checkessential
Well-known member
- Joined
- Mar 6, 2002
- Posts
- 65
On the ground the FBW computers will allow a linear deflection of the ailerons and elevators according to the pilot input. Assuming the pilots used a crosswind correction technique to keep the wings level, this would explain the deflection on the takeoff roll. Once the aircraft became airborne, the FBW system goes into C* or the airbus equivalent of normal law. This is why the ailerons "snapped" back to a more correct deflection for the commanded roll rate, which was significantly less than the linear sidestick deflection vs. aileron position. In addition, the sidestick input was probably decreased by the pilot as the airspeed increased, and near zero at rotation. As is the technique on any other plain-jane aircraft.