32-03. PERFORMANCE CLASS B — MULTI-ENGINE AEROPLANES
Всего заданий: 90
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. Large flap settings:
2. The climb gradient of an aircraft after takeoff is 6% in standard atmosphere, no wind, at 0 ft pressure altitude. Using the following corrections:
± 0,2% I1.000 ft field elevation ±0,1%/°C from standard temperature -1% with wing anti-ice — 0,5% with engine anti-ice
The climb gradient after takeoff from an airport situated at 1.000 ft, 17 °C; QNH 1.013,25 hPa, with wing and engine anti-ice operating for a functional check is:
.
3. Changing the takeoff flap setting from flap 15° to flap 5° will normally result in:
4. (Refer to figure 032-08)
Given:
OAT: 0 °C, Pressure Altitude: 18.000 ft, Gross Mass: 3.750 lbs
Mixture: leaned to 25°F rich of peak EGT Other conditions as associated in the header of the graph.
What is the two-engine rate of climb?
.
5. (Refer to figure 032-06)
Given:
OAT: 20 °C, Pressure Altitude: 2.000 ft
RWY: 24L, Wind: 120V8 kts
Takeoff Mass: 4.500 lbs, Heavy Duty Brakes installed.
Other conditions as associated in the header of the chart.
Find the Accelerate-Stop distance:
.
