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FCOM 19 AUG 10
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET DSC-45-PLP-TOC P 1/2
FCOM 19 AUG 10
DSC-45-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-45-10 DESCRIPTION
GENERAL............................................................................................................................................................1/8
COMPONENTS...................................................................................................................................................1/8
MODES OF OPERATION...................................................................................................................................1/8
ARCHITECTURE.................................................................................................................................................2/8
FAILURE/FAULT CLASSIFICATION.................................................................................................................. 5/8
FUNCTIONS OF THE CENTRALIZED FAULT DISPLAY SYSTEM (CFDS)....................................................... 6/8
COCKPIT/CFDS INTERFACE............................................................................................................................ 8/8
DSC-45-20 SYSTEM OPERATION
MAINTENANCE MENU.....................................................................................................................................1/16
LAST (OR CURRENT) LEG REPORT...............................................................................................................4/16
LAST (or CURRENT) LEG ECAM REPORT......................................................................................................5/16
PREVIOUS LEGS REPORT.............................................................................................................................8/16
AVIONICS STATUS..........................................................................................................................................9/16
SYSTEM REPORT/TEST................................................................................................................................. 9/16
GMT/DATE INITIALIZATION...........................................................................................................................11/16
BACK UP MODE............................................................................................................................................ 13/16
DSC-45-25 DATA LOADING
GENERAL............................................................................................................................................................1/2
DATA LOADING SELECTOR ON THE OVERHEAD PANEL..............................................................................1/2
DSC-45-30 PRINTER
GENERAL............................................................................................................................................................1/2
SYSTEM DESCRIPTION....................................................................................................................................1/2
DSC-45-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-45-PLP-TOC P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 1/8
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
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
COMPONENTS
Applicable to: ALL
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
　
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