's continue the lecture, shall we?