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TMUPNEI01-P04 LEVEL 3
EFFECTIVITY 36-12-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 67
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS
APU BLEED CHECK VALVE
IDENTIFICATION
FIN: 7260HM
LOCATION
ZONE: 150
COMPONENT DESCRIPTION
The APU bleed check valve is of the flapper type.
It protects the APU from reverse flow when another
source is supplying Bleed air at a higher pressure.
TMUPNEI01-T05 LEVEL 3
EFFECTIVITY 36-12-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 68
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS - APU BLEED CHECK VALVE
TMUPNEI01-P05 LEVEL 3
EFFECTIVITY 36-12-00 Page 11
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 69
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS
HP GROUND CONNECTOR
IDENTIFICATION
FIN: 7300HM
LOCATION
ZONE: 191
COMPONENT DESCRIPTION
The HP ground connector contains a check valve of the
flapper type and a built-in nipple.
A duct connects the HP ground connector with the
crossfeed duct on the left hand side of the cross bleed
valve.
TMUPNEI01-T06 LEVEL 3
EFFECTIVITY 36-12-00 Page 12
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 70
ALL
GND AND APU BLEED AIR SUPPLY COMPONENTS - HP GROUND CONNECTOR
TMUPNEI01-P06 LEVEL 3
EFFECTIVITY 36-12-00 Page 13
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 71
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUPNEI01 LEVEL 3
EFFECTIVITY 36-12-00 Page 14
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 72
ALL
36 - PNEUMATIC SYSTEM
36-22-00 PNEUMATIC LEAK DETECTION
COMPONENTS
CONTENTS:
Wing Leak Detection Element
Pylon Detection Element
APU Detection Element
TMUPNEK01 LEVEL 3
EFFECTIVITY 36-22-00 Page 1
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 73
ALL
PNEUMATIC LEAK DETECTION COMPONENTS
WING LEAK DETECTION ELEMENT
IDENTIFICATION
FIN: 21HF ® 79HF
LOCATION
ZONE:
COMPONENT DESCRIPTION
Installed in each wing along the forward face of the
front spar and in the mid fuselage along the hot air
ducts.
Triggering signal: Temperature > 124°C.
Sensing elements mounted in series with connecting
cables where necessary.
At the alarm temperature, the impedance between the
solid nickle conductor and the outer tubing decreases
suddenly, the center conductor grounds and gives an
alarm signal to the BMC.
TMUPNEK01-T01 LEVEL 3
EFFECTIVITY 36-22-00 Page 2
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 74
ALL
PNEUMATIC LEAK DETECTION COMPONENTS - WING LEAK DETECTION ELEMENT
TMUPNEK01-P01 LEVEL 3
EFFECTIVITY 36-22-00 Page 3
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 75
ALL
PNEUMATIC LEAK DETECTION COMPONENTS
PYLON DETECTION ELEMENT
IDENTIFICATION
FIN: 1HF1, 1HF2
LOCATION
ZONE: 410, 420
COMPONENT DESCRIPTION
Located at the outlet of the pylon ventilation duct.
Triggering signal: Temperature > 204°C.
Only one sensing element.
At the alarm temperature, the impedance between the
solid nickle conductor and the outer tubing decreases
suddenly, the center conductor grounds and gives an
alarm signal to the BMC.
TMUPNEK01-T02 LEVEL 3
EFFECTIVITY 36-22-00 Page 4
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 76
ALL
PNEUMATIC LEAK DETECTION COMPONENTS - PYLON DETECTION ELEMENT
TMUPNEK01-P02 LEVEL 3
EFFECTIVITY 36-22-00 Page 5
Nov 30/97
　
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