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OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 18/38
FCOM 19 AUG 10
APU START/SHUTDOWN DURING REFUELING/DEFUELING
Applicable to: ALL
APU starts or shutdowns are permitted during refuel/defuel procedures. If it is necessary to operate
the APU, the limits that follow apply :
a. An APU start is not permitted during a refuel/defuel procedure if the APU has failed to start or an
automatic shutdown has occured
b. A normal APU shutdown must be completed if a fuel spill has occured during the refuel defuel
procedure.
USE OF MANUAL MAGNETIC INDICATORS (MMI)
Applicable to:
GENERAL
Indicators are disposed as follows :
• five in each wing tank, four in inner tank and one in outer tank
• one in the center tank
A/C ATTITUDE........................................................................................................................NOTE
Note the grid square letter and grid square number shown by the bubble on the attitude monitor.
ACCESS PLATFORM...................................................................................................IN POSITION
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 19/38
FCOM 19 AUG 10
Applicable to:
MSN,
GENERAL
Indicators are disposed as follows :
Indicators are disposed as follows :
• five in each wing tank, four in inner tank and one in outer tank
• one in the center tank
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 20/38
FCOM 19 AUG 10
TO DETERMINE AIRCRAFT ATTITUDE
Set ADIRS 1, 2, 3 to the NAV position.
On the LH or RH MCDU, press MCDU MENU pushbutton.
Select CFDSline key (LSK 4L).
Select SYSTEM REPORT/TEST line key (LSK 5L).
Select the line key adjacent to the FUEL indication.
On the MCDU control panel, push the NEXT PAGE key to display the FUEL Main Menu second
page.
Select the line key adjacent to the INPUT PARAMETERS VALUES indication.
Use the Table given on the next page to determine the equivalent number and letter from
PITCH and ROLL data.
Select RETURN line key (LSK 6L) until CFDS main menu appears.
Press MCDU MENU pushbutton.
PITCH REF ROLL REF
Minus 1.5 1Minus 1.5 A
Minus 1.0 2Minus 1.0 B
Minus 0.5 3Minus 0.5 C
0.0 4 0.0 D
Plus 0.5 5 Plus 0.5 E
Plus 1.0 6 Plus 1.0 F
Plus 1.5 7 Plus 1.5 G
Note: 1. This procedure can only be used if :
The PITCH and ROLL data is taken from the ADIRS ‐ (identified by an “A” after the
PITCH and ROLL title).
‐ The PITCH data displayed for the LEFT, CTR, and RIGHT is no more or less than
0.1 of each other.
‐ The ROLL data displayed for the LEFT, CTR, and RIGHT is no more or less than
0.1 of each other.
2. The FQIS input parameters are not automatically updated. Use the NEXT PAGE
control on the MCDU to cycle the pages to update the screen.
ACCESS PLATFORM...............................................................................................IN POSITION
Applicable to: ,
, MSN,,
GENERAL
Indicators are disposed as follows :
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 21/38
FCOM 19 AUG 10
Indicators are disposed as follows :
• seven in each wing tank,
• one in the center tank
TO DETERMINE AIRCRAFT ATTITUDE
Set ADIRS 1, 2, 3 to the NAV position.
On the LH or RH MCDU, press MCDU MENU pushbutton.
Select CFDSline key (LSK 4L).
Select SYSTEM REPORT/TEST line key (LSK 5L).
Select the line key adjacent to the FUEL indication.
On the MCDU control panel, push the NEXT PAGE key to display the FUEL Main Menu second
page.
Select the line key adjacent to the INPUT PARAMETERS VALUES indication.
Use the Table given on the next page to determine the equivalent number and letter from
PITCH and ROLL data.
Select RETURN line key (LSK 6L) until CFDS main menu appears.
Press MCDU MENU pushbutton.
PITCH REF ROLL REF
Minus 1.5 1Minus 1.5 A
Minus 1.0 2Minus 1.0 B
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 22/38
FCOM 19 AUG 10
Continued from previous page
PITCH REF ROLL REF
Minus 0.5 3Minus 0.5 C
0.0 4 0.0 D
Plus 0.5 5 Plus 0.5 E
Plus 1.0 6 Plus 1.0 F
Plus 1.5 7 Plus 1.5 G
　
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