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DUALCOMP
IDENTIFICATION
FIN: 53QT
LOCATION
ZONE: 540
COMPONENT DESCRIPTION
The dualcomp is installed in the lowest part of the
left wing tank.
It houses two parallel plate capacitors.
The capacitive charge is used by the FQIC for fuel
mass calculation.
TMUFUEN05-T02 LEVEL 3
EFFECTIVITY 28-42-00 Page 184
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 334
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - ULTRACOMP - DUALCOMP
TMUFUEN05-P02 LEVEL 3
EFFECTIVITY 28-42-00 Page 185
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 335
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
FUEL QUANTITY PRESELECTOR
IDENTIFICATION
FIN: 5QT
LOCATION
ZONE: 640
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.
MULTI-TANK INDICATOR
IDENTIFICATION
FIN: 6QT
LOCATION
ZONE: 640
COMPONENT DESCRIPTION
Each LED display presents fuel quantity in kg x 1000.
The display is justified to the right and the zero in
the 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.
TMUFUEN05-T03 LEVEL 3
EFFECTIVITY 28-42-00 Page 186
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 336
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - FUEL QUANTITY PRESELECTOR -
MULTI-TANK INDICATOR
TMUFUEN05-P03 LEVEL 3
EFFECTIVITY 28-42-00 Page 187
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 337
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
FQIC
IDENTIFICATION
FIN: 3QT
LOCATION
ZONE: 92VU
COMPONENT DESCRIPTION
The FQIC is of the 4 MCU size and is connected to the
aircraft electrical wiring through an ARINC 600
connector.
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 OBRMs (EPROM) to make sure that the
hardware is compatible with the FQIS.
TMUFUEN05-T04 LEVEL 3
EFFECTIVITY 28-42-00 Page 188
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 338
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - FQIC - MEMORY MODULE
TMUFUEN05-P04 LEVEL 3
EFFECTIVITY 28-42-00 Page 189
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 339
ALL
FUEL QUANTITY INDICATING SYSTEM COMPONENTS
MAGNETIC LEVEL INDICATOR
IDENTIFICATION
FIN: 104QM to 111QM, 204QM to 211QM, (92QM)
LOCATION
ZONE: 540, 640, (142)
COMPONENT DESCRIPTION
CAUTION: You can easily cause damage to the magnetic
level indicators.Do not touch or push against
them when you are in the fuel tank.
ATTITUDE MONITOR
IDENTIFICATION
FIN: 39QM
LOCATION
ZONE: 192
TMUFUEN05-T05 LEVEL 3
EFFECTIVITY 28-42-00 Page 190
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 340
ALL
TMUFUEN05-P05 LEVEL 3
FUEL QUANTITY INDICATING SYSTEM COMPONENTS - MAGNETIC LEVEL INDICATOR - ATTITUDE MONITOR
EFFECTIVITY 28-42-00 Page 191
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 341
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFUEN05 LEVEL 3
EFFECTIVITY 28-42-00 Page 192
May 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 28 FUEL SYSTEM
UF94200
EFFECTIVITY Page 342
ALL
28 - FUEL SYSTEM
28-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENTS:
Fqis Status
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ATA 28 FUEL SYSTEM(41)
