(For this question use CAP 696 - Figure 4.14)
A revenue flight is planned for the transport aeroplane. Take-off mass is not airfield limited. The following data applies:

Dry Operating Mass 34930 kg
Performance limited landing mass 55000 kg
Fuel on board at ramp:
Taxi fuel 350 kg
Trip fuel 9730 kg
Contingency and final reserve fuel 1200 kg
Alternate fuel 1600 kg
Passengers on board 130
Standard mass for each passenger 84 kg
Baggage per passenger 14 kg
Traffic load Maximum possible

Use the loading manual provided and the above data. Determine the maximum cargo load that may be carried without exceeding the limiting aeroplane landing mass.