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Fire Extinguisher Pressure),
- SLIDE BOTTLE PRESSURE,
- DOORS BOTTLE PRESSURE,
- DRAINMASTS,
- DOORS CLOSED/SLIDES ARMED STATUS.
NOTE : If an optional system/function is not requested
by the customer, it will not be monitored or
shown on the display.
MAINTENANCE
The MAINTENANCE page allows access to the following
items (identical to CFDS SYSTEM REPORT/TEST concerning
the CIDS) :
- LAST LEG REPORT,
- PREVIOUS LEGS REPORT,
- LRU IDENTIFICATION,
- FAULT DATA,
- CLASS 3 FAULTS,
- GROUND SCAN
In flight, only the "CURRENT LEG REPORT" item is
displayed and available.
TMUCI2X02-T02 LEVEL 3
EFFECTIVITY 23-73-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 336
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PTP UTILIZATION (STATUS)
TMUCI2X02-P02 LEVEL 3
EFFECTIVITY 23-73-00 Page 5
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 337
ALL
PTP UTILIZATION (STATUS AND TEST)
LAST LEG REPORT
This display presents the LAST/CURRENT LEG REPORT,
with the date and time of the failure occurence, the
ATA chapter and the name of the failed unit. It contains
class 1+2 failures
PREV LEGS REPORT
This display presents the previous legs. It contains
class 1+2 failures.
The various failed units can be :
- DIRECTOR 1,
- DIRECTOR 2,
- DEU A,
- DEU B,
- CIDS TOP BUS,
- CIDS MID BUS,
- PROG. AND TEST PNL,
- FWD ATTND PNL,
- SDAC 1+2,
- CFDIU.
- EPSUs,
- SDCU CHANNEL 1+2,
- CABIN ASSIGNMENT MODULE,
NOTE : The PREV LEG report contains the fault
information of the last 64 flight legs and
includes the date, time and ATA chapter.
LRU IDENTIFICATION
The Part Number of the relevant unit is displayed.
TMUCI2X02-T03 LEVEL 3
EFFECTIVITY 23-73-00 Page 6
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 338
ALL
PTP UTILIZATION (STATUS)
TMUCI2X02-P03 LEVEL 3
EFFECTIVITY 23-73-00 Page 7
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 339
ALL
PTP UTILIZATION (STATUS AND TEST)
FAULT DATA
This display contains the same DATA as "TROUBLE
SHOOTING DATA" when using the MCDU with the CFDS.
It shows :
- The date,
- the leg number,
- the hour,
- the number of occurences,
- a 6 digit code which gives a more precise
failure identification.
For example, code 240A07 means DEU A 200RH07 discrete
output or wiring connection pin J2-2.
NOTE : Present failures are marked with "LEG 03".
CLASS 3 FAULTS
This display presents class 3 fault messages from the
following items :
- CFDIU,
- SDCU CHANNEL 1,
- SDCU CHANNEL 2,
- SDAC 1,
- SIGN LAMP,
- CALL LAMP,
- ATTND INDICATION PANEL,
- ADD ATTND PANEL,
- ANNOUNCEMENT REPRODUCER,
- READING LIGHT
- READING LIGHT PCB,
- POWER READING LIGHT PCB,
- WORK LIGHT FWD, MID, AFT,
- WORK LIGHT PCB FWD, MID,
- POWER PCB FWD, MID, AFT,
- PES MUX,
- ANNOUCEMENT REPRODUCER,
- VIDEO SYSTEM.
PCB = Printed Circuit Board.
GROUND SCAN
The GND SCAN indicates all class 1 and 2 failures which
are present on ground.
For the continuously monitored systems, the ground
memory will be updated when the failure has been
cancelled.
For non-monitored systems, the update will occur after
a director power-on or after a test activation via the
PTP or MCDU.
TMUCI2X02-T04 LEVEL 3
EFFECTIVITY 23-73-00 Page 8
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 340
ALL
PTP UTILIZATION (STATUS)
TMUCI2X02-P04 LEVEL 3
EFFECTIVITY 23-73-00 Page 9
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 341
ALL
PTP UTILIZATION (STATUS AND TEST)
SYSTEM TEST
The SYSTEM TEST function allows the following units
to be tested on ground only :
- ACTIVE DIRECTOR,
- CIDS BUS,
- DEU A,
- DEU B,
- CAM,
- PROG AND TEST PNL,
- FWD ATTND PNL,
　
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