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MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 76
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS - FLOW CONTROL VALVE
TMUTEMN0A-P03 LEVEL 3
EFFECTIVITY 21-50-00 Page 7
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 77
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS
FLOW CONTROL VALVE REMOVAL/INSTALLATION
IDENTIFICATION
FIN: 8HB, 11HB
LOCATION
ZONE: 182, 191
COMPONENT DESCRIPTION
The Flow Control Valve is connected via V-clamps to
the bleed air duct on one side and the heat exchanger
duct on the other side.
TMUTEMN0A-T04 LEVEL 3
EFFECTIVITY 21-50-00 Page 8
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 78
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS - FLOW CONTROL VALVE R/I
TMUTEMN0A-P04 LEVEL 3
EFFECTIVITY 21-50-00 Page 9
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 79
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS
BYPASS VALVE (BPV)
IDENTIFICATION
FIN: 10HH, 30HH
LOCATION
ZONE: 191, 192
COMPONENT DESCRIPTION
The ByPass Valve (BPV) is electrically controlled and
actuated by a stepper motor. Limit switches signal
fully open or fully closed positions to the pack
controller secondary computer.
Pack controller primary and secondary computers
receive a step counting signal used for the ByPass
Valve position determination.
A manual override and visual position indicator device
is installed on the bottom of the shaft.
TMUTEMN0A-T05 LEVEL 3
EFFECTIVITY 21-50-00 Page 10
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 80
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS - BYPASS VALVE (BPV)
TMUTEMN0A-P05 LEVEL 3
EFFECTIVITY 21-50-00 Page 11
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 81
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS
RAM AIR INLET (RAI) ACTUATOR
IDENTIFICATION
FIN: 8HH, 28HH
LOCATION
ZONE: 191, 192
COMPONENT DESCRIPTION
The ram air inlet actuator has:
- an AC motor, electrically supplied by the pack
controller (two different motor suppliers),
- two limit switches (one for the closed
position, the other for the 70% open position).
These send signals to the secondary computer,
- two potentiometers (one for control through
the primary computer, the other for
indication through the secondary computer).
TMUTEMN0A-T06 LEVEL 3
EFFECTIVITY 21-50-00 Page 12
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 82
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS - RAM AIR INLET (RAI) ACTUATOR
TMUTEMN0A-P06 LEVEL 3
EFFECTIVITY 21-50-00 Page 13
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 83
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS
ANTI-ICE VALVE
IDENTIFICATION
FIN: 17HH, 37HH
LOCATION
ZONE: 191, 192
COMPONENT DESCRIPTION
The Anti-Ice Valve is electrically controlled and
pneumatically operated.
Anti-ice mode: valve energized.
The valve opens if ice is detected across the high or
low pressure side of the condenser.
Pneumatic temperature control mode: valve
de-energized.
The valve is controlled by a pneumatic sensor to get
a fixed temperature (15ºC or 59ºF).
TMUTEMN0A-T07 LEVEL 3
EFFECTIVITY 21-50-00 Page 14
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 84
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS - ANTI-ICE VALVE
TMUTEMN0A-P07 LEVEL 3
EFFECTIVITY 21-50-00 Page 15
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 85
ALL
ZONE TEMPERATURE CONTROL - PACK COMPONENTS
PACK DOWNSTREAM CHECK VALVE
　
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