Can anyone tell me what the angle of incidence of the flaperons on a Mk2 should be in their neutral position, with flaps NOT extended?
Also, what are the reference point(s) on the flaperons and the aircraft against which this angle should be measured?
I am trying to re-rig a 1991 aircraft and the builder's manual I have, which is in loose leaf format, is missing this information.
Thanks in advance.