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· Fault Light Illuminates
amber to
indicate:
· Overpressure
downstream of
Bleed valve
· Bleed overheat
· Wing or engine leak on
associated side
· Bleed valve not closed during
Engine Start
· Bleed valve not closed with
APU Bleed ON
APU BLEED Switch
· ON Opens
APU Bleed valve provided
N is greater than 95% and there is no
leak on APU or left side Bleed.
· OFF Closes
APU valve.
· Fault Light Illuminates
amber when
APU leak is detected.
·
X BLEED Selector
· AUTO Opens
crossbleed valve if
APU Bleed valve is open; closes
crossbleed valve if APU Bleed valve is
closed or an air leak is detected.
· OPEN Opens
crossbleed valve
SHUT Closes
crossbleed valve
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 242.2.10.
Anti Ice Control, Window Heat & Cabin Press Panel(A320)
Anti Ice
Wing
Controls Wing Anti Ice system simultaneously
on both Wings.
· ON
· "ON" light illuminates
· "WING A. ICE" message
appear on ECAM MEMO
display
· Wing Anti Ice valves open
provided pneumatic supply is
available. On the ground, the
valves open for 30 seconds
only
· OFF
· "ON" light goes OFF
· Wing Anti Ice valves close
· Fault Light Illuminates
when either of
the following occur:
· Wing Anti Ice valve position
disagrees with selected
position.
· Low pressure is detected.
·
ENG 1 / 2
Controls the respective engine antiice
system.
· ON
· "ON" light illuminates
· "ENG A. ICE" message
appear on ECAM MEMO
display
· Engine Anti Ice valves open
provided Engine bleed air is
available.
· Continuous ignition is provided
when the valve is open
· OFF
· "ON" light goes OFF
· Engine Anti Ice valves close
· Fault Light Illuminates
if Engine Anti
Ice valve position disagrees with
switch position.
Probe/Window Heat
Probe/Window Heat
· AUTO Provides
automatic Heating of
Probes and Windows:
· Inflight
· On the ground provided one
engine is running. (TAT
Probes excluded)
· ON Provides
Heating of Probes and
Windows:
·
Cabin PRESS
MAN V/S CTL Switch
Controls the outflow valve position via the
manual motor, when MODE SEL switch is
positioned to MAN. Spring loaded to neutral.
Switch must be held in position until target V/S
is reached, as outflow valve operation is slow.
· UP Moves
valve towards open
position.
· DN Moves
valve towards closed
position.
·
Mode SEL Switch
· Auto Automatic
mode is operating.
Outflow valve is controlled by one
system at a time.
· MAN Allows
manual control by the
MAN V/S CTL switch. Illuminates white
when selected. The cabin altitude
indication on the ECAM PRESS page
may fluctuate when switching from
AUTO to MAN.
· Fault Light Illuminates
amber only
when fault detected in both automatic
systems.
LDG ELEV Selector
· Auto (Detent) Pressurization
system
uses FMGSdetermined
landing
elevation to optimize pressure
schedule.
· Other Positions Pressurization
system uses selected value for landing
elevation reference in the event of an
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Flight Deck Documentation AIRBUS A320
12.11.06 Ralf Anderseck Seite 25FMGC
failure or incorrect landing
elevation in the database. Actual value
is displayed on the ECAM CRUISE
and PRESS pages.
·
Ditching Switch ( Guarded )
· Normal Selects
normal system
operation.
· ON Commands
operating system to
close the outflow valve, emergency
ram air inlet, avionics ventilation inlet
and extract valves and pack flow
control valve.
Outflow valve will not automatically
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