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AI.VII.E.R1

Risk management

Selection of runway based on pilot capability, airplane performance and limitations, available distance, and wind.

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From the FAA library

  • Chapter 6: Takeoffs and Departure Climbs › Short-Field Takeoff and Maximum Performance Climb

    runway is long enough or if no obstacles exist, ground effect can be used to the pilot’s advantage by using the reduced drag to improve initial acceleration. When taking off from an unsatisfactory surface, the pilot should apply ... ground run and lift-off, using ground effect as an aid, prior to attaining true flying speed. The pilot should reduce AOA to attain normal airspeed before attempting to fly out of the ground effect areas. Short-Field Takeoff…

  • Chapter 6: Takeoffs and Departure Climbs › Short-Field Takeoff and Maximum Performance Climb › Initial Climb

    premature lift-off. The objective is to rotate to the appropriate pitch attitude at (or near) VX. The pilot should be aware that some airplanes have a natural tendency to lift off well before reaching VX. In these airplanes ... necessary to allow the airplane to lift off in ground effect and then reduce pitch attitude to level until the airplane accelerates to VX with the wheels just clear of the runway surface. This method is preferable to forcing…

  • Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Takeoff Performance

    Figure 11-19 illustrates the general effect of wind by the percent change in takeoff or landing distance as a function of the ratio of wind velocity to takeoff or landing speed. The effect of proper takeoff speed is especially ... important when runway lengths and takeoff distances are critical. The takeoff speeds specified in the AFM/POH are generally the minimum safe speeds at which the aircraft can become airborne. Any attempt to take off below the recommended speed means that…

  • Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance

    cases, the pilot must make an accurate prediction of takeoff distance from the performance data of the AFM/POH, regardless of the runway available, and strive for a polished, professional takeoff procedure. In the prediction of takeoff distance from the AFM/POH ... following primary considerations must be given: • Pressure altitude and temperature—to define the effect of density altitude on distance • Gross weight—a large effect on distance • Wind—a large effect due to the wind or wind component along the runway…

  • Chapter 13: Transition to Multiengine Airplanes › Performance and Limitations

    highest altitude at which the airplane can maintain a steady rate of climb of 100 fpm with both engines operating. The airplane has reached its absolute ceiling when climb is no longer possible. ⦁ The single-engine service ceiling is reached ... when the multiengine airplane can no longer maintain a 50 fpm rate of climb with OEI, and its single-engine absolute ceiling when climb is no longer possible. The takeoff in a multiengine airplane should be planned in sufficient detail…