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information from two Total Air Temperature sensors.
NOTE: that ADIRU3 receives the Total Air Temperature
(TAT) from the TAT 1 sensor which is composed
of two elements.
WATER DRAIN
The probes are installed in such a way that their
pressure lines do not require a water drain, except
for that of the standby static ports.
TMUADIB01-T01 LEVEL 1
EFFECTIVITY 34-13-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 62
ALL
AIR DATA PROBES PRESENTATION
TMUADIB01-P01 LEVEL 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 63
ALL
SELF EXAMINATION
How do pitot and static probes supply the ADIRUs?
A - Using ADMs which convert pressure into
digital format.
B - Directly with total and static pressures.
C - Directly with digital format.
Where does ADIRU3 receive TAT information from?
A - Captain TAT sensor.
B - First-Officer TAT sensor.
C - Standby TAT sensor.
Which pressure line(s) need(s) to be drained?
A - All pitot lines.
B - All static lines.
C - Only the standby static line.
TMUADIB01 LEVEL 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
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ALL
34 - NAVIGATION
34-10-00 ADIRS CDU PRESENTATION
CONTENTS:
System Selector
Keyboard
ON BAT Light
IR Lights
Mode Rotary Selector
ADR P/BSW
Data Selector
Data Display
Status Messages
Status Action Codes
Self Examination
TMUNAV101 LEVEL 1
EFFECTIVITY 34-10-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 65
ALL
ADIRS CDU PRESENTATION
SYSTEM SELECTOR
In OFF position, the CDU display is not energized
(Blank Display).
In position 1, 2 or 3 the corresponding system is
selected for data display.
KEYBOARD
The keyboard is used to enter in the selected system
the present position for alignment or Magnetic Heading
if in ATTITUDE mode.
N, S, E, W keys permit position entry.
H allows heading entry in attitude mode.
The green ENTER pushbutton light comes on when either
the NORTH, SOUTH, WEST, EAST, or HEADING has been
selected. When pressed the displayed data is entered
into the Inertial Reference Systems.
The green CLEAR pushbutton light comes on when any key
has been pressed.
When pressed, the displayed data, not yet entered, is
cleared.
ON BAT LIGHT
The amber ON BAT light comes on when one or more Air
Data Inertial Reference Unit are operating on aircraft
batteries.
The ON BAT light comes on for five seconds during the
power up test. ON BAT stays off in case of fast
realignment.
IR LIGHTS
An amber FAULT light comes on, accompanied by ECAM
activation when a fault affects the related Inertial
Reference.
When flashing, attitude and heading may be recovered
in ATT mode.
A white ALIGN light illuminates steady when the related
Inertial Reference is in the alignment phase.
The ALIGN light goes off when alignment has been
completed.
ALIGN light flashes in case of:
- An alignment error
- No Present Position entry within ten minutes
of NAV mode selection.
- Significant difference memorized position at
shutdown and entered position.
MODE ROTARY SELECTOR
The mode rotary selector permits selection of three
modes for each Inertial Reference.
In OFF position, the ADIRU is not energized (ADR and
IR data not available).
NAVIGATION is the normal mode of operation providing
full inertial data to the aircraft systems.
ATTITUDE is a back-up mode, mainly providing attitude
and heading information in case of loss of navigation
capability.
In ATT mode, the magnetic heading must be entered
through the CDU and has to be updated frequently.
TMUNAV101-T01 LEVEL 1
EFFECTIVITY 34-10-00 Page 2
May 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 66
ALL
ADIRS CDU PRESENTATION - SYSTEM SELECTOR
TMUNAV101-P01 LEVEL 1
EFFECTIVITY 34-10-00 Page 3
May 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
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