31-01. PURPOSE OF MASS AND BALANCE CONSIDERATIONS
All questions: 54
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1. For a large aircraft where the main and nose landing gears retract forward, the effect on the CG on lowering the gear is:
2. The higher the Takeoff Mass: 1) Manoeuvrability is reduced. 2) Range will decrease but endurance will increase. 3) Gliding range will reduce. 4) Stalling speed will increase.
3. Prior to departure an aeroplane is loaded with 16.500 litres of fuel at a fuel density of 780 kg/m3. This is entered into the load sheet as 16.500 kg and calculations are carried out accordingly. As a result of this error, the aeroplane is:
4. During takeoff you notice that, fora given elevator input, the aeroplane rotates much more rapidly than expected. This is an indication that:
5. If during flight a considerable amount of fuel was transferred from the fuselage forward fuel tank to the fuselage rear tank, what effect would this have on the aircraft?