FCTM-OP-020 -OPERATIONAL PHILOSOPHY-FLIGHT CONTROLS
NORMAL LAW
CHARACTERISTICS IN PITCH
IN FLIGHT
When the PF performs sidestick inputs, a constant G-load maneuver is ordered, and the aircraft responds with a G-Load/Pitch rate. Therefore, the PF’s order is consistent with the response that is "naturally" expected from the aircraft: Pitch rate at low speed; Flight Path Rate or G, at high speed.