曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
blue until the corresponding action is
taken. They are shown in green if the item
status is correct.
The takeoff checklist shows the autobrakes, the signs
(seat belts/no smoking) and the flaps are correctly
set for takeoff, but the spoilers should be armed and
the takeoff config should be checked prior to takeoff.
7. Status message area : Like for the warning/
alert messages, their color depends on the
message severity. The only exceptions are
the takeoff and landing inhibit messages,
which are displayed in magenta. These
messages indicate that low severity alerts
are inhibited during takeoff and landing to
avoid catching the attention of the crew
during these critical flight phases.
SD – SYSTEM DISPLAY
The content of this EFIS depends on the ECAM
Control Panel located on the pedestal. If no
page is selected on the ECAM CP, the page
displayed on the SD is automatically selected
according to the flight phase and possible
alerts. The system automatically displays the
right page at the right time.
Whatever page is displayed, the SD also shows
common information in the bottom part of the
screen.
1. TAT : Total Air Temperature, in °C
2. SAT : Saturated Air Temperature, in °C
3. Clock (UTC time)
4. GW : Gross Weight, in kg or lbs (depending
on the unit system selected on the
configuration page). The gross weight is
computed by the FMGC according to the
data entered in the MCDU INIT pages. If no
data was entered, the FMGC is unable to
calculate the gross weight and amber XX is
shown.
For information, all the SD pages are shown here.
They are detailed in the aircraft system section.
Air Conditioning Page APU Page
EFIS
Airbus Series Vol.1
46 For Microsoft Flight Simulator use only. Not for use in real aviation.
Air Bleed Page Cabin Pressure Page
Door Page Electricity Page
Engine Page Flight Controls Page
Fuel Page Hydraulics Page
Wheel Page
EFIS
Airbus Series Vol.1
(c) 2007 Wilco Publishing www.wilcopub.com - www.FeelThere.com 47
Airbus Series Vol.1
48 For Microsoft Flight Simulator use only. Not for use in real aviation.
SYSTEMS
This section describes the aircraft systems.
Most of them are controlled trough the
overhead panel and can be monitored on the
various SD pages.
You should always keep in mind that this
aircraft is based on the “dark cockpit”
philosophy. It means that when no light is on,
everything is all right.
ECAM CONTROL PANEL
The SD EFIS is here to provide information
about the aircraft systems. The SD page to
display is automatically selected when
needed. For example, when the crew starts
the APU, the APU page is automatically
displayed during the starting sequence.
If the crew wants to display a page at any time,
the ECAM control panel should be used. It is
located on the upper part of the pedestal. It
provides one key for each page. If the pilot
presses a key, the associated light turns on and
the corresponding page is displayed on the SD.
To give the control back to the system, the pilot
can press the same key again. The light then
turns off, which means the system will
automatically select the appropriate page
when necessary.
1. TO CONFIG : This button is used to check the
takeoff configuration prior to departure. It
checks some elements of the aircraft configuration
to make sure everything is OK for
takeoff.
2. ENG : The engine page displays
information about the engines.
3. BLEED : This page shows information
about the air bleed system.
4. PRESS : This page displays information
about the cabin pressurization system.
5. ELEC : The electricity page shows the
aircraft electric circuit.
6. HYD : This page displays the hydraulic
system.
7. FUEL : The fuel page shows the fuel
information and all the aircraft fuel tanks.
8. APU : This page shows information about
the APU.
9. COND : Shows information about air
conditioning.
10. DOOR : This page shows the aircraft door
status.
11. WHEEL : This page shows the wheel and
brake status.
12. F/CTL : The flight control page shows the
position of all the flight controls and the
flight control computer status.
13. STS : The status page shows the current
failure status.
ELECTRICITY
The electricity circuit can be controlled from
the overhead ELEC section.
1.2.Battery switches. They are dark when
batteries are on (default). The battery
voltage is displayed next to each switch.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
航空资料4(86)
