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PEDESTAL..........................................................................................................................................................1/2
DSC-31-60-30 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)
DESCRIPTION.................................................................................................................................................... 1/2
CONTROLS ON PEDESTAL..............................................................................................................................2/2
DSC-31-75 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-31-80 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - INTRODUCTION
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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
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - INTRODUCTION
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FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - COCKPIT ARRANGEMENT
A330/A340 FLEET DSC-31-05-20 P 1/2
FCOM 19 AUG 10
COCKPIT ARRANGEMENT
Applicable to: ALL
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - COCKPIT ARRANGEMENT
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FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - ARCHITECTURE
A330/A340 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: ,
The instrument panels have six identical units.
These DUs are full-color Liquid Crystal Displays (LCD).
DISPLAY MANAGEMENT COMPUTER (DMC)
Applicable to: ALL
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, and is able to
drive simultaneously one PFD, one ND, and either of the ECAMs in its engine warning or system
status task.
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.
‐ through the SDACs to generate amber cautions.
The ECAM display units display the alert messages generated by the FWCs.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING/RECORDING
EIS GENERAL - ARCHITECTURE
A330/A340 FLEET DSC-31-05-30 P 2/4
FCOM 19 AUG 10
The FWCs also generate :
‐ radio altitude callouts.
‐ decision height callouts.
‐ landing speed increments.
ATTENTION-GETTERS
Applicable to: ALL
The FWCs also drive the attention-getters. Each pilot has a set of these on the panel under the
glareshield. They are :
‐ a master warning light that flashes “MASTER WARN” in red for red warnings
　
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