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UF94200
EFFECTIVITY Page 2
ALL
SYSTEM DESIGN PHILOSOPHY
TMUFUE001-P01 LEVEL 1
EFFECTIVITY 28-00-00 Page 3
Aug 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 3
ALL
SELF EXAMINATION
Which tanks are the main supply tanks?
A - Center tank and inner cells.
B - Center Tank.
C - Outer Cells.
The Fuel Quantity Indicating System comprises...
A - Two FQICs and two FLSCUs.
B - One FQIC and two FLSCUs.
C - One FQIC and one FLSCU.
TMUFUE001 LEVEL 1
EFFECTIVITY 28-00-00 Page 4
Aug 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 4
ALL
28 - FUEL SYSTEM
28-11-00 TANK USABLE CAPACITIES
CONTENTS:
Wing Tanks
Center Tank
Vent Surge Tanks
Self Examination
TMUFUE201 LEVEL 1
EFFECTIVITY 28-11-00 Page 1
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 5
ALL
TANK USABLE CAPACITIES
WING TANKS
Fuel is carried in three tanks: the left hand wing
tank, the right hand wing tank and the center tank.
Each wing tank is divided into two cells, the outer
cell and the inner cell.
TMUFUE201-T01 LEVEL 1
EFFECTIVITY 28-11-00 Page 2
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 6
ALL
TMUFUE201-P01 LEVEL 1
TANK USABLE CAPACITIES - WING TANKS
EFFECTIVITY 28-11-00 Page 3
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 7
ALL
TANK USABLE CAPACITIES
CENTER TANK
VENT SURGE TANKS
A vent surge tank is positioned in the outer section
of each wing.
Each fuel tank, when normally full, has two percent
additional space for expansion without spillage into
the vent surge tank.
TMUFUE201-T02 LEVEL 1
EFFECTIVITY 28-11-00 Page 4
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 8
ALL
TANK USABLE CAPACITIES
TMUFUE201-P02 LEVEL 1
EFFECTIVITY 28-11-00 Page 5
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 9
ALL
SELF EXAMINATION
What is the maximum total fuel capacity?
A - 41291 LBS (18729 KG)
B - 45920 LBS (20866 KG)
C - 52174 LBS (23707 KG)
TMUFUE201 LEVEL 1
EFFECTIVITY 28-11-00 Page 6
JUL 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 10
ALL
28 - FUEL SYSTEM
28-20-00 ENGINE AND APU FUEL FEED
PRESENTATION
CONTENTS:
Pumps
Sequence Valves
Crossfeed Valve
LP Valves
Pressure Switches
APU Pump
Transfer Valves
Air Release Valve
Self Examination
TMUFUE101 LEVEL 1
EFFECTIVITY 28-20-00 Page 1
Jul 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 11
ALL
ENGINE AND APU FUEL FEED PRESENTATION
PUMPS
Each main tank has 2 centrifugal booster pumps capable
of supplying the engines with fuel at the required
pressure and flow rate.
There are 2 pumps per tank.
The wing tank pumps run continuously during normal
operation.
SEQUENCE VALVES
Pressure relief sequence valves on the wing tank pumps
give priority to center tank pump supply.
The sequence valves give priority by limiting wing
tank pumps output pressure.
CROSSFEED VALVE
A CROSSFEED VALVE permits connection of the left and
right engine supply lines.
The crossfeed valve is normally closed.
LP VALVES
The Low Pressure valves isolate the engines or APU
from the fuel supply.
The LP valve is open when the related engine or APU
is running; it closes when engine or APU is shut down
or when FIRE pushbutton is released out.
PRESSURE SWITCHES
A pressure switch for each pump monitors the pump
pressure for the low pressure warning.
APU PUMP
A specific fuel pump supplies the APU if the tank pumps
are not operating. This pump takes fuel from the left
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ATA 28 FUEL SYSTEM(2)
