Moving as slow as molasses on a 40 degree day (which it was) a little progress was made between a few warm up trips to the house. Guess it won’t be long before I’ll need to break out the winter clothing if serious work is to be accomplished through the winter months.
Because of the space constraints at DOG Aviation,
only one wing will be assembled at a time. The left wing will be assembled first only because
the left spar was on the top in the spar crate. The AEX tie down extrusion was
first on the day’s agenda beginning with drilling out the holes on both ends to
prepare the holes for being tapped. Decided to go ahead and tap out both holes
as suggested in the drawings … even though the likelihood of using a tie down
ring on the top of the wing is very remote. But if a tie down ring is needed on
the top of the wing for transport, the threads will be there.
Tapping threads in the hole of the AEX tie down
The plans call for separating some doubler plates
which become a left and a right … this was done earlier prior to priming. The
left doubler plate has an extra row of holes on it and needs to be clecoed onto
the left spar’s inner most rib attach clip which has already been installed at
the factory. Once the doubler is clecoed in place, the rib clip on the spar is
match drilled to the extra row of holes on the left doubler plate. An extra long drill bit is used so it can be
slightly flexed to get straight onto the hole. Using a short drill bit would
place the bit on an angle because the drill body will be touching the spar
keeping the drill at an angle.
Match drilling the left spar’s inner most rib
clip to the doubler plate with an extra long drill bit.
There are ten rib attach clips that get clecoed
onto the fore and aft of the left spar and will be riveted during the next work
Clecoing the rib attach clips onto the left spar for
Where the spar narrows at the outboard end, an
angle is riveted onto it … this creates a surface to rivet the skin onto at the
outer end of the spar. Because I’m planning on using flush rivets on the outer
skins, the rivet holes on the angle where the outer skin will attach required dimpling before
riveting it in place. AN470AD4-4.5 solid rivets were used here in the place of the LP4-3 pop
rivets called for in the plans.
First riveting on the wing spars … using the
pneumatic squeezer to set solid rivets attaching an angle onto the left spar.