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๐Ÿ›ซFlight Controls are divided into two main categories

๐Ÿ›ซPrimary Flight Control Systems
-AILERONS AND FLAPERONS
-SPOILERS AND SPEEDBRAKES
-ELEVATORS
-HORIZONTAL STABILIZER
-RUDDER.

๐Ÿ›ซHigh Lift Control systems
-TRAILING EDGE FLAPS
-LEADING EDGE SLATS
-KRUEGER FLAPS

๐Ÿ›ซPurpose of the primary flight control system (PFCS)- It controls the airplane flight attitude in relation to the three basic axes:
- Longitudinal (roll axis)
- Lateral (pitch axis)
- Vertical (yaw axis)

๐Ÿ›ซRoll Control- the roll control uses the ailerons, flaperons, and spoilers to control the airplane attitude about the longitudinal axis. During a bank of the airplane, the aileron and flaperon on one wing move in an opposite direction from the aileron and flaperon on the other wing.


๐Ÿ›ซPitch Control- The pitch control uses the horizontal stabilizer and the elevator to control the airplane attitude about the lateral axis.

๐Ÿ›ซYaw Control- The yaw control uses the rudder to control the airplane attitude about the vertical axis. The rudder has a tab which moves to increase the effectiveness of the rudder.

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