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MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 149
ALL
ADIRS COMPONENTS
AIR DATA MODULE
IDENTIFICATION
FIN: 19FP1, 19FP2, 19FP3, 19FP4
19FP5, 19FP6, 19FP7, 19FP8
LOCATION
ZONE: 121, 125, 126, 127, 128
COMPONENT DESCRIPTION
The ADMs are near and above the level of the pitot and
static probes, this to permit the ADM pneumatic
plumbing to be self draining (except stby static line).
AOA SENSORS
IDENTIFICATION
FIN: 3FP1, 3FP2, 3FP3
LOCATION
ZONE: 127, 128
COMPONENT DESCRIPTION
The AOA sensor is of the windvane type.
The sensing element is a small wing, positioned in the
airflow direction, linked to a free turning shaft.
TMUADIO03-T01 LEVEL 3
EFFECTIVITY 34-10-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 150
ALL
TMUADIO03-P01 LEVEL 3
ADIRS COMPONENTS - ADMs AND AOAS
EFFECTIVITY 34-10-00 Page 3
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 151
ALL
ADIRS COMPONENTS
STATIC PROBES
IDENTIFICATION
FIN: 7DA1, 7DA2, 7DA3
8DA1, 8DA2, 8DA3
LOCATION
ZONE: 121, 122, 127, 128
COMPONENT DESCRIPTION
The probes are protected from icing by a heater
circuit.
TAT SENSORS
IDENTIFICATION
FIN: 11FP1, 11FP2
LOCATION
ZONE: 121, 122
COMPONENT DESCRIPTION
There are 2 sensing elements in each sensor.
The TAT sensors are heated through the Probe Heating
Computer (PHC).
The heating element must not be energized on the
ground.
NOTE: The second sensing element on the TAT 2 sensor
is not used.
TMUADIO03-T02 LEVEL 3
EFFECTIVITY 34-10-00 Page 4
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 152
ALL
ADIRS COMPONENTS - STATIC PROBES AND TATS
TMUADIO03-P02 LEVEL 3
EFFECTIVITY 34-10-00 Page 5
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 153
ALL
ADIRS COMPONENTS
PITOT PROBES
IDENTIFICATION
FIN: 9DA1, 9DA2, 9DA3
LOCATION
ZONE: 125, 126
COMPONENT DESCRIPTION
The probes are protected from icing by a heater
circuit.
ADIRS CDU
IDENTIFICATION
FIN: 2FP
LOCATION
ZONE: 211
COMPONENT DESCRIPTION
The ADIRS CDU is located on overhead panel 20VU.
It contains 3 identical connectors, each connector is
linked to one ADIRU.
TMUADIO03-T03 LEVEL 3
EFFECTIVITY 34-10-00 Page 6
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 154
ALL
ADIRS COMPONENTS - PITOT PROBES AND ADIRS CDU
TMUADIO03-P03 LEVEL 3
EFFECTIVITY 34-10-00 Page 7
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 155
ALL
ADIRS COMPONENTS
ADIRUs
IDENTIFICATION
FIN: 1FP1, 1FP2, 1FP3
LOCATION
ZONE: 127, 128
COMPONENT DESCRIPTION
The ADIRU is contained in a 4 MCU case as defined in
ARINC 600.
The ADIRU contains an ADR and an IR portion supplied
by a common power source.
VMO/MMO SWITCH
IDENTIFICATION
FIN: 22FP
LOCATION
ZONE: 128
COMPONENT DESCRIPTION
This switch is selected for particular flights with
the landing gear down (Ferry flights for example).
It allows the ADR to determine the normal or alternate
VMO/MMO law.
TMUADIO03-T04 LEVEL 3
EFFECTIVITY 34-10-00 Page 8
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 156
ALL
ADIRS COMPONENTS - ADIRUS AND VMO/MMO SWITCH
TMUADIO03-P04 LEVEL 3
EFFECTIVITY 34-10-00 Page 9
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 157
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUADIO03 LEVEL 3
EFFECTIVITY 34-10-00 Page 10
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 158
　
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