1.

Castor angle is defined as the angle

A. ormed by the longitudinal axis of the aircraft and the direction of movement of the nose gear
B. etween the direction of wind and the longitudinal axis of the runway
C. etween the true speed of the aircraft and the crosswind component
D. etween the horizontal and the fuselage axis
Answer» B. etween the direction of wind and the longitudinal axis of the runway


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