Can anyone comment to their experience in this area when comparing these options..
VANS Fuse FAQ:
You have two options. One is to dimple all three surfaces. The builder
will find the F-704 a bit thick to take a good dimple so if the dimple is found
insufficient, lightly machine countersinking the initial dimple will improve the fit
(nesting) of the dimples of the F-776/F-772 skins. The second method is simply
to continue the process used for the four floor stiffener locations. Thus machine
countersink the combination of the F-776 skin and F-704 spar flange sufficiently
to accept the dimple of the F-772. This will work fine.
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AP/IA/CFI/ATP/EAA TC
RV-7 Tip N77XA
Not knowing any better, I just followed the instructions here. I machine countersunk the F-776/F-704 combinaton only at the holes for the stiffeners, and dimpled the rest. The flange of the F-704 is only 0.040 thick, and I didn't have any problem with dimpling it; same as the rear spar in the wing.