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Note: 1. This procedure can only be used if :
The PITCH and ROLL data is taken from the ‐ ADIRS ( Make sure that the FQIS
Status page does not show "NO DATA FROM ADIRU 1" and "NO DATA FROM
ADIRU 2").
‐ 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 every 5.50 s
ACCESS PLATFORM...............................................................................................IN POSITION
Applicable to:
MSN,
TO DETERMINE FUEL QUANTITY IN THE OUTER TANK
MMI number 5.........................................................................................UNLOCK and WITHDRAW
The crewmember must withdraw the MMI slowly until he feels the magnetic attraction between the
rod and float magnets.
Do not use force when withdrawing the MMI as this will disengage the float magnet from the rod
magnet and bring the rod down onto the mechanical stop.
ROD GRADUATION (which aligns with bottom wing surface).................................................READ
MMI............................................................................................................. IN PLACE and LOCKED
Use the table for the applicable aircraft wing side, aircraft attitude (grid square letter and number),
and the MMI stick number 5, to find the volume of fuel in the outer tank (See below).
Multiply the result by the specific gravity to find the fuel weight.
Applicable to: ,
, MSN,,
MMI (from number 7 to number 1)..............................................................UNLOCK and WITHDRAW
The crewmember must slowly withdraw the MMI, until magnetic attraction is felt between the rod and
float magnets.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
FUEL
A318/A319/A320/A321 FLEET PER-LOD-FUL P 23/38
FCOM 19 AUG 10
Do not use force when withdrawing the MMI, as this will disengage the float magnet from the rod
magnet, and bring the rod down on to the mechanical stop.
ROD GRADUATION (which aligns with bottom wing surface).....................................................READ
MMI................................................................................................................. IN PLACE and LOCKED
Enter the table for the applicable aircraft wing side, aircraft attitude (grid square letter and number),
and the applicable MMI stick number, to find the volume of fuel in the wing tank (See below).
Multiply the result by the specific gravity to find the fuel weight.
Applicable to:
MSN,
TO DETERMINE FUEL QUANTITY IN THE INNER TANK
MMI (from number 4 to number 1)..........................................................UNLOCK and WITHDRAW
The crewmember must withdraw the MMI slowly until he feels the magnetic attraction between the
rod and float magnets.
Do not use force when withdrawing the MMI as this will disengage the float magnet from the rod
magnet and bring the rod down onto the mechanical stop.
ROD GRADUATION (which aligns with bottom wing surface).................................................READ
MMI............................................................................................................. IN PLACE and LOCKED
MMIs shall be withdrawn from number 4 to number 1 until one MMI measures fuel.
Use the table for the applicable aircraft wing side, aircraft attitude (grid square letter and number),
and the applicable MMI stick number to find the volume of fuel in the inner tank (Refer to
PER-LOD-FUL-C USE OF MANUAL MAGNETIC INDICATORS (MMI) - WING TANKS (LITERS)).
Multiply the result by the specific gravity to find the fuel weight.
Applicable to: ALL
CENTER TANK MMI...................................................................................UNLOCK and WITHDRAW
The crewmember must withdraw the MMI slowly until he feels the magnetic attraction between the
rod and float magnets.
Do not use force when withdrawing the MMI as this will disengage the float magnet from the rod
magnet and bring the rod down onto the mechanical stop.
ROD GRADUATION (which aligns with bottom wing surface).....................................................READ
MMI................................................................................................................. IN PLACE and LOCKED
Use the table for the center tank, and for the applicable aircraft attitude (grid square letter and
number) to find the volume of fuel in the center tank (See below).
Multiply the result by the specific gravity to find the fuel weight.
A318/A319/A320/A321 FLIGHT CREW
　
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