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For the given air distance, the optimum fuel tankering weight is 62 000 kg, which is lower than the
ok􀁄mmdc􀀃s􀁄􀁎dnee􀀃vdhfgs􀀃→􀀃mn􀀃etdk􀀃s􀁄m􀁎dqhmf􀀃qdbnlldmcdc􀀑
2. Fuel price ratio = 0.928
Cruising Altitude = FL 350
Planned TOW = 60 000 kg (mission weight without fuel tankering)
Air Distance = 1 625 nm
Enter graph Refer to PER-FPL-FLP-FTK FL350.
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 2/76
FCOM 19 AUG 10
For the given air distance, the optimum fuel tankering weight is 67 000 kg, which is 7 000 kg
higher than the planned takeoff weight →􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃6􀀃///􀀃􀁎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 = 0.940
Cruising Altitude = FL 390
Planned TOW = 60 000 kg (mission weight without fuel tankering)
Air Distance = 625 nm
Enter graph Refer to PER-FPL-FLP-FTK FL390.
Interpolate for the air distance of 625 nm between the borderline and 750 nm.
For the given air distance, the optimum fuel tankering weight is 70 000 kg, which is 10 000 kg
higher than the planned takeoff weight →􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃0/􀀃///􀀃􀁎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
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 64 200 kg, which is lower than the
planned takeoff weight →􀀃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 69 500 kg, which is 9 500 kg
ghfgdq􀀃sg􀁄m􀀃sgd􀀃ok􀁄mmdc􀀃s􀁄􀁎dnee􀀃vdhfgs􀀃→􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃8􀀃4//􀀃􀁎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 3/76
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
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 61 000 kg, which is 1 000 kg
ghfgdq􀀃sg􀁄m􀀃sgd􀀃ok􀁄mmdc􀀃s􀁄􀁎dnee􀀃vdhfgs􀀃→􀀃noshltl􀀃pt􀁄mshsx􀀃ne􀀃dwsq􀁄􀀃etdk􀀃hr􀀃0􀀃///􀀃􀁎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
EXAMPLES
Applicable to: MSN,
1. Fuel price ratio = 0.948
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 58 000 kg, which is lower than the
planned takeoff weight →􀀃mn􀀃etdk􀀃s􀁄m􀁎dqhmf􀀃qdbnlldmcdc􀀑
2. Fuel price ratio = 0.942
Cruising Altitude = FL 350
Planned TOW = 62 000 kg (mission weight without fuel tankering)
　
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