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the avionics
compartment lighting to come on
automatically when the avionics
compartment door is opened.
· ON Turns
the avionics compartment
lighting on.
HYD
Blue Pump OVRD Switch (Guarded)
· ON The
Blue electric pump is
energized, provided the BLUE ELEC
PUMP switch, located on the hydraulic
panel, is in AUTO.
Leak Measurement Valve Switches
(Guarded)
Used for Maintenance ground test only. When
the light is on, portions of the Hydraulic system
are inoperative.
APU Auto Extinguishing Panel
APU TEST Switch
Tests APU Fire Warning, auto extinguishing
and shutdown circuits. For test, MASTER
switch must be ON and TEST switch must be
held down for 10 seconds. The OK light comes
on to indicate a successful test.
Reset Switch
Resets test circuit.
ENG
ENG FADEC GND PWR
Switches (Guarded)
· ON Supply
the associated FADEC
with ground power, provided the ENG
FIRE switch is not released.
· Off Disconnect
ground power.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 92.1.6.
Captain's and F/O's
Read Light Control(A320)
Ajustable Light
Reading Light Knob
Controls the intensity of the overhead Reading Light.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 102.2.
Overhead Panel 2
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 112.2.1.
OBS Audio ENT ( A320 )
OBS Audio ENT
Observer Audio
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 122.2.2.
ADIRS Control Display Panel
(A320)
Data Display Window
Displays the data selected by the DATA
Selector. Keyboard entry overrides the display.
Data Selector
· Test Displays
all 8s in data display
window and illuminates ENT and CLR
keys.
· TK/GS Displays
true track and
groundspeed.
· PPOS Displays
present latitude and
longitude.
· WIND Displays
true Wind direction
and speed.
· HDG Displays
true Heading and
minutes remaining until alignment is
completed.
· STS Displays
system status
message code.
SYS Selector
· OFF Blanks
data display window.
· 1, 3 or 2 Displays
data for associated
IRS.
Data Entry Keyboard
Allows entry of preset position or heading in
ATT mode, in the selected system.
· Alpha Keys Select
N, S, E, W for
present position entry or H for heading
entry in ATT mode.
· Numeric Keys Key
in present position
or present magnetic heading in ATT
mode, to the data display window.
· ENT Key Illuminates
when and alpha
key is selected. Enters keyed data into
the ADIRS when pushed.
· CLR Key Illuminates
when keyed
data is of an unreasonable value.
Clears keyed (but not yet entered)
data from display window when
pushed.
ON BAT Light
Illuminates amber when one or more ADIRUs
is supplied by airplane battery only. Also
illuminates for a few seconds at the beginning
of the alignment.
IR Lights 1, 2 & 3 toptop
· FAULT Illuminates
amber when a
Fault affects the associated IR.
Flashes if attitude and heading
information is recoverable in the ATT
mode.
· ALIGN Illuminates
white when the
associated IR is operating normally in
the ALIGN mode.
Flashes if:
· IR alignment fault detected.
· No present position entry has
been made after ten minutes.
· Difference between position at
shut down and entered
position exceeds 1° of latitude
or longitude.
IR Mode Selector toptop
· OFF Deactivates
associated ADIRU.
Both ADR and IR data are not
available,
· NAV Provides
full inertial data to
airplane system.
· ATT Provides
only attitude and
　
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