TEST BORRADO, QUIZÁS LE INTERESE:
Commercial Pilot - (CH. 1) Basic Aerodynamics FIG
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Título del Test:
Commercial Pilot - (CH. 1) Basic Aerodynamics FIG Descripción: Examen PC DGAC Autor:
Fecha de Creación: 06/03/2024 Categoría: Otros Número Preguntas: 11 |
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6.- Figure 3
The L/D ratio at a 2° angle of attack is approximately the same as the
L/D ratio for a 9.75° angle of attack. 10.5° angle of attack. 16.5° angle of attack. 8.- Figure 3 If an airplane glides at an angle of attack of 10°, how much altitude will it lose in 1 mile? 240 feet. 480 feet. 960 feet. 9.- Figure 4 What is the stall speed of an airplane under a load factor of 2 Gs if the unaccelerated stall speed is 60 knots? 66 knots. 74 knots. 84 knots. 15.- Figure 3 How much altitude will this airplane lose in 3 miles of gliding at an angle of attack of 8°? 440 feet. 880 feet. 1,320 feet. 16.- Figure 4 What increase in load factor would take place if the angle of bank were increased from 60° to 80°? 3 Gs. 3.5 Gs. 4 Gs. 27.- Figure 5 The horizontal dashed line from point C to point E represents the ultimate load factor. positive limit load factor. airspeed range for normal operations. 33.- Figure 5 The vertical line from point E to point F is represented on the airspeed indicator by the upper limit of the yellow arc. upper limit of the green arc. blue radial line. 51.- (Ver figura 1) At the airspeed represented by point A, in steady flight, the airplane will have its maximum L/D ratio. have its minimum L/D ratio. be developing its maximum coefficient of lift. 54.- (Ver Figura 1) At an airspeed represented by point B, in steady flight, the pilot can expect to obtain the airplane's maximum endurance. glide range. coefficient of lift. 62.- (Ver Figura 2) Select the correct statement regarding stall speeds. Power-off stalls occur at higher airspeeds with the gear and flaps down. In a 60° bank the airplane stalls at a lower airspeed with the gear up. Power-on stalls occur at lower airspeeds in shallower banks. 67.- (Ver Figura 2) Select the correct statement regarding stall speeds. The airplane will stall 10 knots higher in a power-on 60° bank with gear and flaps up than with gear and flaps down. 25 knots lower in a power-off, flaps up, 60° bank, than in a power-off, flaps down, wings-level configuration. 10 knots higher in a 45° bank, power-on stall than in a wings-level stall with flaps up. |
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