31-02. (H) LOADING
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1. Given:
Maximum Structural Takeoff Mass: 146.900 kg, Maximum Structural Landing Mass: 93.800 kg
Maximum Zero Fuel Mass: 86.400 kg
Trip Fuel: 27.500 kg, Block Fuel: 35.500 kg
Engine starting and taxi fuel: 1.000 kg
The Maximum Takeoff Mass is equal to:
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2. The Takeoff Mass of a helicopter is 8.420 kg which in¬cludes a Traffic Load of 1.640 kg and a usable fuel load of 1.150 kg. If the standard mass for the crew is 270 kg the Dry Operating Mass is:
3. What mass has to be entered in the loading chart for aviation fuel if 170 I may be refuelled? (Fuel density = 0,78 kg/I)
4. The responsibility for determination of the mass of OPERATING MASSES and CREW MEMBERS included within the Dry Operating Mass lies with:
5. An aircraft has a Dry Operating Mass of 37.400 kg. The Performance Limited Takeoff Mass is 67.400 kg and the Performance Limited Landing Mass 52.800 kg. The Certificate of Airworthiness Maximum Structural Takeoff Mass is 66.000 kg, the Maximum Structural Landing Mass is 54.000 kg and the Maximum Zero Fuel Mass is 52.000 kg. The fuel load before taxi is 16.000 kg. Allowing 500 kg for start, taxi and takeoff and 12.400 kg for Trip Fuel, the maximum allowed Traffic Load is:
