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EFFECTIVITY 28-12-00 Page 3
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 91
ALL
TANK AND VENTING SYSTEM COMPONENTS
CLACK VALVE
IDENTIFICATION
FIN: None
LOCATION
ZONE: 540, 640
COMPONENT DESCRIPTION
Ribs 1 and 2 form a Collector Box around the wing tank
fuel pumps.
Clack valves at the bottom of rib 2 permit fuel to
enter the box but prevent it draining out again.
This ensures a fuel supply at the pumps during wing
down manoeuvres.
TMUFUEJ01-T02 LEVEL 3
EFFECTIVITY 28-12-00 Page 4
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 92
ALL
TMUFUEJ01-P02 LEVEL 3
TANK AND VENTING SYSTEM COMPONENTS - CLACK VALVE
EFFECTIVITY 28-12-00 Page 5
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 93
ALL
TANK AND VENTING SYSTEM COMPONENTS
CAP/ADAPTER GRAVITY FILL
IDENTIFICATION
FIN: 42QM, 43QM, 44QM, 45QM
LOCATION
ZONE: 540, 640
COMPONENT DESCRIPTION
An overwing gravity fill cap/adapter is installed in
the top surface of each wing tank, giving direct access
to the outer cell.
The cap is removed by lifting the hinged handle, set
flush in the top of the cap, and turning to unlock.
NOTE: Before gravity refuelling make sure that
transfer valves are open.
TMUFUEJ01-T03 LEVEL 3
EFFECTIVITY 28-12-00 Page 6
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 94
ALL
TMUFUEJ01-P03 LEVEL 3
TANK AND VENTING SYSTEM COMPONENTS - CAP/ADAPTER GRAVITY FILL
EFFECTIVITY 28-12-00 Page 7
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 95
ALL
TANK AND VENTING SYSTEM COMPONENTS
OVERPRESSURE PROTECTOR
IDENTIFICATION
FIN: 46QM, 47QM, 102QM, 103QM, (96QM)
LOCATION
ZONE: 540, 640, (147)
TMUFUEJ01-T04 LEVEL 3
EFFECTIVITY 28-12-00 Page 8
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 96
ALL
TMUFUEJ01-P04 LEVEL 3
TANK AND VENTING SYSTEM COMPONENTS - OVERPRESSURE PROTECTOR
EFFECTIVITY 28-12-00 Page 9
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 97
ALL
TANK AND VENTING SYSTEM COMPONENTS
FUEL VENT PROTECTOR
IDENTIFICATION
FIN: 48QM, 49QM
LOCATION
ZONE: 550, 650
COMPONENT DESCRIPTION
Vent protector consists of:
- ice protector
- flame arrestor
Ice protector prevents freezing of the flame arrestor
during descent. Flame arrestor reduces the risk of
ground fire igniting the fuel tank.
TMUFUEJ01-T05 LEVEL 3
EFFECTIVITY 28-12-00 Page 10
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 98
ALL
TMUFUEJ01-P05 LEVEL 3
TANK AND VENTING SYSTEM COMPONENTS - FUEL VENT PROTECTOR
EFFECTIVITY 28-12-00 Page 11
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 99
ALL
TANK AND VENTING SYSTEM COMPONENTS
FLOAT VENT VALVE
IDENTIFICATION
FIN: 15QM, 16QM, 17QM, 18QM
LOCATION
ZONE: 540, 640
COMPONENT DESCRIPTION
A float operated arm opens or closes this valve
depending upon the fuel level, to permit air to be
vented.
Valve also opens when:
- inward pressure differential is 0.5 psig
(0.0345 bar) with a full tank.
- outward pressure differential is 1 psig
(0.69 bar) with fuel level below float.
TMUFUEJ01-T06 LEVEL 3
EFFECTIVITY 28-12-00 Page 12
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 100
ALL
TANK AND VENTING SYSTEM COMPONENTS - FLOAT VENT VALVE
TMUFUEJ01-P06 LEVEL 3
EFFECTIVITY 28-12-00 Page 13
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
　
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