23
5. Slide a .046" x 11
1
/
4
" carbon rod from
the upper fuselage to the lower side force
generator. Leave at least 1/16" of the rod
exposed at both ends. Glue only the rod at the
fuselage. Apply foam-safe CA to the rod both
at the inside and outside in order to capture the
rod in position.
6. Place the bottom wing on a surface that will
allow the wing panel to lie perfectly flat. Apply
glue to the inside edge of the rod. Once the
glue fully cures carefully lift the airframe and
apply CA to the top of the rod.
7. Repeat Steps 5 and 6 to complete the
cross bracing.
