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OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 24/38
FCOM 19 AUG 10
Applicable to:
MSN,
WING TANKS (LITERS)
(*) GRID SQUARE LETTER
(**) GRID SQUARE NUMBER
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 25/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 26/38
FCOM 19 AUG 10
(*) GRID SQUARE LETTER
(**) GRID SQUARE NUMBER
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 27/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 28/38
FCOM 19 AUG 10
(*) GRID SQUARE LETTER
(**) GRID SQUARE NUMBER
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 29/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 30/38
FCOM 19 AUG 10
(*) GRID SQUARE LETTER
(**) GRID SQUARE NUMBER
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 31/38
FCOM 19 AUG 10
Applicable to: ,
, MSN,,
WING TANKS (LITERS)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 32/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 33/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 34/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 35/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 36/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 37/38
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
Intentionally left blank
A318/A319/A320/A321 FLEET PER-LOD-FUL P 38/38
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 1/10
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
This chart allows the determination of Aircraft CG location (MAC) function of dry operating weight,
pantry adjustment, cargo loads, passengers and fuel on board.
The operational limits shown on the load and trim sheet are more restrictive than the certified limits
because error margins have been taken into account.
The load and trim sheet needs to be updated when :
a modification which changes the ‐ aircraft certified limits is included or
‐ a modification (cabin layout, cargo arrangement ...) which influences the operational limits is
made.
It is the airline responsibility to define a load and trim sheet and to keep it up to date. Refer to
PER-LOD-WBA-LTS DESCRIPTION is a description of the Load and Trim Sheet utilization (Refer to
PER-LOD-WBA-LTS LOAD AND TRIM SHEET), for a typical passenger arrangement.
Refer to customized load and trim sheet for preparing a revenue flight.
DATA
Applicable to: ,
, MSN,,
Dry Operating Weight = 49 000 kg and CG = 22 % (H-arm = 23 m)
Deviation or adjustment = + 100 kg in zone F
Cargo = 8 500 kg with the following distribution : cargo 1 = 1 000 kg ; cargo 2 = 1 000 kg ; cargo 3 =
3 000 kg ; cargo 4 = 3 000 kg ; cargo 5 = 500 kg
Passengers = 180 pax with the following distribution : cabin OA = 50 ; cabin OB = 70 ; cabin OC = 60
Fuel = 17 000 kg
DATA
Applicable to:
Dry Operating Weight = 40 500 kg and CG = 25.5 % (H-arm = 17.27 m)
Deviation or adjustment = + 100 kg in zone F
Cargo = 4 000 kg with the following distribution : cargo 1 = 1 500 kg ; cargo 4 = 2 000 kg ; cargo 5 =
500 kg
Passengers = 120 pax with the following distribution : cabin OA = 50 ; cabin OB = 70
　
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