what I mean is with the wings attached permanently to the fuselage (hence the term fused) the wing load will be transfered from the wings to the fuselage instead of just the spars. I increased the weight by 18lbs and the airframe is designed for less if set up the original way it is designed.

since I plan to put high G loads on it with a heaviar airframe, it is the only way to do it.


btw if you read all of that then maybe you would have understood and I wouldn't have to 'water it down'. :stupid:



Cheers


Cyril