AI.II.D.K4

From the FAA library

• Airplane Flying Handbookp. 3-23
  Chapter 3: Basic Flight Maneuvers › Glides › Gliding Turns

  rudder inputs as a result of reduced flight control pressures. 3. The normal stability and inherent characteristics of the airplane to nose-down with the power off. These three factors make it necessary to use more back pressure ... gliding turn; however, the required rudder pedal pressures are reduced as a result of the reduced forces acting on the control surfaces. A learner may apply excessive rudder pedal pressures based on experience with powered flight. This overcontrol…

• Airplane Flying Handbookp. 3-2
  Chapter 3: Basic Flight Maneuvers › Effect and Use of Flight Controls

  left shoulder to the pilot’s right shoulder. ⦁ When forward pressure is applied to the left rudder pedal, the airplane’s nose moves (yaws) to the left in relation to the pilot. Think of this movement from the pilot ... long as all forces acting upon them remain balanced. Resistance to movement increases as airspeed increases and decreases as airspeed decreases. Resistance also increases as the controls move away from a streamlined position. While maneuvering the airplane…

• Pilot's Handbook of Aeronautical Knowledgep. 3-14
  Chapter 4: Principles of Flight

  physical laws governing the forces acting on an aircraft in flight, and what effect these natural laws and forces have on the performance characteristics of aircraft. To control an aircraft, be it an airplane, helicopter, glider, or balloon, the pilot…

• Pilot's Handbook of Aeronautical Knowledgep. 5-2
  Chapter 5: Aerodynamics of Flight

  Figure 5-2] Figure 5-1. Relationship of forces acting on an aircraft. In glides, a portion of the weight vector is directed along the forward flight path and, therefore, acts as thrust. In other words, any time the flight ... angle of attack (AOA). Since the early days of flight, AOA is fundamental to understanding many aspects of airplane performance, stability, and control. The AOA is defined as the acute angle between the chord line of the airfoil…

• Airplane Flying Handbookp. 3-12
  Chapter 3: Basic Flight Maneuvers › Level Turns

  airplane is banked into a turn, total lift is the resultant of two components: vertical and horizontal. [Figure 3-11] The vertical lift component continues to act perpendicular to the earth and opposes gravity. The horizontal lift component acts parallel ... lift components act at right angles to each other, causing the resultant total lifting force to act perpendicular to the banked wing of the airplane. It is the horizontal lift component that begins to turn the airplane…

• Aviation Maintenance Technician Handbook - Generalp. 5-36
  Chapter 5: Physics for Aviation › Aircraft Theory of Flight › Four Forces of Flight

  aircraft. Names like fuselage, empennage, wing, and so many others, come into play when describing what an airplane is and how it operates. For helicopters, names like main rotor, anti-torque rotor, and autorotation come to mind as a small ... understanding why aircraft operate the way they do. Four Forces of Flight During flight, there are four forces acting on an airplane. These forces are lift, weight, thrust, and drag. [Figure 5-53] Lift is the upward force created…