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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 77
ALL
PNEUMATIC LEAK DETECTION COMPONENTS
APU DETECTION ELEMENT
IDENTIFICATION
FIN: 11HF ® 20 HF
LOCATION
ZONE: APU duct
COMPONENT DESCRIPTION
Installed between check valve and APU compartment
Triggering signal: Temperature > 124°C.
Sensing elements mounted in series.
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-T03 LEVEL 3
EFFECTIVITY 36-22-00 Page 6
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 78
ALL
PNEUMATIC LEAK DETECTION COMPONENTS - APU DETECTION ELEMENT
TMUPNEK01-P03 LEVEL 3
EFFECTIVITY 36-22-00 Page 7
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 79
ALL
THIS PAGE INTENTIONALYY BLANK
TMUPNEK01 LEVEL 3
EFFECTIVITY 36-22-00 Page 8
Nov 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 36 PNEUMATIC SYSTEM
UF94200
EFFECTIVITY Page 80
ALL
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ATA 36 PNEUMATIC(11)
