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IL.V.E.R6

Risk management

Potential powerplant failure during takeoff or other malfunction considering operational factors such as aircraft characteristics, runway/takeoff path length, surface conditions, environmental conditions, and obstructions.

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From the FAA library

  • 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 › Performance › Straight-and-Level Flight

    Straight-and-Level Flight All of the principal components of flight performance involve steady-state flight conditions and equilibrium of the aircraft. For the aircraft to remain in steady, level flight, equilibrium must be obtained by a lift equal ... aircraft weight and a powerplant thrust equal to the aircraft drag. Thus, the aircraft drag defines the thrust required to maintain steady, level flight. As presented in Chapter 4, Aerodynamics of Flight, all parts of an aircraft contribute…

  • Chapter 11: Aircraft Performance › Takeoff and Landing Performance

    Takeoff and Landing Performance The majority of pilot-caused aircraft accidents occur during the takeoff and landing phase of flight. Because of this fact, the pilot must be familiar with all the variables that influence the takeoff and landing performance ... aircraft and must strive for exacting, professional procedures of operation during these phases of flight. Takeoff and landing performance is a condition of accelerated and decelerated motion. For instance, during takeoff an aircraft starts at zero speed and accelerates…

  • Chapter 16: Transition to Jet-Powered Airplanes › Jet Airplane Takeoff and Climb › Takeoff Roll

    pilot not flying. Retarding a thrust lever would only be necessary in case an engine exceeds any limitation. Takeoff data, including V1/VR and V2 speeds, takeoff power settings, and required field length should be computed prior to each takeoff ... make and model without an FMS, the data should be recorded on a takeoff data card. This data is based on airplane weight, runway length available, runway gradient, field temperature, field barometric pressure, wind, icing conditions, and runway condition. Both…

  • Chapter 4. Air Traffic Control › Section 3. Airport Operations › 4-3-25. Flight Inspection/‘Flight Check’ Aircraft in Terminal Areas

    discretion of the pilot-in-command, all exterior lights should be illuminated when taxiing on or across any runway. This increases the conspicuousness of the aircraft to controllers and other pilots approaching to land, taxiing, or crossing the runway. Pilots ... should comply with any equipment operating limitations and consider the effects of landing and strobe lights on other aircraft in their vicinity. g. When entering the departure runway for takeoff or to “line up and wait,” all lights, except…