33-06. FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
All questions: 36
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1. At 1000 UTC Shanwick Oceanic clear you to enter the Oceanic control Area at 47°00’N 008°W, 220 track miles from your current position, at time 1033 UTC. At FL200, ISA conditions and with TAS 430 kts, headwind 30 kts, FMS being unavailable, what is the required Mach number to comply with this instruction?
2. The still air distance in the climb is 189 Nautical Air Miles (NAM) and time 30 minutes. What ground distance would be covered in a 30 kts headwind?
3. (Refer to figure 033-29)
An aircraft on an extended range operation is required never to be more than 180 minutes from an alternate, based on 1 engine inoperative LRC conditions in ISA. Using the above table and a given mass of 50.000 kg at the most critical point, the maximum air distance to the relevant alternate is:
4. 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:
5. 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?
