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(11).
j. Check if the intersection point is within the Zero Fuel Weight operational limits, if not rearrange
cargo loading.
k. Read in table (13) the fuel index correction : – 2 and carry forward in fuel scale (14).
l. From this point draw a vertical line which intersects (16) the takeoff weight horizontal line (15).
m. Check if the intersection point is within the Takeoff Weight operational limits.
n. Read zero fuel weight and CG position : 32.7 % and fill in table (17).
o. Read takeoff CG position : 30.5 % and fill in table (18).
CAUTION If there is no customized trim sheet for your airline in this section, do not use the
information enclosed herein for day to day operation as margins and load CG vary
with cabin and cargo layout.
Note: When referring to CG lower than 27 %, an operational margin is taken into account. It is the
reason why performance at forward CG (lower than 25 %) must be used for operational CG
lower than 27 %.
LOAD AND TRIM SHEET
Applicable to: ,
, MSN,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 5/10
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 6/10
FCOM 19 AUG 10
LOAD AND TRIM SHEET
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 7/10
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 8/10
FCOM 19 AUG 10
LOAD AND TRIM SHEET
Applicable to: MSN,
4473
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 9/10
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
Intentionally left blank
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 10/10
FCOM 19 AUG 10
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 1/6
FCOM 19 AUG 10
GENERAL
Applicable to:
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–17.25)/1000+K or I= [(CG–25)×W×0.000042]+K
(Weight in kg, H-arm in m)
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
GENERAL
Applicable to: ,
, MSN,,
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).
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 2/6
FCOM 19 AUG 10
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
　
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