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UF94200
EFFECTIVITY Page 305
ALL
CFDS: CFDS REPORTS
PFR FILTER PROGRAM
The purpose of this function is to improve the
operational use of the POST FLIGHT REPORT (PFR) by
filtering all the spurious or injustified
failures/messages.
It concerns the PFR printed at the end of the flight
as well as the real-time failure and warning
information transmitted by the ATSU.
Filter Activated
The filter data base is activated after correct
uploading. It can be deactivated then activated again
through the 2L line key.
This data base is a copy of the SIL (Service Information
Letter) 0028 under diskette form. It must be
periodically updated.
Print Filter Content
This function enables printing of the maintenance
filter data base.
TMUCFDR03-T15 LEVEL 1
EFFECTIVITY 31-32-00 Page 30
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 306
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CFDS: CFDS REPORTS - PFR FILTER PROGRAM
TMUCFDR03-P15 LEVEL 1
EFFECTIVITY 31-32-00 Page 31
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 307
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SELF EXAMINATION
Which Centralized Fault Display System functions
are available in flight?
A - LAST LEG REPORT and LAST LEG ECAM REPORT.
B - AVIONICS STATUS, LAST LEG REPORT, SYSTEM
REPORT/TEST.
C - CURRENT LEG REPORT, CURRENT LEG ECAM
REPORT.
When you make a print of the PREVIOUS LEGS REPORT?
A - You print only the page displayed on the
Mutipurpose Control and
Display Unit, even if the report
contains several pages.
B - You print all the report, even if it
contains several pages.
C - You print the sum of the failure data
delivered by the BITEs and the
warning messages delivered by the ECAM.
Which Centralized Fault Display System functions
are available in BACK-UP mode, on ground?
A - None.
B - SYSTEM REPORT/TEST for main systems.
C - LAST LEG REPORT and LAST LEG ECAM REPORT.
TMUCFDR03 LEVEL 1
EFFECTIVITY 31-32-00 Page 32
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 308
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31 - INDICATING/RECORDING SYSTEMS
31-32-00 CFDS: CFDS PHASES
CONTENTS:
Ground/Flight Transition
"In Flight" Phase
Flight/Ground Transition
"On Ground" Phase
Self Examination
TMUCFDY02 LEVEL 2
EFFECTIVITY 31-32-00 Page 1
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 309
ALL
CFDS: CFDS PHASES
GROUND/FLIGHT TRANSITION
Transition to flight (Event "1") is defined "at the
soonest" or "at the latest" depending on whether the
flight number has been entered by the crew before
take-off or not.
Event "1":
- "At the soonest": First engine start + 3 minutes
if flight number entered prior to first engine
start.
- "At the latest": Aircraft speed > 80 knots if
flight number not entered prior to first engine
start.
At event "1", the leg number is incremented.
"IN FLIGHT" PHASE
From event "1" until aircraft speed has been below 80
knots for 30 seconds, type 1 and 3 systems are
considered in flight.
NOTE: Type 2 systems are only considered in flight
from 30 seconds after lift off up to touch down.
In flight, the system Built-In Test Equipment (BITEs)
ensures:
- detection (Type 1/2/3 systems) and memorization
in their flight memory (Type 1/2 systems only
as type 3 system BITEs do not have any memory)
of internal and external faults,
- transmission to the Centralized Fault Display
Interface Unit (CFDIU) of internal and external
faults for memorization and establishment of
the CURRENT LEG REPORT.
This "in flight" phase corresponds to the Post Flight
Report (PFR) recording time (Beginning and end of fault
and ECAM warning message memorization in the CFDIU).
FLIGHT/GROUND TRANSITION
Transition to ground occurs when, after touch down,
the aircraft speed has been below 80 knots for 30
seconds.
At this time, the CURRENT LEG REPORT is renamed under
the title LAST LEG REPORT and is stored in the PREVIOUS
LEGS REPORT.
NOTE: As the leg has not changed, the content of the
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ATA 31 INDICATING AND RECORDING SYSTEM(38)