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时间:2010-07-29 09:34来源:蓝天飞行翻译 作者:admin
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• Non lights out switch position - White light. If normally the system should
be operating and is deactivated a white OFF light is illuminated. If normally
the system should not be operating and is activated a white ON light is
illuminated.
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ELECTRONIC INSTRUMENT MENU
System presentation 13/32
There are some switches on the overhead panel which are used on a
temporary basis or may have an indication of their state. The logic is;
• Temporary selection for operational reasons - Blue ON light e.g. anti-ice
• Applicable system status - Green light - e.g. APU available.
You will see this philosophy demonstrated throughout the course.
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ELECTRONIC INSTRUMENT MENU
System presentation 14/32
Below the ECAM displays, on the center
pedestal, is the ECAM control panel. The two
controls on the left hand side are to adjust the
brightness of the two ECAM screens or to turn
them off. We will look at the rest of the
controls on this panel in more detail later.
ELECTRONIC INSTRUMENT MENU
System presentation 15/32
Just below the ECAM screens, on the pedestal, is a switching panel for
use in abnormal situations to restore data to the EFIS and ECAM displays.
You will use this panel in the EIS Reconfiguration module.
ELECTRONIC INSTRUMENT MENU
System presentation 16/32
In front of each pilot there are two attention
getters, a red MASTER WARNING, and an
amber MASTER CAUTION. As a further means
of getting the pilots attention, there is a
loudspeaker on each side of the cockpit for
aural alerts and voice messages.
Note; The loudspeakers can also be used to
listen to ATC and the intercom.
ELECTRONIC INSTRUMENT MENU
System presentation 17/32
ADIRS DATA
DMC1 DMC3 DMC2
NAV DATA
Now, let’s go back to the EFIS system.
For the EFIS displays, data from the Air
Data and Inertial Reference System
(ADIRS) plus Navigation data from the
Flight Management and Guidance System
(FMGS) is fed directly to three Display
Management Computers (DMC).
ELECTRONIC INSTRUMENT MENU
System presentation 18/32
ADIRS DATA NAV DATA
The three identical DMC process the data
and generate the images to be displayed.
Under Normal circumstances:
• DMC1 supplies EFIS information to the
Captains’ PFD and ND
• DMC2 supplies the First Officers’ PFD
and ND.
• DMC3 is available as a backup.
You will see the use of DMC3 in the
abnormal operation module.
BACKUP
DMC1 DMC3 DMC2
ELECTRONIC INSTRUMENT MENU
System presentation 19/32
Now, let’s look at the other EIS sub-system,
ECAM, and how the ECAM displays get their
data.
Sensors are fitted throughout the aircraft to
monitor the various systems, including system
controls operated in the flight deck.
AIRCRAFT SYSTEM SENSORS
ELECTRONIC INSTRUMENT MENU
System presentation 20/32
DMC 3
Data for certain
parameters, for example
Fuel Quantity and
Primary Engine
Indications, is routed
directly from the system
sensors to the three
DMC.
Note that there are
separate channels within
each DMC for ECAM and
EFIS.
AIRCRAFT SYSTEM SENSORS
DMC1 DMC3 DMC2
ECAM EFIS
ELECTRONIC INSTRUMENT MENU
System presentation 21/32
AIRCRAFT SYSTEM SENSORS
For the majority of the systems the sensors
supply data to 2 System Data Acquisition
Concentrators (SDAC). The SDAC acquire
system data, process it, and send System page
data to the 3 DMC.
SDAC1 SDAC2
DMC1 DMC3 DMC2
ELECTRONIC INSTRUMENT MENU
System presentation 22/32
AIRCRAFT SYSTEM SENSORS
Normally:
• DMC 1 supplies the E/WD,
• DMC2 supplies the SD,
• DMC 3 is available as a
backup.
SDAC1 SDAC2
DMC1 DMC3 DMC2
BACKUP
ELECTRONIC INSTRUMENT MENU
System presentation 23/32
AIRCRAFT SYSTEM SENSORS
FWC1 SDAC1 SDAC2 FWC2
DMC1 DMC3 DMC2
Two identical Flight Warning
Computers (FWC) receive data from:
• the aircraft system sensors to
generate red Warnings,
• the SDAC to generate amber
Cautions.
ELECTRONIC INSTRUMENT MENU
System presentation 24/32
AIRCRAFT SYSTEM SENSORS
FWC1 SDAC1 SDAC2
DMC1 DMC3 DMC2
FWC2
The FWC then supply;
• the DMC for the display of alert
messages,
• the attention getters,
• the loudspeakers for aural alerts and
 
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