32-02. PERFORMANCE CLASS B — SINGLE-ENGINE AEROPLANES
Всего заданий: 51
В режиме ОБУЧЕНИЕ показываются все задания дисциплины с предъявлением правильных ответов. Для перехода к следующему заданию нажать кнопку «Далее».
Заданий на экзамен: 10
В режиме ЭКЗАМЕН правильные ответы не показываются, переход на следующее задание происходит автоматически, после выбора ответа.
1. (Refer to figure 032-01)
With regard to the takeoff performance chart for the single engine aeroplane determine the maximum Allowable Takeoff Mass. Given:
OAT: ISA
Pressure Altitude: 4.000 ft, Headwind component: 5 kts
Flaps: up, Runway: Tarred and Dry, Factored runway length: 2.000 ft
Obstacle height: 50 ft
.
2. (Refer to figure 032-01)
An extract of the flight manual of a single engine propeller aircraft is reproduced in the diagram. Airport characteristics: hard, dry and zero slope runway. Actual conditions are:
Pressure Altitude: 1.500 ft, Outside Temperature: +18 °C
Wind Component: 4 knots tailwind
For a Takeoff Mass of 1.270 kg, the takeoff distance will be:
.
3. (Refer to figure 032-03)
Using the climb performance chart, for the single engine aeroplane, determine the ground distance to reach a height of 1.500 ft above the reference zero in the following conditions, given:
OAT at Takeoff: ISA
Airport pressure altitude: 5.000 ft
Aeroplane mass: 3.200 lbs, Speed: 100 KIAS
Wind component: 5 kts Tailwind
.
4. The maximum indicated air speed of a piston engined aeroplane, in level flight, is reached:
5. (Refer to figure 032-04)
With regard to the landing chart for the single engine aeroplane determine the minimum runway length. Given:
OAT: ISA
Pressure Altitude: 1.000 ft, Aeroplane Mass: 3.500 lbs
Tailwind component: 5 kts, Flaps: Landing position (down)
Runway: Tarred and Wet, Runway Slope: 2% upslope
.
