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  • Chapter 11: Aircraft Performance › Performance › Straight-and-Level Flight

    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 to the 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 to the drag…

  • 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 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 ... 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 the aircraft could stall, be difficult…

  • Chapter 1: Introduction To Flying › Aircraft Classifications and Ultralight Vehicles

    Airplane—an engine-driven fixed-wing aircraft heavier than air, that is supported in flight by the dynamic reaction of the air against its wings. • Glider—a heavier-than-air aircraft, that is supported in flight by the dynamic reaction ... against its lifting surfaces and whose free flight does not depend principally on an engine. • Lighter-than-air aircraft—an aircraft that can rise and remain suspended by using contained gas weighing less than the air that is displaced…

  • Chapter 10: Teaching Practical Risk Management during Flight Instruction › Notes on Instructional Risk Management in the Flight Deck › Managing Risk while Teaching Landings

    Managing Risk while Teaching Landings Many complex decisions are made during the landing phase. Novice learner pilots have little experience to rely on. Instructors sometimes fall prey to teaching landings mechanically. Instead, it is necessary to convey problems and solutions ... equipped to identify or manage constantly changing conditions. This teaching method may result in unstable approaches and faulty landings. The instructor should prompt the learner on the current conditions and how to correct the situation to maintain a stabilized approach…

  • 14 CFR § 61.195 Flight instructor limitations and qualifications.

    training is conducted provided the pilot receiving the training holds a pilot certificate with category and class ratings appropriate to the aircraft in which the training is being conducted. (m) Training in an aircraft with a simplified flight controls designation ... flight instructor may not conduct instruction in a simplified flight control designation aircraft unless they hold the appropriate category and class rating prior to adding the make and model endorsement required by § 61.31(l). (n) Initial cadre training…