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UF94200
EFFECTIVITY Page 226
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - CTR TK PRESSURE RELIEF VALVE
TMUFUEM01-P04 LEVEL 3
EFFECTIVITY 28-25-00 Page 9
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 227
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
SPILL PIPE CHECK VALVE
IDENTIFICATION
FIN: 54QM, 55QM
LOCATION:
ZONE: 540, 640
COMPONENT DESCRIPTION
A check valve is installed in each spill pipe.
This sphincter-type valve allows fuel in the spill
pipe to drain through it into the tank but does not
permit reverse flow.
TMUFUEM01-T05 LEVEL 3
EFFECTIVITY 28-25-00 Page 10
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 228
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - SPILL PIPE CHECK VALVE
TMUFUEM01-P05 LEVEL 3
EFFECTIVITY 28-25-00 Page 11
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 229
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
REFUEL VALVE
IDENTIFICATION
FIN: 7QU, 10QU, 8QU
LOCATION:
ZONE: 520, 620, 148
TMUFUEM01-T06 LEVEL 3
EFFECTIVITY 28-25-00 Page 12
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 230
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - REFUEL VALVE
TMUFUEM01-P06 LEVEL 3
EFFECTIVITY 28-25-00 Page 13
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 231
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
REFUEL VALVE CANISTER
IDENTIFICATION
FIN: 19QM, 20QM, 88QM
LOCATION:
ZONE: 540, 640, 148
COMPONENT DESCRIPTION
The valve assembly may be removed from the canister
without loss of fuel.
TMUFUEM01-T07 LEVEL 3
EFFECTIVITY 28-25-00 Page 14
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 232
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - REFUEL VALVE CANISTER
TMUFUEM01-P07 LEVEL 3
EFFECTIVITY 28-25-00 Page 15
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 233
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
DEFUEL/TRANSFER VALVE
IDENTIFICATION
FIN: 11QM
LOCATION:
ZONE: 142
COMPONENT DESCRIPTION
When open, the defuel/transfer valve connects the
refuel pipeline to the engine supply line when
defuelling or transferring from tank to tank.
TMUFUEM01-T08 LEVEL 3
EFFECTIVITY 28-25-00 Page 16
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 234
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - DEFUEL/TRANSFER VALVE
TMUFUEM01-P08 LEVEL 3
EFFECTIVITY 28-25-00 Page 17
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 235
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
DEFUEL/TRANSFER VALVE ACTUATOR
IDENTIFICATION
FIN: 11QU
LOCATION:
ZONE: 148
COMPONENT DESCRIPTION
The actuator (11GV) is secured to its mounting by a
"V" band clamp.
TMUFUEM01-T09 LEVEL 3
EFFECTIVITY 28-25-00 Page 18
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 236
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS - DEFUEL/TRANSFER VALVE ACTUATOR
TMUFUEM01-P09 LEVEL 3
EFFECTIVITY 28-25-00 Page 19
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 237
ALL
REFUEL AND DEFUEL SYSTEM COMPONENTS
AIR INLET VALVE
IDENTIFICATION
FIN: None
LOCATION:
ZONE: 520, 620
COMPONENT DESCRIPTION
The air inlet valve admits air into the refuel line,
so that the line may drain.
TMUFUEM01-T10 LEVEL 3
EFFECTIVITY 28-25-00 Page 20
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
　
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