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DSC-31-60-30 AIRCRAFT INTEGRATED DATA SYSTEM
DESCRIPTION.................................................................................................................................................... 1/4
CONTROLS ON PEDESTAL..............................................................................................................................2/4
DSC-31-70 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-31-75 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - INTRODUCTION
A318/A319/A320/A321 FLEET DSC-31-05-10 P 1/2
FCOM 19 AUG 10
INTRODUCTION
Applicable to: ALL
The Electronic Instrument System (EIS) presents data on six identical Display Units (DUs):
The Electronic Flight Instrument System (EFIS) displays mostly ‐ flight parameters and navigation
data on the Primary Flight Displays (PFDs) and Navigation Displays (NDs).
‐ The Electronic Centralized Aircraft Monitor (ECAM) presents data on the Engine/Warning Display
(E/WD) and System Display (SD) :
• Primary engine indications, fuel quantity, flap and slat position
• Warning and caution alerts, or memos
• Synoptic diagrams of aircraft systems, and status messages
• Permanent flight data
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - INTRODUCTION
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A318/A319/A320/A321 FLEET DSC-31-05-10 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - COCKPIT ARRANGEMENT
A318/A319/A320/A321 FLEET DSC-31-05-20 P 1/2
FCOM 19 AUG 10
COCKPIT ARRANGEMENT
Applicable to: ALL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - COCKPIT ARRANGEMENT
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A318/A319/A320/A321 FLEET DSC-31-05-20 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - ARCHITECTURE
A318/A319/A320/A321 FLEET DSC-31-05-30 P 1/4
FCOM 19 AUG 10
DISPLAY UNIT (DU)
Applicable to:
The instrument panels have six identical units.
These DUs are full-color cathode ray tubes.
DISPLAY UNIT (DU)
Applicable to:
,
,
MSN,,,,
The instrument panels have six identical units.
These DUs are full-color Liquid Crystal Displays (LCD).
DISPLAY MANAGEMENT COMPUTER (DMC)
Applicable to:
Three identical Display Management Computers acquire and process all the signals received from
sensors and other computers to generate the images to be displayed on the primary flight displays,
navigation displays, engine/warning display, and system display.
Each DMC has two independent channels : An EFIS channel and an ECAM channel. Each DMC is
able to simultaneously drive one PFD, one ND, and either one of the ECAMs in its engine warning or
system status mode.
DISPLAY MANAGEMENT COMPUTER (DMC)
Applicable to:
,
,
MSN,,,,
Three identical Display Management Computers (DMC) acquire data from the different sensors and
computers and send it to the DUs. The DUs generate the adequate images and display them.
Each DMC has two independent channels : An EFIS channel and an ECAM channel. Each DMC is
able to simultaneously drive one PFD, one ND, and either one of the ECAMs in its engine warning or
system status mode.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - ARCHITECTURE
A318/A319/A320/A321 FLEET DSC-31-05-30 P 2/4
FCOM 19 AUG 10
SYSTEM DATA ACQUISITION CONCENTRATOR (SDAC)
Applicable to: ALL
The two identical SDACs acquire data, then generate signals. Some of these signals go to the three
DMCs, which use them to generate displays of system pages and engines parameters. Others go to
the flight warning computers, which use them to generate ECAM messages and aural alerts.
FLIGHT WARNING COMPUTER (FWC)
Applicable to: ALL
The two identical FWCs generate alert messages, memos, aural alerts, and synthetic voice
messages. For this purpose they acquire data :
Directly from aircraft sensors, or systems, ‐ to generate red warnings.
　
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