(Refer to figures 033_209A, 033_209B)
Assuming a departure/destination fuel price ratio of 0.91, the commander decides to optimize fuel tankering by using the following data:
Cruise flight level: FL 350
Air distance to be covered: 2 500 NM
Planned take-off mass: 200 000 Kg (with the minimum prescribed fuel quantity of 38 000 Kg that includes a trip fuel of 29 000 Kg)
Maximum landing mass: 180 000 Kg
Maximum take-off mass: 205 000 Kg
Maximum tank capacity: 40 000 Kg
The additional fuel quantity will be:
|
| A. |
0 Kg
|
| B. |
3 000 Kg
|
| C. |
2 000 Kg
|
| D. |
5 000 Kg
|
|
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