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MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 264
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - CADENSICON SENSOR
TMUFUEN01-P02 LEVEL 3
EFFECTIVITY 28-42-00 Page 5
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 265
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
FUEL QUANTITY PRESELECTOR
IDENTIFICATION
FIN: 5QT
LOCATION
ZONE: 192
COMPONENT DESCRIPTION
Each LED display presents fuel quantity in kg x 1000.
The PRESELECTOR has self contained BITE operations
which are controlled by the FQI Computer, by data
supplied through the Arinc 429 data bus link.
TMUFUEN01-T03 LEVEL 3
EFFECTIVITY 28-42-00 Page 6
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 266
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - FUEL QUANTITY PRESELECTOR
TMUFUEN01-P03 LEVEL 3
EFFECTIVITY 28-42-00 Page 7
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 267
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
MULTI-TANK INDICATOR
IDENTIFICATION
FIN: 6QT
LOCATION
ZONE: 192
COMPONENT DESCRIPTION
Each LED display presents fuel quantity in kg x 1000.
The display is justified to the right and the zero,in
tens columns is never displayed. If the fuel mass is
less than 1000 kg, the display will show a leading
"0".
If an Arinc 429 bus failure or an internal processing
failure occurs, the MTI will blank all displays.
TMUFUEN01-T04 LEVEL 3
EFFECTIVITY 28-42-00 Page 8
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 268
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - MULTI-TANK INDICATOR
TMUFUEN01-P04 LEVEL 3
EFFECTIVITY 28-42-00 Page 9
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 269
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
FQIC
IDENTIFICATION
FIN: 3QT
LOCATION
ZONE: 92VU
COMPONENT DESCRIPTION
The FQI computer is of the 3 MCU size and is connected
to the aircraft electrical wiring through an Arinc 600
connector.
TMUFUEN01-T05 LEVEL 3
EFFECTIVITY 28-42-00 Page 10
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 270
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - FQIC
TMUFUEN01-P05 LEVEL 3
EFFECTIVITY 28-42-00 Page 11
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 271
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
MEMORY MODULE
IDENTIFICATION
FIN: 7QT
LOCATION
ZONE: 92VU
COMPONENT DESCRIPTION
The connector plug is polarized to prevent damage
caused by incorrect installation.
The FQIC uses the OBRM (EPROM) to make sure that the
hardware is compatible with the FQIS.
TMUFUEN01-T06 LEVEL 3
EFFECTIVITY 28-42-00 Page 12
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 272
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - MEMORY MODULE
TMUFUEN01-P06 LEVEL 3
EFFECTIVITY 28-42-00 Page 13
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 273
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
MANUAL MAGNETIC FUEL LEVER INDICATOR
IDENTIFICATION
FIN: 104QM TO 113QM, 92QM
LOCATION
ZONE: 540, 640, 142
COMPONENT DESCRIPTION
MMI OPERATION:
- Press in the pushbutton and quarter turn in
either direction to eject the rod.
- Withdraw the rod lightly until magnetic
attraction is felt.
- Read fuel level on graduated rod at point
coinciding with sight collar.
- Using this reading, the fuel specific gravity
and the a/c attitude, calculate the quantity
of fuel in the tank using charts.
- Replace the indicator rod by sliding it into
the tube and lock by a quarter turn.
CAUTION: YOU CAN EASILY CAUSE DAMAGE TO THE MAGNETIC
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