Thanks. I understand that the stabilizer is powerful. I'm wondering whether it's true that, when your plane is in that danger state of "flinging itself past critical AoA", 2.5 degrees over 15 seconds is sufficient to avoid or recover the wing stall in time to avoid terrain.
(I think the proposed software changes also reduce this control authority but I'm not sure how.)
(I think the proposed software changes also reduce this control authority but I'm not sure how.)