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Basic Controls | page 1 |
The pilot uses the elevators on the tail to pitch the airplane. This means that if the pilot pulls back on the stick or yoke the elevators move up. The lift on the tail surfaces decreases, causing the nose to pitch up (the opposite happens if the stick or yoke is pushed forward). At the nose pitches up (and the wings too) the airflow will increase the overall lift on the plane. The plane will begin to climb. The pitching motion is longitudinal (over the length of the airplane), and so the elevators are known as longitudinal controls. To start a yawing (turning) motion, the pilot will use the rudder. Almost all rudders are controled by pedals operated by the feet of the pilot. If the pilot steps on the right rudder pedal, the rudder moves to the pilot's right. The pressures on the right side of the rudder are now higher. The plane begins to rotate in a clockwise direction, or to the right! The rudder is called a directional control, since yawing is considered a directional motion.
Rolling and yawing of the airplane are related; it is very hard to do
one without the other. For example, during a right turn, when the lift
is increased on the left wing, drag is also increased on that same
wing. This causes the airplane to be pushed slightly to the left. To
overcome this, the pilot will push the right rudder pedal. So, in most
cases he or she will use both the ailerons and the rudder to turn the
aircraft.
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