The total mass of an aeroplane is 145000 kg and the centre of gravity limits are between 4.7 m and 6.9 m aft of the datum. The loaded centre of gravity position is 4.4 m aft. How much mass must be transferred from the front to the rear hold in order to bring the out of limit centre of gravity position to the foremost limit:4
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Given the following data how much cargo must be moved from the forward hold to the aft hold to achieve a CG at 33% MAC?AUM 200000kgForward Hold Cargo 6500kg Aft hold Cargo 4000kg Distance between holds 10m Current CG: 30%MACMAC 4.6m4
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Given:Maximum structural take-off mass: 7400 kg Maximum structural landing mass: 7400 kg Zero Fuel Mass: 5990 kgTaxi Fuel: 15 kg Contingency Fuel: 110 kg Alternate Fuel: 275 kg Final Reserve Fuel: 250 kg Trip Fuel: 760 kgThe expected Landing Mass at destination will be:4
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Traffic load is the difference between:4
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The Basic Empty Mass is 4960 kg, the Dry Operating Mass is 5220 kg and the Zero Fuel Mass is 6040 kg.If the take-off mass is 7630 kg the useful load is4
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Basic Empty Mass is:4
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Given the following data calculate the CG as a %MAC when 12000N of last minute cargo is added to a hold 10m from the datum:AUM 460000NLEMac 14m from datum MAC 4.6mCurrent CG 15.4m from datum4
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The mass of an item multiplied by it's distance from the datum is it's4
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The maximum quantity of fuel that can be loaded into an aircraft's tanks is given as 400 US Gallons.If the fuel density (specific gravity) is given as 0.79 the mass of fuel which may be loaded is:4
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