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UF94200
EFFECTIVITY Page 296
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CFDS: CFDS REPORTS - SYSTEM REPORT/TEST-GCU EMER (TYPE 3 SYSTEM)
TMUCFDR03-P10 LEVEL 1
EFFECTIVITY 31-32-00 Page 21
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 297
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CFDS: CFDS REPORTS
POST FLIGHT REPORT
The POST FLIGHT REPORT is the sum of the LAST LEG
REPORT and of the LAST LEG ECAM REPORT.
It is only available on the printer.
ECAM WARNINGS display the LAST LEG ECAM REPORT.
FAULT MESSAGES display the LAST LEG REPORT.
TMUCFDR03-T11 LEVEL 1
EFFECTIVITY 31-32-00 Page 22
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 298
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CFDS: CFDS REPORTS - POST FLIGHT REPORT
TMUCFDR03-P11 LEVEL 1
EFFECTIVITY 31-32-00 Page 23
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 299
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CFDS: CFDS REPORTS
GMT/DATE INIT
The GMT/DATE INIT function is available only in case
of clock failure and CFDIU power interrupt.
In normal operation, the CFDIU receives the time from
the clock.
In the event of main clock failure, the CFDIU transmits
the time and the date using its internal clock.
Re initialization of the time and the date will be
only necessary after a power cut-off. It shall be
carried out on MCDU trough the GMT/DATE INIT function.
GMT and date are entered using the scratchpad.
TMUCFDR03-T12 LEVEL 1
EFFECTIVITY 31-32-00 Page 24
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 300
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CFDS: CFDS REPORTS - GMT/DATE INIT
TMUCFDR03-P12 LEVEL 1
EFFECTIVITY 31-32-00 Page 25
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 301
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CFDS: CFDS REPORTS
BACKUP MODE
The BACKUP MODE function is only automatically
displayed in case of CFDIU failure.
It enables access to the functions of the backup
channel.
The BACKUP MODE function is added to the CFDS main
menu in case of minor failure.
If the failure is serious, when the CFDS item is
selected in the MCDU MENU, the CFDS BACKUP MODE is
directly displayed on the MCDU.
In flight, no function is available.
On ground, the only function possible is SYSTEM/REPORT
TEST. This function is available for the main systems
only.
TMUCFDR03-T13 LEVEL 1
EFFECTIVITY 31-32-00 Page 26
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 302
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CFDS: CFDS REPORTS - BACKUP MODE
TMUCFDR03-P13 LEVEL 1
EFFECTIVITY 31-32-00 Page 27
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 303
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CFDS: CFDS REPORTS
ACARS/PRINT PROGRAM
This item allows automatic transmission, via the ATSU,
or printing of the following functions:
- Post Flight Report,
- Real time failures,
- Real time warnings and
- Avionics data.
If "YES" is selected for the send and print columns,
the CFDIU will automatically transmit or print the
Post Flight Report at the end of the flight or the
failures and warnings in real time.
For avionics data, "YES" in the send column, means
that the system pages will be sent to the ground when
the operator requests a print.
A star beside "YES" or "NO" means that these items are
modifiable. The programming of the send column is
provided by the ATSU and the programming of the print
control for the avionics data, is provided by the
system itself.
TMUCFDR03-T14 LEVEL 1
EFFECTIVITY 31-32-00 Page 28
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 304
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CFDS: CFDS REPORTS - ACARS/PRINT PROGRAM
TMUCFDR03-P14 LEVEL 1
EFFECTIVITY 31-32-00 Page 29
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
　
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