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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.
MODES OF OPERATION
Applicable to: ALL
The CFDS operates in two main modes :
‐ the NORMAL mode or REPORTING mode (in flight)
‐ the INTERACTIVE mode or MENU mode (on ground).
In NORMAL mode, the CFDS records and displays the failure messages transmitted by each system
BITE.
In INTERACTIVE mode, the CFDS allows any BITE to be connected with the MCDU in order to
display the maintenance data stored and formatted by the BITE or to initiate a test.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 2/8
FCOM 19 AUG 10
ARCHITECTURE
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 3/8
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 4/8
FCOM 19 AUG 10
ARCHITECTURE
Applicable to:
,
,
MSN,,,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 5/8
FCOM 19 AUG 10
FAILURE/FAULT CLASSIFICATION
Applicable to: ALL
The Centralized Fault Display System (CFDS) identifies the faulty system and puts any failures or
faults into one of three classes :
Class 1 : Failures indicated to the flight crew by means of the ECAM, or other flight deck effect.
They must be repaired or entered in the MEL (Minimum Equipment List) before the
aircraft can depart.
Class 2 : Faults indicated to maintenance personnel by the CFDS and which trigger a MAINT
status entry on the maintenance part of the ECAM status page. The aircraft can
operate with these faults, but they must be repaired within 10 days.
Class 3 : Faults indicated to maintenance personnel by the CFDS, but which do not trigger a
MAINT status. The operator may have these faults corrected at his convenience.
Failure/fault classes Class 1 Class 2 Class 3
Operational
consequences
YES NO NO
Indication to the flight
crew
YES
Automatically displayed
Warning ‐ or caution messages on
Engine
Warning Display
‐ Flag or indication in the flight
deck.
YES
Available on ECAM status
page.
NO
Dispatch consequences Refer to MEL may be :
"GO"
"GO IF"
"NO GO"
No need to refer to MEL
except for the messages
‐ AIR BLEED
For all the other class 2
messages, "GO" without
conditions.
Can be left uncorrected for
10 days.
MEL not applicable
Indication to the
maintenance team
YES
Automatically print out at the end of each flight :
Fault messages on the CFDS Post Flight Report.
YES
Available on request through
system report/Test
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 6/8
FCOM 19 AUG 10
FUNCTIONS OF THE CENTRALIZED FAULT DISPLAY SYSTEM (CFDS)
Applicable to:
The main functions of the CFDS are :
obtaining and storing messages transmitted by the connected ‐ system BITEs, or by the Flight
Warning Computer (Warning and Caution titles)
‐ Detailing the maintenance phases.
‐ Presenting maintenance reports :
• Last leg report
• Last leg ECAM report
• Previous leg report
• Avionics status
• System report test
• Post-flight report.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
MAINTENANCE SYSTEM
DESCRIPTION
A318/A319/A320/A321 FLEET DSC-45-10 P 7/8
FCOM 19 AUG 10
FUNCTIONS OF THE CENTRALIZED FAULT DISPLAY SYSTEM (CFDS)
Applicable to:
,
,
MSN,,,,
The main functions of the CFDS are :
‐ obtaining and storing messages transmitted by the connected system BITEs, or by the Flight
Warning Computer (Warning and Caution titles)
‐ Detailing the maintenance phases.
‐ Presenting maintenance reports :
• Last leg report
• Last leg ECAM report
• Previous leg report
• Avionics status
• System report test
• Post-flight report.
　
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