Open Question to the group: Has anyone had experience (good or bad) with using carbon fiber push rods for their aileron & flap servo linkage. This past season, due to slow thumb response at that critical moment of retracting flaps just before touch down, I was bending the flap push rods (bottom hinged, linkage on top of flap, servo arm on bottom of wing. Carbon fiber rods would give stiffness/rigidity but would they be prone to breakage? This set up was/and is on a F3J 144" Shadow. All comments and suggestions would be greatly appreciated.

Regards,

Robert

Robert P Buxton
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