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.


Случайные 5 вопросов:
1. The takeoff distance of an aircraft is 600 m in standard atmosphere, no wind at 0 ft pressure-altitude. Using the following corrections:
± 20 ml 1.000 ft field elevation
— 5 m /kts headwind
+ 10 mlkts tailwind
± 15 m /% runway slope
±5 m/»C deviation from standard temperature
The takeoff distance from an airport at 1.000 ft elevation, temperature 17 «C, QNH 1.013,25 hPa, 1% up-slope, 10 kts tailwind is:
.

2. (Refer to figure 032-08)
Given:
OAT: — 20 °C, Pressure Altitude: 14.000 ft, Gross Mass: 4.000 lbs
Other conditions as associated in the header of the graph.
What is the one engine inoperative rate of climb?
.

3. (Refer to figure 032-05)
Given:
OAT: -15 °C, Pressure Altitude: 4.000 ft
RWY: 12R, Wind: 080V12 kts
Takeoff Mass: 4.000 lbs
Other conditions as associated in the header of the graph.
What is the takeoff distance over a 50 ft obstacle?
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4. At a given mass, the stalling speed of a light twin engine piston aircraft is 100 kts in the landing configuration. The minimum speed a pilot must maintain on short final is:
5. Following a takeoff determined by the 50 ft (15 m) screen height, a light twin climbs on a 10% over-the-ground climb gradient. It will clear a 900 m high obstacle in relation to the runway (horizontally), situated at 10.000 m from the 50 ft clearing point with an obstacle clearance of: