AI.IX.C.S5

From the FAA library

• Airplane Flying Handbookp. 10-5
  Chapter 10: Performance Maneuvers › Chandelle

  rate of rollout is too rapid or sluggish, the airplane either exceeds the 180° turn or does not complete the turn as the wings come level to the horizon. Figure 10-3. Chandelle. Prior to starting the chandelle, the flaps ... traffic and hazards. The maneuver should be entered from straight-and-level flight or a shallow dive at an airspeed recommended by the manufacturer—in many cases this is the airplane’s design maneuvering speed (VA) or operating maneuvering speed…

• Airplane Flying Handbookp. 3-19
  Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns › Establishing a Climb

  Establishing a Climb A straight climb is entered by gently increasing back pressure on the elevator flight control to the pitch attitude referencing the airplane’s nose to the natural horizon while simultaneously increasing engine power to the climb power ... setting. The wingtips should be referenced in maintaining the climb attitude while cross-checking the flight instruments to verify performance. In many airplanes, as power is increased, an increase in slipstream over the horizontal stabilizer causes the airplane’s pitch…

• 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. 3-11
  Chapter 3: Basic Flight Maneuvers › Level Turns

  throttle provides thrust, which may be used for airspeed control and to vary the radius of the turn. ⦁ The pilot uses the rudder to offset any adverse yaw developed by wing’s differential lift and the engine/propeller. The rudder does ... turn the airplane. The rudder is used to maintain coordinated flight. For purposes of this discussion, turns are divided into three classes: shallow, medium, and steep. ⦁ Shallow turns—bank angle is approximately 20° or less. This shallow bank is such…

• Airplane Flying Handbookp. 5-11
  Chapter 5: Maintaining Aircraft Control: Upset Prevention and Recovery Training › Slow Flight › Maneuvering in Slow Flight

  airplanes, torque, slipstream effect, and P-factor may produce a strong left yaw, which requires right rudder input to maintain coordinated flight. The closer the airplane is to the 1G stall, the greater the amount of right rudder pressure required ... Figure 5-7. Slow flight—low airspeed, high angle of attack, high power, and constant altitude. Maneuvering in Slow Flight When the desired pitch attitude and airspeed have been established in straight-and-level slow flight, the pilot needs…

• Instrument Flying Handbookp. 8-8
  Chapter 8: Helicopter Attitude Instrument Flying › Turn Indicator › Power Control During Straight-and-Level Flight

  airspeed is changing, adjust the pitch attitude to maintain a constant altitude. A constant heading should be maintained throughout the change. As the desired airspeed is approached, adjust power to the new cruising power setting and further adjust pitch attitude ... maintain altitude. The instrument indications for straight-and-level flight at normal cruise and during the transition from normal cruise to slow cruise are illustrated in Figures 8-9 and 8-10. After the airspeed stabilizes at slow cruise…