31-02. (H) LOADING
Всего заданий: 139
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Заданий на экзамен: 30
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1. The Basic Empty Mass of a helicopter is 5.200 kg. The operational items (including crew) is given as a mass of 270 kg. If the Takeoff Mass is 7.840 kg (including a us¬able fuel quantity of 1.220 kg) the Useful Load is:
2. The following data applies to a planned flight:
Dry Operating Mass: 34.900 kg
Performance Limited Takeoff Mass: 66.300 kg, Performance Limited Landing Mass: 55.200 kg
Maximum Zero Fuel Mass: 53.070 kg
Fuel required at ramp:
Taxi Fuel: 400 kg, Trip Fuel: 8.600 kg
Contingency Fuel: 430 kg
Alternate Fuel: 970 kg, Holding Fuel: 900 kg, Traffic Load: 16.600 kg
Fuel costs at the departure airfield are such that it is decided to load the maximum fuel quantity possible. The total fuel which may be safely loaded prior to departure is:
.
3. The Dry Operating Mass of a helicopter:
4. A helicopter is to depart at Takeoff Mass of 8.220 kg. Takeoff Fuel (including Reserve Fuel of 710 kg) is 1.750 kg. The Basic Empty Mass is 4.920 kg. Considering a To¬tal Mass of crew and operating items of 420 kg, the per¬missible Traffic Load will be:
5. Given:
Maximum Structural Takeoff Mass: 72.000 kg, Maximum Structural Landing Mass: 56.000 kg
Maximum Zero Fuel Mass: 48.000 kg
Taxi Fuel: 800 kg, Trip Fuel: 18.000 kg, Contingency Fuel: 900 kg
Alternate Fuel: 700 kg, Final Reserve Fuel: 2.000 kg
Determine the actual Takeoff Mass:
.
