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Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
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TMUADIL04 LEVEL 3
EFFECTIVITY 34-10-00 Page 20
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 528
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TMUADIL04-P10 LEVEL 3
ADR SELF TEST VALUES (OUTPUT BINARY WORD)(1/2)
EFFECTIVITY 34-10-00 Page 21
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
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ADR SELF TEST VALUES (2/2)
TMUADIL04-P11 LEVEL 3
EFFECTIVITY 34-10-00 Page 22
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 530
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IR SELF TEST VALUES (1/2)
TMUADIL04-P12 LEVEL 3
EFFECTIVITY 34-10-00 Page 23
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 531
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IR SELF TEST VALUES (2/2)
TMUADIL04-P13 LEVEL 3
EFFECTIVITY 34-10-00 Page 24
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 532
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34 - NAVIGATION
34-42-00 RADIO ALTIMETER/CFDS SPECIFIC
PAGE PRESENTATION
CONTENTS:
General
LRRA ARINC Test
LRRA RAMP Test
TMURADE02 LEVEL 3
EFFECTIVITY 34-42-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 533
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RADIO ALTIMETER/CFDS SPECIFIC PAGE PRESENTATION
GENERAL
The RA is a type 1 system.
The RA system is not available in CFDS back-up mode.
LRRA ARINC TEST
During the ARINC TEST, an integrity test is performed,
the antena circuit and the CFDIU input data are tested.
This test is performed after a Removal/Installation
of a Radio Altimeter antenna or transceiver.
During the test (0.8 second), observe the following
indications on the CAPT PFD:
- the bottom sector line moves down from the
horizon line.
- the radio altitude value indicates 40 ft.
If no failure, at the end of the test, NO FAILURE
DETECTED message appears on the MCDU.
LRRA RAMP TEST
The RAMP TEST tests the complete Radio Altimetric
chain.
A start altitude, a stop altitude and a slope must be
entered prior to triggering the test.
Then, the line key adjacent to TRIGGER has to be
pressed.
Observe on the CAPT PFD that:
- Radio Altitude starts from the entered value,
0 ft in this example, then increases at a
constant rate of 25 ft/s until reaching the
Stop Altitude of 2500 ft. Also notice the
movement of the red ribbon and the lower line
of the attitude sphere on the PFD.
NOTE: The REPLAY line key restarts the test.
The CONTINUE line key continues the RAMP TEST
if it was interrupted before the end.
TMURADE02-T01 LEVEL 3
EFFECTIVITY 34-42-00 Page 2
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 534
ALL
RADIO ALTIMETER/CFDS SPECIFIC PAGE PRESENTATION
TMURADE02-P01 LEVEL 3
EFFECTIVITY 34-42-00 Page 3
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 535
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TMURADE02 LEVEL 3
EFFECTIVITY 34-42-00 Page 4
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 536
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