by Kai » Tue Nov 22, 2022 5:33 am
I´d be surprised if anyone is in a position to quantify this.
Neither wings, fuselage, flaps, nor ailerons are built in jigs: not two airplanes are exactly identical. As long as the threaded parts of the control rods cover the ident holes in their respective spherical bearings when the their control surfaces are initially rigged as close to the drawings as you can possibly get them, you should structurally be good to go. And don´t forget the lock nuts! Check that the rods are free to rotate slightly in their bearings with full rudder deflections.
Aerodynamically only flight testing of your particular airplane will tell.
Sonex A #0525- SG, DS.
EdgePerfomance EP915ECI, 123HP