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┃ A~7-~'M" A321 ┃ CONTENTS ┃SEQ 001 ┃REV 30 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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45.00 CONTENTS
45.10 DESCRIPTION
- GENERAL
- COMPONENTS
-MODES OF OPERATION . .
- ARCHITECTURE
- FAILURE CLASSIFICATION .
-FUNCTIONS OF CFDS
- COCKPIT / CFDS INTERFACE
45.20 SYSTEM OPERATION
- MAINTENANCE MENU
- LAST OR CURRENT LEG REPORT
- LAST OR CURRENT LEG ECAM REPORT
-PREVIOUS LEGS REPORT
- AVIONICS STATUS
- SYSTEM REPORT/TEST
- GMT/DATE INITIALIZATION
-BACK UP MODE
-ACARS PRINT PROGRAM <~
R 45.25 DATA LOADING <~
45.30 PRINTER <~
R 45.40 ELECTRICAL SUPPLY
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┃I -~ A318 ┃MAINTENANCE SYSTEM ┃1.45.10 P 1 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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The purpose of the Centralized Fault Display System (CFDS) is to make the maintenance
task easier by displaying fault messages in the cockpit and permitting the flight crew to
make some specific tests.
There are two levels of maintenance :
at the line stop : removal and replacement of equipment
at the main base : troubleshooting
The CFDS includes :
- the BITE (Built-In Test Equipment) for each electronic system
- a central computer, the Centralized Fault Display Interface Unit (CFDIU)
-two MCDUs (Multipurpose Control and Display Units), used also for FMGS (Flight
Management and Guidance System), AIDS (Aircraft Integrated Data System), and
ACARS (Aircraft Communication And Reporting System, if installed), which work with
the CFDIU to display information or initiate tests
- one printer.
If a main channel of the CFDIU fails, the backup channel takes over.
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本文鏈接地址:
AIRBUS A320 Flight Crew Operating Manual5(31)