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  2. Trim tab - Wikipedia

    en.wikipedia.org/wiki/Trim_tab

    Trim tabs are variously integrated into the rudder, elevators, and ailerons of a fixed-wing aircraft. As such, they are elements of an aircraft's system for allowing the pilot to control and maintain airspeed with a minimum of inputs and mental concentration. Many newer aircraft, especially jet aircraft, have electric trim controls.

  3. Empennage - Wikipedia

    en.wikipedia.org/wiki/Empennage

    a servo tab used to move the main control surface, as well as act as a trim tab. Usually controlled by a cockpit wheel or crank. [5] Multi-engined aircraft often have trim tabs on the rudder to reduce the pilot effort required to keep the aircraft straight in situations of asymmetrical thrust, such as single engine operations. [7]

  4. Flight control surfaces - Wikipedia

    en.wikipedia.org/wiki/Flight_control_surfaces

    Most fixed-wing aircraft have a trimming control surface on the elevator, but larger aircraft also have a trim control for the rudder, and another for the ailerons. The rudder trim is to counter any asymmetric thrust from the engines. Aileron trim is to counter the effects of the centre of gravity being displaced from the aircraft centerline ...

  5. Wag-Aero CUBy - Wikipedia

    en.wikipedia.org/wiki/Wag-Aero_CUBy

    The aircraft does differ from the original Piper design in several ways including having its fuselage fabricated from 4130 steel instead of the Cub's original 1025 carbon steel and utilizing a conventional elevator-mounted trim tab in place of the Cub's jack screw trimming system that adjusts the Cub's elevator angle of incidence. [2] [6]

  6. Stabilizer (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Stabilizer_(aeronautics)

    A Boeing 737 uses an adjustable stabilizer, moved by a jackscrew, to provide the required pitch trim forces. Generic stabilizer illustrated. A horizontal stabilizer is used to maintain the aircraft in longitudinal balance, or trim: [3] it exerts a vertical force at a distance so the summation of pitch moments about the center of gravity is zero. [4]

  7. Aircraft flight control system - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_control_system

    Cockpit controls and instrument panel of a Cessna 182D Skylane. Generally, the primary cockpit flight controls are arranged as follows: [2] A control yoke (also known as a control column), centre stick or side-stick (the latter two also colloquially known as a control or joystick), governs the aircraft's roll and pitch by moving the ailerons (or activating wing warping on some very early ...

  8. Embraer Phenom 300 - Wikipedia

    en.wikipedia.org/wiki/Embraer_Phenom_300

    The Embraer EMB-505 Phenom 300 is a light business jet designed and produced by the Brazilian aerospace manufacturer Embraer. Certified for single-pilot operations, it can carry up to 11 occupants. [4] Work on the Phenom 300 started in response to customer demands for a larger business aircraft than the Phenom 100, a very light jet. While the ...

  9. Vertical stabilizer - Wikipedia

    en.wikipedia.org/wiki/Vertical_stabilizer

    A trim tab may similarly be mounted on the rudder. Together, their role is to enable trim in the yaw direction (compensate moments in yaw generated by any asymmetry in thrust or drag ), enable the aircraft to be controlled in yaw (for example, to initiate side slip during a crosswind landing ), as well as provide stability in yaw (weathercock ...

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