Flight Controls: Overview

081-05-01Pablo Asensio Martínez2026-04-011 min

Primary Control Services

Controls that rotate the aircraft around its three axes:

  1. Elevator (Pitch / Lateral Axis).
  2. Ailerons (Roll / Longitudinal Axis).
  3. Rudder (Yaw / Normal Axis).

Secondary Flight Controls

Used to change the aerodynamic configuration or assist primary controls.

  • Trim Tabs: Relieve control forces.
  • Balance Tabs: Assist in moving the control surface (reduce force).
  • Anti-Balance Tabs: Increase control feel (increase force).
  • Flaps/Slats: High lift devices.
  • Spoilers: Lift dumpers / Airbrakes.

Interaction

  • Maneuverability vs Stability: A highly stable aircraft is harder to control (heavy controls). A highly maneuverable aircraft (like a fighter) is less stable.
  • Control Reversal: At very high speeds, aeroelastic twisting of the wing can cause aileron reversal (deflecting aileron down twists the wing leading edge down, reducing lift instead of increasing it).
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.