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- remove attachment bolts
- use extractor screws in removal holes
- drain it
- turn the pump
- pull it out
TMUFUEK01-T07 LEVEL 3
EFFECTIVITY 28-20-00 Page 14
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 140
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS - WING TANK FUEL PUMP REMOVAL INFORMATION
TMUFUEK01-P07 LEVEL 3
EFFECTIVITY 28-20-00 Page 15
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 141
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS
SCAVENGE JET PUMP
IDENTIFICATION
FIN: 66QM to 69QM, 89QM, 90QM
LOCATION
ZONE: 540, 640, 141, 142
COMPONENT DESCRIPTION
The Jet pump has:
- a venturi type passage
- a non-return valve
- ports for pipe connection
- an attachment plate with studs
TMUFUEK01-T08 LEVEL 3
EFFECTIVITY 28-20-00 Page 16
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 142
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS - SCAVENGE JET PUMP
TMUFUEK01-P08 LEVEL 3
EFFECTIVITY 28-20-00 Page 17
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 143
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS
TRANSFER VALVE
IDENTIFICATION
FIN: 27QM, 28QM, 29QM, 30QM
LOCATION
ZONE: 540, 640
COMPONENT DESCRIPTION
Each valve consists of a cast light alloy body housing
a spherical plug.
TMUFUEK01-T09 LEVEL 3
EFFECTIVITY 28-20-00 Page 18
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 144
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS - TRANSFER VALVE
TMUFUEK01-P09 LEVEL 3
EFFECTIVITY 28-20-00 Page 19
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 145
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS
TRANSFER VALVE DRIVE
IDENTIFICATION
FIN: 70QM, 71QM, 72QM, 73QM
LOCATION
ZONE: 540, 640
COMPONENT DESCRIPTION
The drive shaft has 2 universal joints. It is keyed
at one end for engagement with the actuator and splined
at the other end for engagement with the valves.
TMUFUEK01-T10 LEVEL 3
EFFECTIVITY 28-20-00 Page 20
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 146
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS - TRANSFER VALVE DRIVE
TMUFUEK01-P10 LEVEL 3
EFFECTIVITY 28-20-00 Page 21
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 147
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS
TRANSFER VALVE ACTUATOR
IDENTIFICATION
FIN: 9QP, 10QP, 11QP, 12QP
LOCATION
ZONE: 520, 620, 570, 670
COMPONENT DESCRIPTION
MECHANICAL INDICATOR: shows valve open or closed.
TMUFUEK01-T11 LEVEL 3
EFFECTIVITY 28-20-00 Page 22
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 148
ALL
MAIN FUEL PUMP SYSTEM COMPONENTS - TRANSFER VALVE ACTUATOR
TMUFUEK01-P11 LEVEL 3
EFFECTIVITY 28-20-00 Page 23
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 149
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFUEK01 LEVEL 3
EFFECTIVITY 28-20-00 Page 24
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 150
ALL
28 - FUEL SYSTEM
28-20-00 ENGINE AND APU COMPONENTS
CONTENTS:
Pressure Holding Valve (recirculation)
Check Valve (recirculation)
Crossfeed Valve
Crossfeed Valve Actuator
Engine LP Fuel Valve
Engine LP Fuel Valve Actuator
APU Fuel Pressure Switch
APU Fuel Pump
APU Fuel Pump Canister
APU Fuel LP Valve
APU Fuel LP Valve Actuator
TMUFUEL01 LEVEL 3
EFFECTIVITY 28-20-00 Page 1
Apr 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
　
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