Can I ask again, a recent question of mine that wasn't answered at the time
In the cruise with relatively aft c.g. (due to trim drag tank being full/relatively full)
What is the effect on this aft c.g. posn. (33% MAC?) when the system reverts to Alt2 law or even Direct law?
Obviously the pitch stability (c.g. closer to Neutral Point) is less strong, wondering if anyone has even contemplated this, let alone flown this config in the simulator?
Thanks...