Chapter 2.2 - Flight Control Flashcards
What are the main primary controls used to fly an aircraft (3)?
- Throttle.
- Pitch Attitude.
- Bank Attitude.
What determines an Aircraft’s performance?
Power and Attitude.
Name the 3 reference axes of an aircraft?
- Lateral.
- Longitudinal.
- Normal.
Name the 3 movements each axes has on an aircraft?
- Pitch (Lateral).
- Roll (Longitudinal).
- Yaw (Normal).
Name the 3 controls which effect the axes of an aircraft?
- Elevator/Stabilator (Pitch).
- Ailerons (Roll).
- Rudder (Yaw).
True or False. The normal axis is the same as vertical axis?
False.
All axes are connected through what?
Centre of Gravity (CG).
The Normal Axis is found?
Perpendicular to the plane’s Lateral and Longitudinal axes.
Where can a parent Aerofoil be found on an Aircraft (3)?
- Wing.
- Tailplane (Horizontal Stabilizer).
- Fin (Vertical Stabilizer).
A pilot must alter the degree of deflection of the control surfaces to maintain what?
Desired Attitude.
Degree of deflection is necessary to resists what?
- Disturbing Influences (Turbulence).
- Attain New Attitudes (Flight Path).
The Elevators/Stabilator are used to control what?
Pitch Attitude of an Aircraft.
What happens when the Control Wheel is pushed forward (name the control surface)?
The Elevators move down, thus the nose of the Aircraft goes down.
What happens when the Control Wheel is pulled back (name the control surface)?
The Elevators move up, thus the nose of the Aircraft goes up.
The Ailerons are used to control what?
Bank Attitude of an Aircraft.
What happens when the Control Wheel is turned to the right (name the control surface)?
Right Aileron is raised and the left is depressed, thus turning the Aircraft to the right.
What happens when the Control Wheel is turned to the left (name the control surface)?
Left Aileron is raised and the right is depressed, thus turning the Aircraft to the left.
The Rudder is used to control what?
The yawing of an Aircraft.