31-04. MASS AND BALANCE DETAILS OF AIRCRAFT
All questions: 63
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1. From the manual for the single engine piston/propeller
aeroplane, the maximum floor loading is:

2. For the light twin engine piston propeller aeroplane the datum is located:
3. What is the centre of gravity position of the aircraft in the diagram, given:
Left main: 1.620 kg
Right main: 1.632 kg
Nose: 640 kg

4. An aeroplane must be re-weighed at certain intervals. Where an operator uses fleet masses and provided that changes have been correctly documented, this interval is:
5. The determination of the centre of gravity in relation to the Mean Aerodynamic Chord: