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The primary flight control surfaces on a fixed-wing aircraft include:
The primary flight control surfaces on a fixed-wing aircraft include:
Ailerons, elevators, and the rudder.
▪The ailerons are attached to the trailing edge of both wings and when moved, rotate the aircraft around the longitudinal axis (Roll).
▪The elevator is attached to the trailing edge of the horizontal stabilizer.
When it is moved, it alters aircraft pitch, which is the attitude about the horizontal or lateral axis.
▪The rudder is hinged to the trailing edge of the vertical stabilizer.
When the rudder changes position, the aircraft rotates about the vertical axis (yaw).

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