Q2 Plans Chapter 9 Page 9-09
- Details
- Category: Q-2/Q-200 Plans
- Published: Monday, 22 May 2006 09:05
- Written by Quickie Aircraft Corporation
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Note the attachment of each CSI0 wedged between
the main wing trailing edge core and the aileron slot foam core.
The main wing tips are carved and glassed later
on, as an option.
INSTALLING THE MAIN WING TRAILING EDGE CORES
..... These cores begin at the outboard end of each CSI0, and run outboard to the main wing tip. When originally hot wired, they were made longer than necessary on the inboard end, so fit each one into position and trim. away the excess. .....The bonding and laminating process is very similar to what you have accomplished previously on the aileron slot foam cores. Attach the cores to the main wing with micro slurry on the cores and epoxy on the main wing shear web (remembering to remove the peel ply), making sure that the top and bottom surfaces make a smooth transition to the main wing curvature. Next, laminate 2 BID on the lower surface of the main wing trailing edge cores, overlapping onto the main wing cores a minimum of 1". When cured, laminate 2 BID on the top surfaces, using a glass-to-glass trailing edge treatment exactly like you did on the aileron. If you are careful, you may be able to accomplish the laminations with the wing jigged vertically, to save time; however, beware of epoxy runoff yielding dry lamination. An alternative method would be to do each surface on the flat, instead. |
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