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Severe Ice Detected
Ice Detect Fault
TMUIC3201 LEVEL 3
EFFECTIVITY 30-81-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
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TMUIC3201-P01 LEVEL 3
DUAL ADVISORY ICE DETECTION SYSTEM WARNINGS
EFFECTIVITY 30-81-00 Page 2
Aug 06/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
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30 - ICE AND RAIN PROTECTION
30-81-00 DUAL ADVISORY ICE DETECTION
SYSTEM INTERFACES
CONTENTS:
FWCs
SDACs
CFDIU
Wing Anti-Ice Relays
TMUIC3301 LEVEL 3
EFFECTIVITY 30-81-00 Page 1
Sep 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
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DUAL ADVISORY ICE DETECTION SYSTEM INTERFACES
FWCs
Each ice detector sends "ICE" and "SEVERITY" signals
to Flight Warning Computers 1 and 2 respectively in
case of an elementary ice detection or 7 elementary
ice detections.
This in order to display class 1 warning messages on
the ECAM warning display. These messages can be
respectively inhibited by engine or wing anti-ice
selection.
SDACs
Each ice detector sends a "FAULT" signal to System
Data Acquisition Concentrators 1 and 2 in case of
failure during either power up, MCDU or in operation
tests.
A class 1 failure message is displayed on the ECAM
warning display in case of dual ice detector failure.
CFDIU
Each ice detector sends a "FAULT" signal to the
Centralized Fault Display Interface Unit in case of
failure during either power up, MCDU or in operation
tests.
A class 2 fault message is displayed on the MCDU
ANTI-ICE ICE DETECTOR 1 or 2 system page in case of
ice detector failure.
WING ANTI-ICE RELAYS
When wing anti-ice valves are controlled to open, two
ground signals are sent to the ice detectors in order
to reset the ice detection counter and cut off the
"SEVERITY" signal.
TMUIC3301-T01 LEVEL 3
EFFECTIVITY 30-81-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
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TMUIC3301-P01 LEVEL 3
DUAL ADVISORY ICE DETECTION SYSTEM INTERFACES
EFFECTIVITY 30-81-00 Page 3
Sep 30/94
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
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TMUIC3301 LEVEL 3
EFFECTIVITY 30-81-00 Page 4
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30 - ICE AND RAIN PROTECTION
30-81-31 DUAL ADVISORY ICE DETECTION
SYSTEM COMPONENTS
CONTENTS:
Ice Detectors
TMUIC3401 LEVEL 3
EFFECTIVITY 30-81-31 Page 1
Aug 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
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DUAL ADVISORY ICE DETECTION SYSTEM COMPONENTS
ICE DETECTORS
IDENTIFICATION
FIN: (LH) 2DD1, (RH) 2DD2
LOCATION
ZONE: 121
DESCRIPTION
The probe consists of a magnetostrictive nickel alloy
tube. In addition, the strut also contains the drive
and feedback coils and probe heaters, and the probe
biaising magnetic.
The microcomputer section consists of a 8035
microcomputer, 27C32 EPROM and an interface latch.
TMUIC3401-T01 LEVEL 3
EFFECTIVITY 30-81-31 Page 2
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TMUIC3401-P01 LEVEL 3
DUAL ADVISORY ICE DETECTION SYSTEM COMPONENTS - ICE DETECTORS
EFFECTIVITY 30-81-31 Page 3
Aug 31/96
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UF94200
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