33-06. FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
All questions: 24
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Questions for exams: 20
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1. 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:
2. 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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3. 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?
4. After flying for 16 min at 100 kts TAS with a 20 kts tailwind component, you have to return to the airfield of departure. You will arrive after:
5. How many feet you have to climb to reach FL75? Given: Departure aerodrome elevation: 1.500 ft QNH: 1023 hPa Temperature: ISA 1 hPa: 30 ft
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