33-06. (H) FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
Всего заданий: 23
В режиме ОБУЧЕНИЕ показываются все задания дисциплины с предъявлением правильных ответов. Для перехода к следующему заданию нажать кнопку «Далее».
Заданий на экзамен: 15
В режиме ЭКЗАМЕН правильные ответы не показываются, переход на следующее задание происходит автоматически, после выбора ответа.
1. An aircraft is in cruising flight at FL140 at TAS 200 kts. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2.000 ft (QNH 1.030 hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent?
2. Given CAS/RAS of 130 kts, OAT 0 °С at 10.000 ft, trip distance of 240 NGM, track 275° (T) and W/V 030/30 kts. What is your true heading and time enroute?
3. 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:
.
4. On a flight from (47°10’N 010°00’E) to (49°10’N 010°00’E) at a TAS of 140 kts with a 20 kts headwind component, how many nautical air miles do you fly?
5. An aircraft flying at 7.500 ft is cleared to descend to be level at 1.000 ft, 6 NM before reaching a beacon. If ground speed is 156 kts and Rate of Descent is 800 ft/min, how many miles before the beacon should descent begin?
