Hey Scott,
Paul are you inserting the word "intercostal" to mean the vertical spar stiffener pieces? - Yes that is what i have called them (the one between the top and bottom spar caps)
And while I don't know for the DE, the general timing for the build would be diagonals first, compression second.
Raking and fitting required all the while maintaining your "square" and rib placements.
Agree with your comments but not sure about this. I have not seen the plans for other Legal Eagles but the DE lower Compression struts run between the faces of the spar caps. If you install the compression struts first then the diagonal rests on top of the compression strut and provides an additional bonding surface (apart from the triangle blocks and ply caps). If you glue the the diagonal on first then epoxy from the join can ooze underneath and the bond may not be that good. I am of the understanding that even when the compression struts are glued then the wing can still flex enough to get the diagonals in. Happy for anyone to shoot holes in that argument :). I maybe over analyzing this.
thanks for your input always appreciated. such a great Forum this.
cheers Paul