33-06. FLIGHT MONITORING AND IN-FLIGHT RE-PLANNING
All questions: 36
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Questions for exams: 30
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1. (Refer to figure 033-29)
For the purpose of planning an extended range flight it is required that with a start of diversion mass of 55.000 kg a diversion of 600 nautical miles should be achieved in 90 minutes. Using the above table, the only listed cruise technique to meet that requirement is:
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. 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?
4. Minimum planned takeoff fuel is 160 kg (30% total reserve fuel is included). Assume the groundspeed on this trip is constant. When the aeroplane has done half the distance the remaining fuel is 70 kg. Is diversion to a nearby alternate necessary?
5. (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:
