Just found the answer on the internet so its gotta be true
....see paste below.
The most common RV-7/7A and RV-9/9A fuselage construction question?
Reference drawing #28: In all of the following text the part references are for an
RV-7/7A. The parts F-772, F-776, and F-704 should be F-972, F-976, and F-904
if you are building an RV-9/9A.
Regions of interest on drawing: Skins F-772, F-776, F-704 spar carry through
(A-9 and A-10), and NOTE #1 (G-6 and G-7).
The drawing indicates three different rivet situations for the two forward rows of
rivets where the spar flange of F-704 and the skin F-776 are "over lapped" by the
skin F-772.
The first situation involves the tricycle gear ?A? model kits only. The construction
plans state that the ?outboard? 5 rivets on both the left and right side of the plane
(most forward row in F-776) need to be installed ?double flush?. Having the
rivet?s shop heads on the inside of the plane flush with the interior surface of the
F-704 allows the tricycle gear leg socket to fully nest into position. To achieve
this, the builder will have to machine countersink the F-704 on the inside (top
surface of the flange of the F-704 if the plane is upright) so that the rivet, when
driven, will end up flush with that surface. On the exterior, the F-772 will be
dimpled and the F-776 and F-704 flange will be machine countersunk to accept
the F-772 dimple. Obviously the F-776 is too thin for a machine countersink and
the result will be an ?over countersinking? of that skin and a slight countersinking
of the F-704 flange underneath. This is standard practice.
The second situation involves the intersection points of the four forward floor
stiffeners with the F-704/F-772/F-776 flange and skins. It is denoted on the plans
with arrows and the comment ?SEE NOTE #1?. In this case, the key point is that
the builder should not for any reason dimple the flange of the F-704, as it would
complicate the fit of the floor stiffeners. In this case the same exterior process
should be used as in the first situation above. Dimple the F-772, machine
countersink the combination of F-776 and the flange of F-704.
The third situation involves all of the remaining rivets (the non-special case
rivets). 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.