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Skip to step 27 – Top Flite Sierra 40 Trainer Kit User Manual

Page 19

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21. The 17/32" x 1-1/2" x 30" tapered

balsa aileron stock fits against the trailing
edge stock with its lower surface flat on the
table. Glue the aileron stock to the trailing
edge of the wing. (See the photo on the

previous page.)

22. Trim the tip end of the aileron stock

flush with the end of the wing.

to the wing trailing edge at the tip as shown on the

RIGHT WING PANEL drawing. (This is done to the
right and left wing.)

26. Trim and sand the aileron stock flush with

the tip of the wing.

it to final shape. HINT: Put masking tape over the

surrounding structure when sanding items such as
the wing tips to protect areas you don't want sanded.

REPEAT STEPS 5-29 OVER THE

RIGHT WING PANEL PLANS TO

BUILD THE RIGHT WING.

23. Trim and sand the root end of the

aileron to match the 4-degree angle of the TE
and spars.

SKIP TO STEP 27

24. Carefully cut a 1-5/8" long piece off the

MAKE THE WING TIPS

27. Look at the FRONT VIEW of the wing on

the plans to see the proper orientation of the 15/32"

x 1-5/8" x 11-1/4" tapered balsawingtips. Thesmall
end of the taper is positioned at the bottom edge of
the wing.

28. Hold the wing tip up to the end of the wing.

Trace the top of the airfoil onto the wing tip. Saw or
carve the wing tip to the rough shape of the wing,

leaving it slightly oversized.

JOIN THE WING

braces. Put reference marks at the center of the
braces. NOTICE: The dihedral brace with the "lock
bumps" for the aileron servo tray is positioned on the

aft side of the spars (these bumps may be trimmed
off if you are not using ailerons).

17/32" x 1-1/2" x 30" tapered balsa aileron stock .

25. Glue the 1 -5/8" long piece of aileron stock

29. Glue the wing tip to the wing. Block sand

31. Test fit the two wing panels together with the

dihedral braces in place. Check to see that the
spars, leading edges, and trailing edges match up
well. Make adjustments if necessary.

The dihedral angle (the angle at which the wings

are "bent up") is not considered critical. This
angle is established by aligning the spars with