31-04. MASS AND BALANCE DETAILS OF AIRCRAFT
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1. What are the limits for the CG as a percentage of the aircraft’s MAC at its maximum Takeoff Mass?
2. Longitudinal CG location is normally expressed:
3. An aircraft that is not within a fleet mass evaluation program must be weighed:
4. Referring to the Loading Manual for the transport aeroplane, the maximum running load for the aft section of the forward lower deck cargo compartment is:
5. The centre of gravity of an aeroplane is at 25% of the Mean Aerodynamic Chord. This means that the centre of gravity of the aeroplane is situated at 25% of the length of:
