I have been reading about wing loading, chord of the wing, how to find the Reynolds number. I would just like to find out how to find wing loading. I have taken my Edge with a 672 square inch wing area and it weighs 8.5 pounds. 8.5 X 16 = 136. Divided by 672 gives me .20. That is not a normal wing loading figure. What am I doing wrong? Someone please help me. I will thank you in advance.