As long as the angle of attack (of the airfoil) does not go beyond it limits you have lift produced by the wing. If the angle of attack for a given airfoil exceeds the angle of attack then the wing stalls because the air no longer flows smoothly over the top of the wing. That is just for changes in attitude about the lateral axis.
There are a surprisingly high number of people that don't understand that the turning of an airplane is caused (not by the control surfaces) but by the horizontal component of lift. The control surfaces just manipulate the attitude of the airplane about/around it axis.
So the answer is no.
To add a little extra info, the Angle of Attack=The difference in angle of the chord line of any given airfoil to the relative airflow, Angle of Incidence=The difference in angle of the chord line of an airfoil to the longitudinal center line of the fuselage.