Would some of you Smithcub guys mind measuring the exit for the aileron cable that comes out the bottom of the wing. I can't read my own pre-cover notes. Would be nice to have an average before I cut the fabric. Gerald, John, Joe, etc.
Bill,
Using the center line of the forward and aft wing strut attach bolt holes as a reference I came up with the following: measuring aft of the forward face of the rear front fitting 17-5/8" to 18-3/4" and outboard of this center line 4-3/16". It is a slot 1-1/8" long. This is for the down aileron cable with the aileron in neutral. It moves forward and aft when the aileron moves.
The up cable ( the one by the strut pulley) is 4-1/2" aft of the forward face of the rear front fitting and inboard of the center of the compression tube 1-13/16". This is the center point of an angled slot 1/2" long.
My wing is a TCOW extended. I don't believe that this should make any difference.
I got several PM's and although they all were measured from different points they all came out about the same. Thus the answer is....
2-5/8" from the center of the compression tube (pretty easy to find as it pushes down through the fabric)
17-5/8 to 18-3/4" aft from the forward face of the rear half of the two part forward strut attach fitting. (basically this is the rear of the forward spar)