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heading data if loss of navigation
capability occurs. Heading must be
entered via the ADIRS Control Display
Unit and must be reset frequently.
ADR Lights 1, 2 & 3 toptop
· FAULT Illuminates
amber when a
fault is detected in the associated air
data reference part.
OFF Switch Disconnects
air data output to
associated ADR. IR is not affected.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 13“
2.2.3 EVAC Controls (A320)“ \|3
2.2.3 EVAC Controls (A320)
Flight Controls
ELAC Switch
· ON Engages
the associated elevator
and aileron computer.
· OFF Disengages
associated
computer.
· Fault Light Illuminates
amber:
· When a failure is detected
· During ELAC power up test.
SEC Switch
· ON Engages
the associated spoiler
and elevator and aileron computer.
· OFF Disengages
associated
computer.
· Fault Light Illuminates
amber when a
failure is detected.
FAC Switch
· ON Engages
the associated flight
augmentation computer.
· OFF Disengages
associated
computer.
· Fault Light Illuminates
amber when a
failure is detected.
·
EVAC
Command Switch
ON Activates
evacuation alert. The EVAC
light flashes and horn sounds in the cockpit.
EVAC lights flash at forward and AFT Flight
Attendant panels and Evacuation tone sounds
in the cabin. Pushing the COMMAND switch a
second time cancels the Evacuation alert.
Horn Shut OFF Switch
Silences the Evacuation Horn in the cockpit
when pushed.
CAPT and CAPT/PURS Switch (Wired
Guard)
Safety wired to the CAPT/PURS position.
Allows activation of an Evacuation alert from
the cockpit or cabin.
EMER ELEC PWR
EMER GEN Test Switch
Normally used by Maintenance.
GEN 1 Line Switch
· OFF Causes
the GEN 1 line
contactor to open. A fuel pump in each
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 14wing
tank remains powered by GEN 1
and GEN 2 powers AC bus 1.
· Smoke Light Illuminates
amber when
Smoke is detected in the avionics
Ventilation systen.
RAT & ENER GEN Fault Light
Illuminates
red with a loss of power to AC
buses 1 and 2 if:
· The emergency generator is not
supplying electrical power, and
· the nose gear is up.
MAN ON Switch
· AUTO The
RAT extends
automatically, provided AC bus 1 and
2 are not electrically powered and
speed is above 100 knots. If the
Landing Gear is up, the emergency
generator is hydraulically powered by
the blue system.
· ON The
RAT extends. Emergency
generators coupling occurs provided
the landing gear is up.
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 152.2.4.
Ground Proximity Warning
System (GPWS) &
Cockpit Voice Recorder (RCDR) (
A320 )
GPWS
TERR
· OFF Inhibits
the GPWS enhanced
modes.
· FAULT Illuminates
when failure is
detected with the enhanced modes.
SYS Switch
· OFF All
GPWS warnings are
inhibited.
· FAULT Light Illuminates
amber when
a GPWS malfunction is detected. All
GPWS warning are inhibited.
G/S Mode
Inhibits the GPWS glide slope mode.
FLAP Mode
Inhibits the GPWS Flap Mode to prevent
nuisance warnings when landing with other
than landing flaps.
LDG FLAP 3
· ON Inhibits
the GPWS Flap Mode to
prevent nuisance warnings when
landing with flaps 3.
RCDR
GND CTL Switch (Springloaded)
Any power interruption may cause the GND
CTL switch to revert to AUTO.
· ON Energizes
the cockpit voice
recorder (CVR) and digital flight data
recorder (DFDR). The ON light
illuminates.
· AUTO CVR
and DFDR are
automatically energized illuminates.
· On the ground for the first five
minutes following electrical
　
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