Test 10 Questions ATPL - Airline Transport Pilot license - Flight Planning and Monitoring, no time limit

1 - Find: Air distance in Nautical Air Miles (NAM) for this leg and fuel consumptionGiven: Flight time from top of climb at FL 280 to the enroute point is 48 minutes. Cruise procedure is long range cruise. Temperature is ISA -5°C. The take-off mass is 56000 kg and climb fuel 1100 kg.
2 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Give the name and frequency of the Flight Information Service for an aeroplane in position (47°59'N, 010°14'E) at 5000'.
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3 - A sector distance is 450 NM long. The TAS is 460 kt. The wind component is 50 kt tailwind. What is the still air distance?
4 - Find the SHORT DISTANCE CRUISE ALTITUDE for the twin jet aeroplane.Given: Brake release mass=45000 kg, Temperature=ISA + 20°C, Trip distance=50 Nautical Air Miles (NAM)
5 - The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5 350 kg. Fuel consumption in holding mode is 6 000 kg/h. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4 380 kg. The destination aerodrome has a single runway. What is the minimum quantity of fuel which should be on board at take-off?
6 - Given:X = Distance A to point of equal time (PET) between A and B E = EnduranceD = Distance A to B O = Groundspeed 'on'H = Groundspeed 'back'The formula for calculating the distance X to point of equal time (PET) is:
7 - The purpose of the decision point procedure is:
8 - When completing Item 9 of the ATC flight plan, if there is no appropriate aircraft designator, the following should be entered:
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9 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W ?
10 - Given: maximum allowable take-off mass 64400 kg maximum landing mass 56200 kgmaximum zero fuel mass 53000 kg dry operating mass 35500 kg estimated load 14500 kg estimated trip fuel 4900kg minimum take-off fuel 7400 kgFind the maximum allowable take-off fuel: