Quickie Q2 Lite, Руководство по монтажу

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..... Next, when you are sure of your framework, break loose the main
wing core female jigging templates with a hammer, (they won't be
needed again), and turn the main wing over so that the unglassed
cores are upward. Set the main wing on the jigging table once again.
..... Check the main wing tip level lines. Jig, and shim, and bondo
until the main wing tip level lines are perfect; almost doesn't
count. Then bondo the heck out of the jigging as if you were
expecting a few kids to use your shop for playing cowboys and
Indians.
..... At the leading edge, feather the bottom skin to a feather edge
at the tangent point just like you did with the ailerons. Prepare the
main wing core top surface just like you did the main wing core
bottom surface. (See "Preparing The Main Wing Cores For Glassing")
you are now ready to laminate the top main wing skins and top spar
caps. Do it similarly to the bottom lamination. The skin is the same
two UNI at 45 degrees to the T.E., draping over the T.E. down to the
bottom of the shear web and the spar caps are G thru M this time. At
the leading edge of the main wing, overlap the bottom skin with the
top skin a minimum of 1". Rather than let the spar caps drape over
the T.E. and down the shear web, trim the caps at the T .E.
..... Peel ply the shear web and all joints. Don't touch the wing for
48 hours after you have finished it. Instead, go sit in the fuselage
some more to pass the time, or else skip ahead and keep working.
Before removing the lumber, bondo a level board at about midspan on
each wing half. This is to help in attaching the main wing to the
fuselage later. Attach the level boards carefully, so that they will
agree.
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