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enter the trim sheet. Check that the actual CG is inside the operational limits. If the CG is outside the
limits transfer fuel to achieve a distribution in accordance with the chart or rearrange the load.
Note: These tables are valid only when used with the following formulae for the index :
I=W×(H-arm–23.117)/1000+K or I= [(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
EXAMPLE
DATA: Fuel in left wing fuel tank = FULL
Fuel in right wing fuel tank = 5 500 kg
Fuel in center tank = 0 kg
Weight Index
Wing tank RLiegfhtt 5600 -- 12
Center tank 0 0
TOTAL 11 580 - 3
Enter the trim sheet with a fuel index of – 3
GENERAL
Applicable to: MSN,
4473
The fuel index table has been established assuming a fuel distribution in accordance with refuel
distribution (Refer to PER-LOD-FUL-A GENERAL INFORMATION - REFUELING).
If after refueling the actual distribution deviates from the chart values, the actual and the trim sheet
CG will show a discrepancy. The following tables allow to determine the fuel index taking into
account the actual fuel quantity in each tank. To determine the actual takeoff CG enter the tables
with the actual fuel quantities in each tank, read the fuel index for each tank and use their sum to
enter the trim sheet. Check that the actual CG is inside the operational limits. If the CG is outside the
limits transfer fuel to achieve a distribution in accordance with the chart or rearrange the load.
Note: These tables are valid only when used with the following formulae for the index :
I=W×(H-arm–18.85)/1000+K or I= [(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - FUEL INDEX TABLE
A318/A319/A320/A321 FLEET PER-LOD-WBA-FIT P 3/6
FCOM 19 AUG 10
EXAMPLE
DATA: Fuel in left inner fuel tank = 4 500 kg
Fuel in right inner fuel tank = 4 500 kg
Fuel in left outer fuel tank = 200 kg
Fuel in right outer fuel tank = FULL
Fuel in center tank = 0 kg
Weight Index
Inner tank RLiegfhtt 4400 -- 33
Outer tank RLiegfhtt01 + 02
Center tank 0 0
TOTAL 9 891 - 4
Enter the trim sheet with a fuel index of – 4
FUEL INDEX TABLES PER TANK
Applicable to:
Note: These tables are valid only when used with the following formulae for the index :
I=W×(H-arm–17.25)/1000+K or I=[(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
Inner Tanks Outer Tanks Center Tank
Weight Index Weight Index Weight Index
400 0 200 0 400 0
800 - 1 400 1 800 - 1
1 200 - 1 600 1 1 200 - 1
1 600 - 2 FULL 2 1 600 - 2
2 000 - 2 2 000 - 3
2 400 - 2 2 400 - 3
2 800 - 3 2 800 - 4
3 200 - 3 3 200 - 5
3 600 - 3 3 600 - 5
4 000 - 3 4 000 - 6
4 400 - 3 4 400 - 6
4 800 - 3 4 800 - 7
5 200 - 3 5 200 - 8
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - FUEL INDEX TABLE
A318/A319/A320/A321 FLEET PER-LOD-WBA-FIT P 4/6
FCOM 19 AUG 10
Continued from previous page
Inner Tanks Outer Tanks Center Tank
Weight Index Weight Index Weight Index
FULL - 2 5 600 - 8
6 000 - 9
6 400 - 10
FULL - 10
FUEL INDEX TABLES PER TANK
Applicable to: ,
, MSN,,
Note: These tables are valid only when used with the following formulae for the index :
I=W×(H-arm–23.117)/1000+K or I=[(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
Wing Tank Center Tank
Weight Index Weight Index
500 - 1 500 - 1
1 000 - 1 1 000 - 1
1 500 - 2 1 500 - 2
2 000 - 2 2 000 - 3
2 500 - 2 2 500 - 4
3 000 - 3 3 000 - 4
3 500 - 3 3 500 - 5
4 000 - 3 4 000 - 6
4 500 - 3 4 500 - 7
5 000 - 3 5 000 - 7
5 500 - 2 5 500 - 8
6 000 - 2 6 000 - 9
FULL - 1 FULL - 10
FUEL INDEX TABLES PER TANK
Applicable to: MSN,
4473
Note: These tables are valid only when used with the following formulae for the index :
I=W×(H-arm–18.85)/1000+K or I=[(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - FUEL INDEX TABLE
A318/A319/A320/A321 FLEET PER-LOD-WBA-FIT P 5/6
FCOM 19 AUG 10
Inner Tanks Outer Tanks Center Tank
Weight Index Weight Index Weight Index
500 - 1 250 1 500 - 1
1 000 - 1 500 1 1 000 - 1
1 500 - 2 FULL 2 1 500 - 2
2 000 - 2 2 000 - 3
2 500 - 2 2 500 - 3
　
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