IL.XIV.I.S1

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 6-3
  Chapter 6: Flight Controls › Flight Control Systems › Ailerons

  Moving the control wheel, or control stick, to the right causes the right aileron to deflect upward and the left aileron to deflect downward. The upward deflection of the right aileron decreases the camber resulting in decreased lift ... right wing. The corresponding downward deflection of the left aileron increases the camber resulting in increased lift on the left wing. Thus, the increased lift on the left wing and the decreased lift on the right wing causes the aircraft…

• Pilot's Handbook of Aeronautical Knowledgep. 6-8
  Chapter 6: Flight Controls › Flight Control Systems › V-Tail

  fixed surface in this case, to the vertical stabilizer or fin. The rudder is controlled by the left and right rudder pedals. When the rudder is deflected into the airflow, a horizontal force is exerted in the opposite direction. [Figure ... pushing the left pedal, the rudder moves left. This alters the airflow around the vertical stabilizer/rudder and creates a sideward lift that moves the tail to the right and yaws the nose of the airplane to the left. Rudder effectiveness…

• Pilot's Handbook of Aeronautical Knowledgep. 16-30
  Chapter 16: Navigation › Angle of Intercept › Automatic Direction Finder (ADF)

  station in relation to the nose of the aircraft. If the needle is deflected 30° to the left for a relative bearing of 330°, this means that the station is located 30° left. If the aircraft is turned left ... When the wind drift correction is established, the ADF needle indicates the amount of correction to the right or left. For instance, if the magnetic bearing to the station is 340°, a correction for a left crosswind would result…

• Pilot's Handbook of Aeronautical Knowledgep. 5-19
  Chapter 5: Aerodynamics of Flight › Aircraft Design Characteristics › Directional Stability (Yawing)

  stopped by the fin because while the aircraft is rotating to the right, the air is striking the left side of the fin at an angle. This causes pressure on the left side of the fin, which resists the turning ... during that moment (since it is assumed that although the yawing motion has stopped, the excess pressure on the left side of the fin still persists), there is necessarily a tendency for the aircraft to be turned partially back…

• Pilot's Handbook of Aeronautical Knowledgep. 8-15
  Chapter 8: Flight Instruments › Gyroscopic Flight Instruments › Precession

  clockwise direction when viewed from the right side of the bicycle, if a rider leans to the left, a force is applied to the top of the wheel to the left. The force actually acts 90° in the direction ... effect of applying a force to the front of the tire, causing the bicycle to move to the left. There is a need to turn the handlebars at low speeds because of the instability of the slowly turning gyros…

• Pilot's Handbook of Aeronautical Knowledgep. 5-31
  Chapter 5: Aerodynamics of Flight › Basic Propeller Principles › Torque Reaction

  during the takeoff roll, an additional turning moment around the vertical axis is induced by torque reaction. As the left side of the aircraft is being forced down by torque reaction, more weight is being placed on the left main ... landing gear. This results in more ground friction, or drag, on the left tire than on the right, causing a further turning moment to the left. The magnitude of this moment is dependent on many variables. Some of these variables…