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Air Distance = 1 000 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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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 = 0.888
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 4/76
FCOM 19 AUG 10
Cruising Altitude = FL 390
Planned TOW = 63 000 kg (mission weight without fuel tankering)
Air Distance = 1 625 nm
Enter graph Refer to PER-FPL-FLP-FTK FL390.
Interpolate for the air distance of 1 625 nm between the borderline and 1 750 nm.
For the given air distance, the optimum fuel tankering weight is 67 000 kg, which is 4 000 kg
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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
EXAMPLES
Applicable to:
1. Fuel price ratio = 0.944
Cruising Altitude = FL 310
Planned TOW = 68 000 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 64 000 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 69 000 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.
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 5/76
FCOM 19 AUG 10
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 63 500 kg, which is 3 500 kg higher than the
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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
EXAMPLES
Applicable to: ,
, MSN
1. Fuel price ratio = 0.950
Cruising Altitude = FL 310
Planned TOW = 70 000 kg (mission weight without fuel tankering)
Air Distance = 1 500 nm
Enter graph on Refer to PER-FPL-FLP-FTK FL310.
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 = 0.926
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.
For the given air distance, the optimum fuel tankering weight is 66 000 kg, which is 6 000 kg
　
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