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TCAS Fault
GPWS Fault
GPWS TERR DET Fault
GPS Fault
FM/GPS POS DISAGREE
TMUWARN01 LEVEL 3
EFFECTIVITY 34-00-00 Page 1
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 503
ALL
ECAM WARNINGS
GENERAL
Note: There are no dedicated ECAM pages for the
navigation system.
In case of a NAV FAULT, there will be no system
page called for the corresponding failure.
ILS FAULT
This warning is triggered in case of an ILS1 (or 2 or
ILS1+2) receiver failure (LOC and G/S parts).
In case of failure of one ILS receiver, the landing
capability is limited to CAT1 (CAT1 inoperative when
both receivers have failed).
PRED W/S FAULT
This warning is triggered in case of a detected
windshear fault.
RA FAULT
This warning is triggered in case of an RA1 (or 2 or
RA1+2) failure.
In case of failure of both RAs, the landing capability
is limited to CAT1.
When only one RA has failed, no local warnings are
shown but CAT3 is inoperative.
TCAS FAULT
This warning is triggered in case of a TCAS internal
failure.
TMUWARN01-T01 LEVEL 3
EFFECTIVITY 34-00-00 Page 2
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 504
ALL
ECAM WARNINGS
TMUWARN01-P01 LEVEL 3
EFFECTIVITY 34-00-00 Page 3
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 505
ALL
ECAM WARNINGS
GPWS FAULT
This warning is triggered in case of a GPWS failure.
Notice the amber FAULT light on the GPWS control panel.
NOTE: In case of ILS1 failure, only mode 5 is inhibited,
consequently the FAULT light does not come on
and the GPWS FAULT message is not triggered.
GPWS TERR DET FAULT
This warning is triggered in case of terrain detection
failure as well as the amber TERR FAULT light on the
GPWS control panel.
GPS FAULT
This warning is triggered in case of a GPS1 (or 2 or
1+2) failure.
FM/GPS POSITION DISAGREE
When latitude or longitude from either GPSSU1 or 2
deviates more than 0.5 Nm the amber NAV FM/GPS POS
DISAGREE is triggered.
TMUWARN01-T02 LEVEL 3
EFFECTIVITY 34-00-00 Page 4
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 506
ALL
ECAM WARNINGS
TMUWARN01-P02 LEVEL 3
EFFECTIVITY 34-00-00 Page 5
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 507
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUWARN01 LEVEL 3
EFFECTIVITY 34-00-00 Page 6
Jun 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 508
ALL
34 - NAVIGATION
34-10-00 ADIRS/CFDS SPECIFIC PAGES
PRESENTATION
CONTENTS:
General
ADR SYSTEM TEST
ADR OUTPUT TESTS
ADR GROUND REPORT
ADR INPUT STATUS
IR SYSTEM TEST
IR INTERFACE TEST
IR GROUND REPORT
IR INPUT STATUS
ADR Self Test Values
IR Self Test Values
TMUADIL04 LEVEL 3
EFFECTIVITY 34-10-00 Page 1
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 509
ALL
ADIRS/CFDS SPECIFIC PAGES PRESENTATION
GENERAL
The tests for ADR 1,2 and 3 are identical and the tests
for IR 1,2 and 3 are also identical.
Therefore, we will only see system 1 for each one.
Remember that the ADR and IR are Type 1 systems.
ADR SYSTEM TEST
The activation of the SYSTEM TEST allows the power-up
test and the continuous BITE test resident in the ADIRU
to be repeated (check of the system integrity after
an ADIRU replacement).
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).
TMUADIL04-T01 LEVEL 3
EFFECTIVITY 34-10-00 Page 2
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 510
ALL
TMUADIL04-P01 LEVEL 3
ADIRS/CFDS SPECIFIC PAGES PRESENTATION (ADR SYSTEM TEST)
EFFECTIVITY 34-10-00 Page 3
　
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