“As the aircraft passed through about 390 ft at 155 knots, engine 2 EPR suddenly dropped to 1.43, while engine 1 remained at its previously set takeoff power. Immediately after engine 2 EPR dropped, the rudder pedal moved to about 5.5 degrees of left rudder, consistent with a command to counteract the adverse yaw of losing thrust on the right engine. The climb paused at 1,000 feet for 25 seconds, then continued to 2,000 ft.
Would the rudder deflection have been commanded by pilot foot or yaw damper at this point in the flight?