AKNick
640cc Uber Pimp
CG consideration. Getting to the point where I can begin to check the CG location. The instructions are wrong, and most always err to nose heavy for safety reasons. Read about Nick's re calculation through trial and error to a reasonable CG.
There is really a good way to check and verify if your CG is safe and what kind of handling you will get with a given CG, but you have to know the neutral point of the aircraft or you are just guessing, most of us with experience get pretty good at guessing, but I always calculate the NP before I decide on a CG. If you don't know, the NP is the point aft on the main wing from the LE at which angle of attack has no effect on pitch, the plane is aerodynamically balanced. The CG is a center of mass calculation only. Static margin is the distance between the NP and the CG expressed as a %. CG is always for our purposes forward by a % of the NP. 7% to 10% is considered a middle ground for static margin on a conventional aircraft. less becomes twitchy, 15% becomes mushy.
I can usually guess a constant cord wing simple plane will balance at about 33% of cord. on the Timber I went conservative and guessed 30% which equates to 4.75 inches. I then ran the calculations for the NP and it more or less confirmed my guess, but It also can give me the static margin so I know what to expect. Long story short using a 7% static margin (on the crisp side) the CG calculated to 5.03" from the leading edge. (1 " ahead of the NP) using a more conservative static margin of 10% the CG came out to 4.63" The actual NP calculated to 6.03 " which is the point where any more Aft CG will result in an unstable aircraft. If you want to try this yourself, there are several online calculators that take the math out of the job.
5.125” is a good spot