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MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 55
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ENGINE BLEED AIR SUPPLY COMPONENTS
BLEED MONITORING COMPUTER (BMC)
IDENTIFICATION
FIN: 1HA1, 1HA2
LOCATION
ZONE: 121, 122
COMPONENT DESCRIPTION
It monitors and controls the engine bleed system.
At each power-up, a test of the BMC and of the leak
detection system is done.
TMUPNEH06-T06 LEVEL 3
EFFECTIVITY 36-11-00 Page 12
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 56
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ENGINE BLEED AIR SUPPLY COMPONENTS - BMC
TMUPNEH06-P06 LEVEL 3
EFFECTIVITY 36-11-00 Page 13
Jun 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 57
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUPNEH06 LEVEL 3
EFFECTIVITY 36-11-00 Page 14
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 58
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36 - PNEUMATIC SYSTEM
36-12-00 GND AND APU BLEED AIR SUPPLY
COMPONENTS
CONTENTS:
APU Bleed Valve (GTCP 36-300)
APU Bleed Valve (APIC)
APU Bleed Valve (GTCP 131-9A)
X Bleed Valve
APU Bleed Check Valve
HP Ground Connector
TMUPNEI01 LEVEL 3
EFFECTIVITY 36-12-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 59
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS
APU BLEED VALVE (GTCP 36-300)
IDENTIFICATION
FIN: 4005KM
LOCATION
ZONE: 310
COMPONENT DESCRIPTION
Spring loaded closed
TMUPNEI01-T01 LEVEL 3
EFFECTIVITY 36-12-00 Page 2
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 60
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS - APU BLEED VALVE (GTCP 36-300)
TMUPNEI01-P01 LEVEL 3
EFFECTIVITY 36-12-00 Page 3
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 61
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS
APU BLEED VALVE (APIC)
IDENTIFICATION
FIN: 110KD
LOCATION
ZONE: 316
COMPONENT DESCRIPTION
The Bleed Control Valve is located on the right lower
part of the APU at the scroll outlet.
It delivers air to the aircraft while avoiding load
compressor surge.
TMUPNEI01-T02 LEVEL 3
EFFECTIVITY 36-12-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 62
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TMUPNEI01-P02 LEVEL 3
GND AND APU BLEED AIR SUPPLY COMPONENTS - APU BLEED VALVE (APIC)
EFFECTIVITY 36-12-00 Page 5
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 63
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS
APU BLEED VALVE (GTCP 131-9A)
IDENTIFICATION
FIN: TBD
LOCATION
ZONE: 316
COMPONENT DESCRIPTION
Spring loaded closed.
TMUPNEI01-T03 LEVEL 3
EFFECTIVITY 36-12-00 Page 6
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 64
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS - APU BLEED VALVE (GTCP 131-9A)
TMUPNEI01-P03 LEVEL 3
EFFECTIVITY 36-12-00 Page 7
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 65
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GND AND APU BLEED AIR SUPPLY COMPONENTS
X BLEED VALVE
IDENTIFICATION
FIN: 6HV
LOCATION
ZONE: 192
COMPONENT DESCRIPTION
For safety reasons, the valve is equipped with two
electric motors which can both actuate the butterfly
in opening or closing directions.
A brake system locks the valve in position when
electrical power is cut off.
TMUPNEI01-T04 LEVEL 3
EFFECTIVITY 36-12-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 66
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS - X BLEED VALVE
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