IL.XIV.I.R5

From the FAA library

• Aviation Instructor's Handbookp. 9-7
  Chapter 9: Techniques of Flight Instruction › The Telling-and-Doing Technique › Instructor Tells—Instructor Does

  maintain altitude. Maintain coordinated flight by applying rudder in the direction of the turn. ⦁ Remember, the ailerons control the roll rate, as well as the angle of bank. The rate at which the aircraft rolls depends on how much aileron ... deflection is used. How far the aircraft rolls (steepness of the bank) depends on how long the ailerons are deflected, since the aircraft continues to roll as long as the ailerons are deflected. When the desired angle of bank…

• Pilot's Handbook of Aeronautical Knowledgep. 5-23
  Chapter 5: Aerodynamics of Flight › Aerodynamic Forces in Flight Maneuvers › Forces in Turns

  horizontal component of lift. It is found that the horizontal component of lift is proportional to the angle of bank—that is, it increases or decreases respectively as the angle of bank increases or decreases. As the angle of bank ... increasing the rate of turn (ROT). Consequently, at any given airspeed, the ROT can be controlled by adjusting the angle of bank. To provide a vertical component of lift sufficient to hold altitude in a level turn, an increase…

• Pilot's Handbook of Aeronautical Knowledgep. 6-4
  Chapter 6: Flight Controls › Flight Control Systems › Adverse Yaw

  ailerons, rudder, and elevator. Applying aileron pressure is necessary to place the aircraft in the desired angle of bank, while simultaneous application of rudder pressure is necessary to counteract the resultant adverse yaw. Additionally, because more lift is required during ... turn than during straight-and-level flight, the angle of attack (AOA) must be increased by applying elevator back pressure. The steeper the turn, the more elevator back pressure that is needed. As the desired angle of bank is established…

• Pilot's Handbook of Aeronautical Knowledgep. 5-26
  Chapter 5: Aerodynamics of Flight › Angle of Attack Indicators

  between the current AOA that the airfoil is operating at, and the AOA at which the airfoil will stall (critical AOA). Figure 5-39. Increase in stall speed and load factor. Figure 5-40. Inflight ice formation. Angle of attack ... Speed by itself is not a reliable parameter to avoid a stall. An airplane can stall at any speed. Angle of attack is a better parameter to use to avoid a stall. For a given configuration, the airplane always stalls…

• Pilot's Handbook of Aeronautical Knowledgep. 5-13
  Chapter 5: Aerodynamics of Flight › Moment and Moment Arm

  moment arm is the distance from a datum [reference point or line] to the applied force.) For aircraft weight and balance computations, “moments” are expressed in terms of the distance of the arm times the aircraft’s weight, or simply ... will not cause the aircraft to pitch when power is changed, and there will be no difference in moment due to thrust for a power-on or power-off condition of flight. Although designers have some control over the location…

• Pilot's Handbook of Aeronautical Knowledgep. 17-9
  Chapter 17: Aeromedical Factors › Health and Physiological Factors Affecting Pilot Performance › Diving or Rolling Beyond the Vertical Plane

  Diving or Rolling Beyond the Vertical Plane This maneuver may produce extreme disorientation. While in straight-and-level flight, the pilot should sit normally, either with eyes closed or gaze lowered to the floor. The instructor pilot starts a positive ... coordinated roll toward a 30° or 40° angle of bank. As this is in progress, the pilot tilts his or her head forward, looks to the right or left, then immediately returns his or her head to an upright position…