Thanks! so this is interesting:
Root Chord A) 430
Tip Chord B) 210
Sweep S) 130
1/2 Wing Span Y) 910

Stab Root Chord AA) 245
Stab Tip Chord BB) 165
Stab Sweep SS) 60
1/2 Stab Span YY) 410
Wing LE to Stab LE D) 1160
STATIC MARGIN: 25% (don't fully understand, higher number moves CG forward, and 5% to 15% is recommended)

CG from Wing Root LE: 167.4

Entering 15% moves CG to 140, and pretty much everyone flying this plane is 160 or more.I started at 170 (which a little birdie told me to do ) which is just about 25%. The tool says this should be incredibly stable, and I should be more like 200-230.

Well this would make sense why I'm at +.5 wing and still need up elevator, but it's contrary to what some talented pilots and builders have been using. I'll try slowly shifting back and see what happens.

Thanks again Jim!