5.11 Manual Planning Fuel Calculations

Fuel Calculation

ROUTE Departure Destination Alternate
  YYZ YUL YOW
Planned Altitude 150 6000
Temperature STD M4 STD
TAS 245  
Wind Component P20K M10K
Ground Speed 265  
Distance 390 90
Time 1:30 :20
Fuel Burn  7500 2500
Additional fuel for (ATC etc.)   1000
Reserve   2200
Max Landing Weight 50000  
Calculated Max Take off Weight = burn + MLW 57500  
Total FOD   5700
Minimum Fuel Required = burn + FOD 13200  
Max Take off Weight 57500  
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