AI.IX.D.S5b

From the FAA library

• Airplane Flying Handbookp. 10-7
  Chapter 10: Performance Maneuvers › Lazy Eight

  direction of the 45° reference point. The climbing turn should be planned and controlled so that the maximum pitch-up attitude is reached at the 45° point with an approximate bank angle of 15°. [Figure ... pitch attitude is raised, the airspeed decreases, which causes the rate of turn to increase. As such, the lazy eight should begin with a slow rate of roll as the combination of increasing pitch and increasing bank may cause…

• Airplane Flying Handbookp. 18-18
  Chapter 18: Emergency Procedures › Inadvertent VFR Flight Into IMC › Attitude Control

  level flight if properly trimmed and left alone. It is designed to maintain a state of equilibrium in pitch, roll, and yaw. The pilot should be aware, however, that a change about one axis affects the stability of the others ... typical light airplane exhibits a good deal of stability in the yaw axis, slightly less in the pitch axis, and even lesser still in the roll axis. The key to emergency airplane attitude control, therefore, is to: ⦁ Trim the airplane…

• Pilot's Handbook of Aeronautical Knowledgep. 5-24
  Chapter 5: Aerodynamics of Flight › Aerodynamic Forces in Flight Maneuvers › Forces in Climbs

  Figure 5-35. Normal, slipping, and skidding turns at a constant altitude. If the climb is entered with no change in power setting, the airspeed gradually diminishes because the thrust required to maintain a given airspeed in level flight ... insufficient to maintain the same airspeed in a climb. When the flight path is inclined upward, a component of the aircraft’s weight acts in the same direction as, and parallel to, the total drag of the aircraft, thereby increasing…

• Airplane Flying Handbookp. 3-20
  Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns › Climbing Turns

  pitch attitude should be decreased smoothly and slowly to allow for the airspeed to increase. A loss of altitude may result if the pitch attitude is changed too rapidly without allowing the airspeed to increase proportionately. After the airplane ... established in level flight at a constant altitude, climb power should be retained temporarily so that the airplane accelerates to the cruise airspeed. When the airspeed reaches the desired cruise airspeed, the throttle setting and the propeller control, if equipped…

• 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…

• Instrument Flying Handbookp. 7-20
  Chapter 7, Section I: Airplane Basic Flight Maneuvers › Turns › Standard Rate Turns

  coordinator indicates a standard rate turn. During the roll-in, check the altimeter, VSI, and attitude indicator for the necessary pitch adjustments as the vertical lift component decreases with an increase in bank. If constant airspeed is to be maintained ... Pitch, power, and trim adjustments are made as changes in vertical lift component and airspeed occur. The ball should be checked throughout the turn, especially if control pressures are held rather than trimmed off. Figure 7-33. Standard rate turn…