Erik Kline wrote: > the two should be 21.625", not 21.56" right. Upon further inspection > there > should be a 1/32" gap between the main spar and the vertical member behind > it. Adding that to the total gives me 21.65625". I know its splitting > hairs, but it will change how much material comes off the aft spar. Has > anyone else noticed this, or did I just measure wrong?
These were drawn up years ago, but if I remember correctly, the top view of the fuselage would show a curve in the side wall, which burns up that .063". I believe the number shown on the templates is from an actual measurement of my plane, which is of course, dead on the money.....or at least "close enough for KR work"... Mark Langford, Huntsville, AL website: www.n5...@hiwaay.net email: N56ML at hiwaay.net
