Given:
Dry operating mass
38000 kg
Maximum structural take-off mass
72000 kg
Maximum landing mass
65000 kg
Maximum zero fuel mass
61000 kg
Fuel burn
8000 kg
Take-off Fuel
10300 kg
The maximum allowed take-off mass and traffic load are respectively :
Given:
Dry operating mass
38000 kg
Maximum structural take-off mass
72000 kg
Maximum landing mass
65000 kg
Maximum zero fuel mass
61000 kg
Fuel burn
8000 kg
Take-off Fuel
10300 kg
The maximum allowed take-off mass and traffic load are respectively :