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EFFECTIVITY 36-11-00 Page 3
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 47
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS
PRESSURE REGULATING VALVE (PRV)
IDENTIFICATION
FIN: 4001HA1, 4001HA2
LOCATION
ZONE: 450, 460
COMPONENT DESCRIPTION
The valve is spring loaded closed.
BLEED PRESSURE REGULATED VALVE CONTROL SOLENOID (CTS)
IDENTIFICATION
FIN: 10HA1, 10HA2
LOCATION
ZONE: 413, 423
COMPONENT DESCRIPTION
Three functions:
- PRV electrical shut off (Solenoid)
- Temperature Limitation
- Reverse flow inhibition
TMUPNEH06-T02 LEVEL 3
EFFECTIVITY 36-11-00 Page 4
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 48
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS - PRV - CTS
TMUPNEH06-P02 LEVEL 3
EFFECTIVITY 36-11-00 Page 5
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 49
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS
PRECOOLER
IDENTIFICATION
FIN: 7150HM1, 7150HM2
LOCATION
ZONE: 410, 420
COMPONENT DESCRIPTION
Single cross pass heat exchanger.
FAN AIR VALVE (FAV)
IDENTIFICATION
FIN: 9HA1, 9HA2
LOCATION
ZONE: 453, 463
COMPONENT DESCRIPTION
The valve is spring loaded closed.
FAN AIR VALVE CONTROL THERMOSTAT (CT)
IDENTIFICATION
FIN: 7170HM1, 7170HM2
LOCATION
ZONE: 410, 420
COMPONENT DESCRIPTION
It is pneumatically coupled to the Fan Air Valve to
control it open if the temperature downstream of the
precooler exceeds 200°C ( 392°F ).
TMUPNEH06-T03 LEVEL 3
EFFECTIVITY 36-11-00 Page 6
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 50
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS - PRECOOLER - FAV - CT
TMUPNEH06-P03 LEVEL 3
EFFECTIVITY 36-11-00 Page 7
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 51
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS
INTERMEDIATE PRESSURE CHECK VALVE (IPC)
IDENTIFICATION
FIN: 7110HM1, 7110HM2
LOCATION
ZONE: 450, 460
OVERPRESSURE VALVE (OPV)
IDENTIFICATION
FIN: 5HA1, 5HA2
LOCATION
ZONE: 453, 563
COMPONENT DESCRIPTION
The valve is spring loaded open.
TMUPNEH06-T04 LEVEL 3
EFFECTIVITY 36-11-00 Page 8
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 52
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS - IPC - OPV
TMUPNEH06-P04 LEVEL 3
EFFECTIVITY 36-11-00 Page 9
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 53
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS
REGULATED PRESSURE (Pr)
IDENTIFICATION
FIN: 8HA1, 8HA2
LOCATION
ZONE: 415, 425
COMPONENT DESCRIPTION
It is connected to both BMCs for pressure indication
and system fault monitoring purposes.
It is also connected by a sense line to the duct
downstream of the PRV.
TRANSFERRED PRESSURE (Pt)
IDENTIFICATION
FIN: 7HA1, 7HA2
LOCATION
ZONE: 415, 425
COMPONENT DESCRIPTION
It is connected to its dedicated BMC for faulty
component identification in case of failure.
It is also connected by a sense line to the duct
downstream of the HP bleed valve.
It gives the tranferred relative static pressure.
HEAT EXCHANGER OUTLET TEMPERATURE SENSOR (T)
IDENTIFICATION
FIN: 6HA1, 6HA2
LOCATION
ZONE: 413, 423
COMPONENT DESCRIPTION
It is connected to both BMCs for temperature indication
(ECAM) and FAULT logic.
It also monitors the temperature downstream of the
precooler.
TMUPNEH06-T05 LEVEL 3
EFFECTIVITY 36-11-00 Page 10
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 54
ALL
ENGINE BLEED AIR SUPPLY COMPONENTS - PR - PT - T
TMUPNEH06-P05 LEVEL 3
EFFECTIVITY 36-11-00 Page 11
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
　
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