AI.XII.F.S9

From the FAA library

• Airplane Flying Handbookp. 13-26
  Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › VMC Demo

  slows the airplane to approximately 10 knots above VSSE or VYSE (whichever is higher) and trims for takeoff. For the remainder of the maneuver, the trim setting remains unaltered. The pilot selects an entry heading and sets high ... 5° (a right bank in this case) may be established as appropriate for the airplane make and model. While maintaining entry heading, the pitch attitude is slowly increased to decelerate at a rate of 1 knot per second (no faster…

• Airplane Flying Handbookp. 5-9
  Chapter 5: Maintaining Aircraft Control: Upset Prevention and Recovery Training › Slow Flight

  pilot training and testing purposes, slow flight includes two main elements: ⦁ Slowing to, maneuvering at, and recovering from an airspeed at which the airplane is still capable of maintaining controlled flight without activating the stall warning—5 to 10 knots ... appropriate to takeoffs, climbs, descents, approaches to landing, and go-arounds. Slow flight should be introduced with the target airspeed sufficiently above the stall to permit safe maneuvering, but close enough to the stall warning for the pilot to experience…

• Pilot's Handbook of Aeronautical Knowledgep. 5-3
  Chapter 5: Aerodynamics of Flight › Thrust

  vectors during a stabilized climb. Likewise, if the engine power is increased, thrust becomes greater than drag and the airspeed increases. As long as the thrust continues to be greater than the drag, the aircraft continues to accelerate. When drag ... equals thrust, the aircraft flies at a constant airspeed. Straight-and-level flight may be sustained at a wide range of speeds. The pilot coordinates AOA and thrust in all speed regimes if the aircraft is to be held…

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

  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 is insufficient to maintain the same airspeed ... aircraft, thereby increasing the total effective drag. Consequently, the total effective drag is greater than the power, and the airspeed decreases. The reduction in airspeed gradually results in a corresponding decrease in drag until the total drag (including the component…

• 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. 8-13
  Chapter 8: Helicopter Attitude Instrument Flying › Turns

  Errors During Straight Climbs and Descents 1. Failure to maintain heading 2. Improper use of power 3. Poor control of pitch attitude 4. Failure to maintain proper pedal trim 5. Failure to level off on desired altitude Turns Turns made ... airspeed. A simple way to determine this amount is to divide the airspeed by 10 and add one-half the result. For example, at 60 knots approximately 9° of bank is required (60 ÷ 10…