31-01. PURPOSE OF MASS AND BALANCE CONSIDERATIONS
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1. For a given configuration, the stall speed of an aeroplane will be highest when loaded:
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. The handling and performance problems encountered with a CG too far aft include:
4. Which of the following is most likely to affect the range of centre of gravity positions on an aeroplane?
5. Which of the following statements is correct?