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Flight controls will be with a side stick (RH side) and rudder pedals.  Flap lever will be on the left side 10* for take off, 25* and 40* for landing.  Stabilator control will be with carbon fiber push-pull tube.  Rudder will have two cables.  Spoilerons will have a single carbon fiber pull tube in each wing, and flaps will use a single carbon fiber torque tube in each wing.  Stabilator will have an anti servo tab for pitch stability and trim.

IMG_0459.JPG                  

Cam plate to control spoilerons to eliminate nul point slop

Flap Mechanism