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What I learned:
Never
use the foam that sands easily and leaves particles that feel like
sugar on your clothing. It doesn't leave a strong enough
structure beneath the fiberglass. I've always hated using
it. In this case I used it to fill the gap behind the spar and
between the spar and the stainless steel firewall. I will never
use it again. I only use it on this part because it is not
structural. It only fills the gap. I used it on the nose
but the fiberglass over it is thicker and stronger. Also it is
stronger on the inside of the nose. The two part urethane foam
would be better, peanut butter could even be better. (psych)
Methods to my Madness:
I didn't have the landing gear. I'm doing retracts so I leveled
and mounted the fuselage to sawhorses and bondoed in place. I
also bondoed the saw horses to the floor. We then put the wings
and spar on tall saw horses and used a pulley system to help seat the
spar into the fuselage. Once it was there I removed the pulley
system and began leveling the wings and spar. We used large foam
wedges to work the wings level, when we were finally satisfied we bondoed foam
in place.
I used the wing level point that is placed on the wing as the wings are
test leveled and mounted to the spar. I also built my own large
water level which consists of 3/8" tubing tee-ed together, (larger
tubing clears of bubbles in the system better than smaller tubing),
taped to the floor, and
mounted on stands. It has been made to test level at six
different points. Two places
equal distant from the wing tips, and two points on each wing
root. This level is the most perfect way to level. It's
like having a large body of water under the plane and being able to get
exact measurements from a perfectly level surface.
Leveling the wings, front to back, and also full width (tip to tip) as
well as measuring from the wing tip to the nose is a process that
requires patience, a few hours of checking and rechecking is what
it takes becuase changing one point affects the others. There was
three of us and we would work all levels and measurements until we all
agreed that every measurement was as good as it possibly could
be. The spar is centered, the wings are level with an equal
dihedral on both sides, also the distance from nosetip to inside
wingtip are the same. I bondoed it all together then let it sit
for a day then rechecked all measurements. After being satisfied
I then floxed the spar into the fuselage. I then applied all
glass layups slightly better than plans to compensate for larger wing
span.
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