Originally Posted by
mi68guel
A320 strong crosswind from the right-hand side. Decrab applying left rudder...if the side stick is in the neutral position, the airplane automatically applies some upwind bank angle (rolls to the right) to zero the roll rate induced by the yaw correction. Am I right?
Not by applying bank angle but by applying some ailron and may be spoilers it will prevent the roll from the yaw. Also the axis is ahead of C of G so the aircraft swings towards the wind.