Apparently the older directions for wing construction on the -6A referenced a ''figure 7-11'' which I guess gave the x and y measurements in order to drill a hole in the main spar web and the rear spar web to run a plumb line through in order to maintain the correct wing incidence when drilling the ribs for skin attachment. My kit did not have any such reference in the manual and I cannot find it. Those pages I believe were updated by Vans years back and the measurements are not in the current section 7. Can anyone either forward me the instruction page 7-11 that shows the x, and y coordinate measurements for drilling the plumb line holes in each spar, or is there some newer way to be sure of the correct alignment before I drill.
Thanks.
Thanks.