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be pre-cut. You may also be able to spot the black dots
where carbon can be referenced for placing. Be sure to
provide a good connection for the carbon by poking through
the foam.
Test fit the horizontal stab/elevator into the rear of the
fuselage. If all is well, glue into place making sure that it is
flush with the fuselage and flat with the rest of the airplane.
Locate the carbon fiber elevator spar. It will be square just
as the wing spar is and cut to fit the cutout in the elevator.
Length will be 400mm.
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