I know what Neutral point is... its the Point at which all Aerodynamic forces are equal And If you want me too, I can get out my Airframe Book from school and give you the Equation for it if you really want me too... I will be the bigger man here and admit I did misread your post and I Apoligize for that. With saying this My Statment is still correct... I was trying to help the guy with his problem, he stated that his CG is centered, If he says it is centered then why are talking about it ??? a Tail-Heavy CG would still not cause a plane to Favor one wing, if it does it would cause the left wing to dip not the right!, That is the whole point I am trying to get across, I do not wish to argue anymore, so I think I will take my ball and go home!