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Check :
a. new TOW less than or equal to MTOW from departure airport ;
b. total fuel to be loaded less than or equal to maximum fuel capacity ;
c. MLW at destination
3. Fuel price ratio = 0.914
Cruising Altitude = FL 390
Planned TOW = 60 000 kg (mission weight without fuel tankering)
Air Distance = 1 125 nm
Enter graph Refer to PER-FPL-FLP-FTK FL390.
Interpolate for the air distance of 1 125 nm between the borderline and 1 250 nm. For the given
air distance, the optimum fuel tankering weight is 68 000 kg, which is 8 000 kg higher than the
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - FUEL TANKERING
A318/A319/A320/A321 FLEET PER-FPL-FLP-FTK P 6/76
FCOM 19 AUG 10
Check :
a. new TOW less than or equal to MTOW from departure airport ;
b. total fuel to be loaded less than or equal to maximum fuel capacity ;
c. MLW at destination
EXAMPLES
Applicable to:
1. Fuel price ratio = 0.942
Cruising Altitude = FL 310
Planned TOW = 66 000 kg (mission weight without fuel tankering)
Air Distance = 1 750 nm
Enter graph on Refer to PER-FPL-FLP-FTK FL310.
For the given air distance, the optimum fuel tankering weight is 65 000 kg, which is lower than the
planned takeoff wehfgs􀀃→􀀃mn􀀃etdk􀀃s􀁄m􀁎dqhmf􀀃qdbnlldmcdc􀀑
2. Fuel price ratio = 0.930
Cruising Altitude = FL 350
Planned TOW = 60 000 kg (mission weight without fuel tankering)
Air Distance = 1 250 nm
Enter graph Refer to PER-FPL-FLP-FTK FL350.
For the given air distance, the optimum fuel tankering weight is 69 000 kg, which is 9 000 kg
ghfgdq􀀃sg􀁄m􀀃sgd􀀃ok􀁄mmdc􀀃s􀁄􀁎dnee􀀃vdhfgs􀀃→􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃8􀀃///􀀃􀁎f􀀑
Check :
a. new TOW less than or equal to MTOW from departure airport ;
b. total fuel to be loaded less than or equal to maximum fuel capacity ;
c. MLW at destination
3. Fuel price ratio = 0.902
Cruising Altitude = FL 390
Planned TOW = 60 000 kg (mission weight without fuel tankering)
Air Distance = 1 375 nm
Enter graph Refer to PER-FPL-FLP-FTK FL390.
Interpolate for the air distance of 1 375 nm between 1 250 nm and 1 500 nm.
For the given air distance, the optimum fuel tankering weight is 63 200 kg, which is 3 200 kg
ghfgdq􀀃sg􀁄m􀀃sgd􀀃ok􀁄mmdc􀀃s􀁄􀁎dnee􀀃vdhfgs􀀃→􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃2􀀃1//􀀃􀁎f􀀑
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - FUEL TANKERING
A318/A319/A320/A321 FLEET PER-FPL-FLP-FTK P 7/76
FCOM 19 AUG 10
Check :
a. new TOW less than or equal to MTOW from departure airport ;
b. total fuel to be loaded less than or equal to maximum fuel capacity ;
c. MLW at destination
EXAMPLES
Applicable to:
1. Fuel price ratio = 0.942
Cruising Altitude = FL 310
Planned TOW = 64 000 kg (mission weight without fuel tankering)
Air Distance = 2 250 nm
Enter graph on Refer to PER-FPL-FLP-FTK FL310.
For the given air distance, the optimum fuel tankering weight is 60 000 kg, which is lower than the
planned takeoff􀀃vdhfgs􀀃→􀀃mn􀀃etdk􀀃s􀁄m􀁎dqhmf􀀃qdbnlldmcdc􀀑
2. Fuel price ratio = 0.914
Cruising Altitude = FL 350
Planned TOW = 62 000 kg (mission weight without fuel tankering)
Air Distance = 1 500 nm
Enter graph Refer to PER-FPL-FLP-FTK FL350.
For the given air distance, the optimum fuel tankering weight is 70 000 kg, which is 8 000 kg
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