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.


Случайные 5 вопросов:
1. (Refer to figure 033-29)
ETOPS — Aircraft can not travel more than 120 minutes from an adequate airfield. Assume LRC and diversion weight of 40.000 kg. What is the still air diversion distance?

2. An aeroplane flies at an airspeed of 380 kts. It flies from A to В and back to A. Distance AB = 480 NM. When going from A to B, it experiences a headwind component = 60 kts. The wind remains constant. The duration of the flight will be:
3. 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?
4. (Refer to figure 033-55)
What is the minimum pressure altitude at which the conditions listed below may be met? Given:
Diversion distance: 720 NM
Tailwind component: 25 kts
Mass at point of diversion: 55.000 kg
Temperature: ISA
Diversion fuel available: 4.250 kg
.

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:
.