IL.VIII.G.S9
SkillTouch down at the appropriate speed, aircraft configuration and pitch attitude.
From the FAA library
- 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 5: Aerodynamics of Flight › High Speed Flight › Subsonic Versus Supersonic Flow
Compressibility (and to a lesser extent viscosity) is of paramount importance at speeds approaching the speed of sound. In these speed ranges, compressibility causes a change in the density of the air around an aircraft. During flight, a wing produces ... lift by accelerating the airflow over the upper surface. This accelerated air can, and does, reach sonic speeds even though the aircraft itself may be flying subsonic. At some extreme AOAs, in some aircraft, the speed of the air over…
- Chapter 7. Safety of Flight › Section 4. Wake Turbulence › 7-4-6. Vortex Avoidance Procedures
Landing behind a larger aircraft- when parallel runway is closer than 2,500 feet. Consider possible drift to your runway. Stay at or above the larger aircraft’s final approach flight path- note its touchdown point. 3. Landing behind ... larger aircraft- crossing runway. Cross above the larger aircraft’s flight path. 4. Landing behind a departing larger aircraft- same runway. Note the larger aircraft’s rotation point-land well prior to rotation point. 5. Landing behind a departing larger…
- Chapter 5: Aerodynamics of Flight › Axes of an Aircraft
Whenever an aircraft changes its flight attitude or position in flight, it rotates about one or more of the three axes. [Figure 5-18] The aircraft’s motion about its longitudinal axis resembles the roll of a ship from side ... side. In fact, the names used to describe the motion about an aircraft’s three axes were originally nautical terms. They have been adapted to aeronautical terminology due to the similarity of motion of aircraft and seagoing ships. The motion…
- Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance
retarding effect of factors such as snow or ice Landing Performance In many cases, the landing distance of an aircraft defines the runway requirements for flight operations. The minimum landing distance is obtained by landing at some minimum safe speed ... that allows sufficient margin above stall and provides satisfactory control and capability for a go-around. Generally, the landing speed is some fixed percentage of the stall speed or minimum control speed for the aircraft in the landing configuration…