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BLEED overhead switches.
ANTI-ICE
The anti-ice protection system is controlled
through the ANTI ICE overhead section.
1. Wing anti-ice. Its status can be monitored
on the BLEED page.
2. Engine anti-ice.
3. Probe and Window anti-ice. It is fully
automatic. It provides low heating when
the aircraft is on the ground (to avoid
having ground personnel burnt if they
touch the probe) and provides full heating
as soon as the aircraft is airborne.
You can initiate full heating by pressing this
button. An 'ON' light then appears.
Alerts & Warnings
Status messages appear on the E/WD when
engine and wing anti-ice are used.
Message Color Reason
ENG A. ICE Green Engine anti-ice is on
WING A. ICE Green Wing anti-ice is on
AUXILIARY POWER UNIT (APU)
It is managed through the APU section of the
overhead.
SYSTEMS
Airbus Series Vol.1
(c) 2007 Wilco Publishing www.wilcopub.com - www.FeelThere.com 55
APU Start & Stop
To turn the APU on, first press the master
switch. The APU system is activated ('ON' blue
light appears on the master switch) and the
APU flap is opened to let the air enter into the
APU ('FLAP OPEN' message displayed on the
APU page). The APU page automatically
appears on the SD.
If fuel is available, the START button can then
be pressed, an 'ON' light appears on the
button. This launches the APU start sequence.
The start sequence can be monitored on the
APU page displayed on the SD.
When the APU is started, a green 'AVAIL' light
replaces the blue 'ON' light on the START
switch. An 'AVAIL' message appears on the
APU page and an ECAM message displays
'APU AVAIL'. The APU is now ready to provide
air and electricity.
The APU can be started at any altitude and at
any airspeed.
The APU fuel consumption is around 100kg per
hour.
APU Bleed
As soon as the APU is running, its air can be
used to start the engines. To do this, the crew
must press the APU BLEED button in the AIR
COND overhead section (see the Air section for
more details).
Note : If you are in Beginner mode, the APU is
not necessary to start the engines.
APU Page
The APU page appears automatically on the SD
during the APU start sequence. The crew can
also access this page by pressing the APU
button on the ECAM control panel.
1. AVAIL message appears as soon as the
APU start sequence is finished and the
APU is available.
2. FLAP OPEN message is displayed as soon
as the APU system is turned on and the
APU flap is opened to let air in.
3. This white box displays the APU electric
information : load, voltage and frequency. The
box disappears if the APU is not available. The
green arrow on top of the box disappears if
the APU GEN is turned off on the overhead.
4. This box shows the APU bleed information,
with the air bleed pressure. Amber XX is
displayed if the air bleed is not available.
5. Bleed air valve; controlled by the APU
BLEED switch on the overhead.
6. APU rotation speed.
7. APU Exhaust Gas Temperature (EGT).
SYSTEMS
Airbus Series Vol.1
56 For Microsoft Flight Simulator use only. Not for use in real aviation.
Alerts & Warnings
Status messages appear on the E/WD when
the APU is used.
Message Color Reason
APU AVAIL Green The APU is up and running
APU BLEED Green The APU is available and
the bleed valve is open
POWER PLANTS
The engines are managed by the Full Authority
Digital Engine Control (FADEC). This device
controls the engine during the start sequence
and during the flight to provide optimal usage.
Engine Monitoring
Engine status is monitored through the
Engine/Warning Display (E/WD), which
displays essential engine and FADEC
information. Information is also available
through the Engine and Cruise page of the SD.
Depending on the engine type and EFIS
generation, the E/WD can have different
layouts. Refer to the EFIS section for more
details. Anyway, the most important engine
information is always displayed on the E/WD.
On this example, N1, EGT, N2 and Fuel Flow
are displayed. In addition, FADEC information
is displayed: the mode, which depends on the
thrust lever detent, and the max N1 that
depends on this mode.
In addition, engine information is displayed on
the ENG page :
1. Fuel used by each engine since last
startup.
2. Oil quantity, in quarts
3. Oil pressure, in Pound per Square Inch (PSI)
4. Oil temperature
5. Vibration on the first compressor stage
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Airbus_Pilots Guide_UK空客飞行员指南(31)
