Editing Flight control surfaces (section)

{{Short description|Surface that allows a pilot to adjust and control an aircraft's flight attitude}}
[[File:ControlSurfaces.gif|thumb|alt=Moving the control stick to the left moves the aileron in the left wing up, that in the right wing down, making the plane lower the left wing. Pulling on the stick moves the elevators up, making the plane raise the nose. Pressing the right rudder pedal moves the rudder to the right, making the plane turn the nose to the right.|upright=1.14|Basic aircraft control surfaces and motion. A)aileron B)control stick C)elevator D)rudder.]]

Aircraft '''flight control surfaces''' are [[aeronautics|aerodynamic devices]] allowing a pilot to adjust and control the aircraft's flight [[aircraft attitude|attitude]].

Development of an effective set of flight control surfaces was a critical advance in the development of aircraft. Early efforts at [[fixed-wing aircraft]] design succeeded in generating sufficient lift to get the aircraft off the ground, but once aloft, the aircraft proved uncontrollable, often with disastrous results. The development of effective flight controls is what allowed stable flight.

This article describes the control surfaces used on a [[fixed-wing aircraft]] of conventional design.  Other fixed-wing aircraft configurations may use different control surfaces but the basic principles remain.  The controls (stick and [[rudder]]) for rotary wing aircraft ([[helicopter]] or [[autogyro]]) accomplish the same motions about the [[aircraft principal axes|three axes of rotation]], but manipulate the rotating flight controls ([[Helicopter rotor|main rotor]] disk and [[tail rotor]] disk) in a completely different manner.

Flight control surfaces are operated by [[aircraft flight control system]]s.

Considered as a generalized [[fluid dynamics|fluid control]] surface, rudders, in particular, are shared between [[aircraft]] and [[watercraft]].