33-06. FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
Всего заданий: 36
В режиме ОБУЧЕНИЕ показываются все задания дисциплины с предъявлением правильных ответов. Для перехода к следующему заданию нажать кнопку «Далее».
Заданий на экзамен: 30
В режиме ЭКЗАМЕН правильные ответы не показываются, переход на следующее задание происходит автоматически, после выбора ответа.
1. During an IFR flight in a Beech Bonanza the fuel indicators show that the remaining amount of fuel is 100 lbs after 38 minutes. The total takeoff fuel at departure was 160 lbs. For the alternate fuel, 30 lbs is necessary. The planned fuel for taxi was 13 lbs. Final reserve fuel is estimated at 50 lbs. If the fuel flow remains the same, how many minutes can be flown to the destination with the remaining fuel?
2. A VFR flight in Piper SENECA III. At a fuel check you have 60 US gallons (USG) of usable fuel remaining. Alternate fuel required is 12 USG. The flight time remaining is 1 hr 35 min. What is the highest consumption rate acceptable?
3. (Refer to figure 033-55)
What is the minimum pressure altitude at which the conditions below may be met? Given:
Distance to alternate: 950 NM
Headwind component: 20 kts
Mass at point of diversion: 50.000 kg
Diversion fuel available: 5.800 kg
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4. Flight planning chart for an aeroplane states, that the time to reach the cruising level at a given gross mass is 36 minutes and the distance travelled is 157 NM (zero- wind). What will be the distance travelled with an average tailwind component of 60 kts?
5. A twin-jet aeroplane carries out the WASHINGTON — PARIS flight. When it reaches point K (35°N 048°W) a non- mechanical event makes the Captain consider rerouting to one of the three following fields. The flight conditions are:
from K to BERMUDAS (distance 847 NM, headwind component = 18 kts)
from K to SANTA MARIA (distance 1.112 NM, tailwind component = 120 kts)
from K to GANDER (distance 883 NM, wind component = 0)
With an aeroplane true airspeed of 460 kts, the field selected will be that more rapidly reached:
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