33-06. (H) FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
All questions: 23
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Questions for exams: 15
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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 sector distance is 450 NM long. The TAS is 460 kts. The wind component is 50 kts tailwind. What is the still air distance?
3. During a flight at night a position has to be reported to ATC. The aeroplane is at a distance of 750 NM from the ground station and at flight level 350. The frequency to be used is:
4. In the cruise at FL155 at 260 kts TAS, the pilot plans for a 500 ft/min descent in order to fly overhead MAN VOR at 2.000 feet (QNH 1030). TAS will remain constant during descent, wind is negligible, temperature is standard. The pilot must start the descent at a distance from MAN of:
5. A descent is planned from FL340 ft so as to arrive at FL100 at a distance 6 NM from a VORTAC. With a GS of 280 kts and a rate of descent of 1.200 ft/min. The distance from the VORTAC when descent is started is:
