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EFFECTIVITY 34-10-00 Page 10
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 518
ALL
TMUADIL04-P05 LEVEL 3
ADIRS/CFDS SPECIFIC PAGES PRESENTATION (ADR INPUT STATUS)
EFFECTIVITY 34-10-00 Page 11
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 519
ALL
ADIRS/CFDS SPECIFIC PAGES PRESENTATION
IR SYSTEM TEST
When the SYSTEM TEST line select key is pressed in, a
complete test of the IR system is activated (power-up
and continuous BITE tests).
When a fault is detected by the system, during the
test, the failure data will be listed on the MCDU in
the same way as trouble shooting data page (HEX
coding).
NOTE: A lockout display is presented in case of a
disagreement between ground information from
CFDIU and ADIRU when the TEST mode is addressed
(with TAS or Inertial GS > or = 100 Kts).
TMUADIL04-T06 LEVEL 3
EFFECTIVITY 34-10-00 Page 12
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 520
ALL
TMUADIL04-P06 LEVEL 3
ADIRS/CFDS SPECIFIC PAGES PRESENTATION (IR SYSTEM TEST)
EFFECTIVITY 34-10-00 Page 13
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 521
ALL
ADIRS/CFDS SPECIFIC PAGES PRESENTATION
IR INTERFACE TEST
When the test input command to the ADIRU is
activated, a sequence is initiated which simulates
an actual flight state of the ADIRU.
The IR will provide calibrated test values to the
instruments.
This checks the computer, the transmission and the
display of inertial reference parameters.
The test mode is inhibited whenever any of the
following conditions exist:
- Ground speed > or = 20 Kts
- IR in ATT mode.
Test sequence:
- 0 to 2 seconds: Output set to functional test,
annunciator discretes energized (see table).
- After 2 seconds: Output set to functional
test, annunciator discretes released to
normal status (see table).
TMUADIL04-T07 LEVEL 3
EFFECTIVITY 34-10-00 Page 14
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 522
ALL
TMUADIL04-P07 LEVEL 3
ADIRS/CFDS SPECIFIC PAGES PRESENTATION (IR INTERFACE TEST)
EFFECTIVITY 34-10-00 Page 15
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 523
ALL
ADIRS/CFDS SPECIFIC PAGES PRESENTATION
IR GROUND REPORT
When the GROUND REPORT line select key is pressed in,
it reports all internal faults detected since the last
landing.
TMUADIL04-T08 LEVEL 3
EFFECTIVITY 34-10-00 Page 16
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 524
ALL
TMUADIL04-P08 LEVEL 3
ADIRS/CFDS SPECIFIC PAGES PRESENTATION (IR GROUND REPORT)
EFFECTIVITY 34-10-00 Page 17
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 525
ALL
ADIRS/CFDS SPECIFIC PAGES PRESENTATION
IR INPUTS STATUS
When the INPUT STATUS line select key is pressed in,
it describes the current state of the selected IR
inputs (discrete, analog and ARINC inputs).
Example on the INPUT STATUS page 4/6, ARINC input value
from the Control Display Unit (CDU):
- The SET LAT, SET LONG and SET HEADING
displayed values are copies of data
received from each of the listed signal
sources (here the CDU).
The latitude and the longitude inputs are
processed during the ALIGN mode, the
heading input is processed during the ATT
mode.
These displayed data are latched as display
values until new valid source data is
received from each signal source.
In case of invalid inputs dashes (-----)
are displayed.
TMUADIL04-T09 LEVEL 3
EFFECTIVITY 34-10-00 Page 18
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 526
ALL
ADR SELF TEST VALUES (IR INPUT STATUS)
TMUADIL04-P09 LEVEL 3
EFFECTIVITY 34-10-00 Page 19
　
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