Originally Posted by
NutLoose
Could you not have simply adjusted the angle of dangle of the wings? It sounds like the cams are both out.
Is adjusting the cams (sympathetically) on both wings going to change the stall-warning margin? Surely the relationship between stall warning vane/slot and the wing chord will be unchanged. Strikes me that all you will be doing is changing the alpha of the fuselage.
Happy to be shot down in flames on this, by the way.