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The DCUs process flight and operating parameter data for transfer and storage to the flight data recorder. The DCUs also process and transfer fault data for the maintenance diagnostic computer.
The DCUs receive information from the major systems and subsystems including:
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Bleed Air;
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Air conditioning;
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Ice and Rain;
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Electrical Power;
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Fire Protection;
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Flight Controls;
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Fuel;
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Hydraulics;
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Landing Gear;
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Lights;
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Oxygen;
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Engine;
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Auxiliary Power Unit;
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Doors; and
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Avionic Systems.
AURAL/VISUAL WARNING SYSTEM Description Vol. 2 03.10.5
Oct 05/06
Lamp Driver Unit
The dual-channel lamp driver unit (LDU) is used to power individual panel and glareshield lights when commanded by the data concentrator units. When the DCU generates an EICAS warning or caution message, the LDU causes the glareshield MASTER WARNING/CAUTION switch/lights to flash, and turns on any associated panel lights.
Cursor Control Panel
Each pilot is provided with a cursor control panel (CCP), located on the center pedestal. Each CCP is the pilot’s main interface to control information presented on the on-side MFD.
The CCP can be divided into 5 functional and visually identifiable sections as described below:
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MFD window formatting – allows selection of navigation formats, display and control of on-screen menus and to enable overlays;
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Memory keys – allows the crew to save specific display formats to memory for quick access;
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Chart control – displays charts from the optional chart system;
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EICAS control – enables the display of synoptic, SUMMARY pages and controls the display of crew alerting messages; and
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Radio tuning – controls communications and navigation radio tuning.
AURAL/VISUAL WARNING SYSTEM Description Vol. 2 03.10.6
Oct 05/06
Cursor Control Panel Figure 03.10.4
Reversionary Control Panel
The multipurpose reversionary control panel, located on the center pedestal, includes several rotary selectors and switch/lights. The functions are as follows:
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TUNE INHIBIT PUSH switch/lights – used to inhibit the tuning functions of a CDU or MFD (see Chapter 6, Communications)
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L(R) DISPLAYS selector – used to control the reversionary functions of the left (right) PFD and MFD
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EICAS selector – used to control the location of the displayed EICAS information
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ADC selector – used to define the source of air data information (see Chapter 11, Flight Instruments)
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