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heading.
NOTE: The calibration of the compass must be done after
the radio receivers are switched on.
TMUADIJ01-T02 LEVEL 3
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STANDBY INSTRUMENT COMPONENTS - COMPASS
TMUADIJ01-P02 LEVEL 3
EFFECTIVITY 34-20-00 Page 5
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STANDBY INSTRUMENT COMPONENTS
HORIZON INDICATOR
IDENTIFICATION
FIN: 7FN
LOCATION:
ZONE: 211
COMPONENT DESCRIPTION
The gyroscopic horizon, installed on the center
instrument panel, is an independent instrument which
provides the crew with a constant indication of the
aircraft’s attitude.
VOR/DME RMI
IDENTIFICATION
FIN: 11FN
LOCATION:
ZONE: 211
COMPONENT DESCRIPTION
The VOR/DME Radio Magnetic Indicator (VOR/DME RMI)
installed on the center instrument panel, uses digital
ARINC 429 type inputs.
It receives parameters from ADIRUs, VORs and DMEs for
the display of:
- Magnetic or true heading,
- VOR bearings,
- DME distances.
TMUADIJ01-T03 LEVEL 3
EFFECTIVITY 34-20-00 Page 6
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STANDBY INSTRUMENT COMPONENTS - HORIZON INDICATOR - VOR/DME RMI
TMUADIJ01-P03 LEVEL 3
EFFECTIVITY 34-20-00 Page 7
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STANDBY INSTRUMENT COMPONENTS
METRIC ALTIMETER (OPTION)
IDENTIFICATION
FIN: 15FN
LOCATION
ZONE: 211
DESCRIPTION
The metric altimeter is supplied with static pressure
by the standby air data to indicate the barometric
altitude of the aircraft in meters.
An integral lighting with external 5VAC is provided
to illuminate the instrument.
VOR/ADF/DME RMI (OPTION)
IDENTIFICATION
FIN: 21FN
LOCATION:
ZONE: 211
DESCRIPTION
The VOR/ADF/DME Radio Magnetic Indicator (VOR/ADF/DME
RMI) installed on the center instrument panel, uses
digital ARINC 429 type inputs.
It receives parameters from ADIRUs, VORs, ADFs and
DMEs for the display of:
- Magnetic or true heading,
- VOR bearings,
- ADF bearings,
- DME distances.
TMUADIJ01-T04 LEVEL 3
EFFECTIVITY 34-20-00 Page 8
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 144
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STANDBY INSTRUMENT COMPONENTS - METRIC ALTIMETER AND VOR/ADF/DME RMI (OPTIONS)
TMUADIJ01-P04 LEVEL 3
EFFECTIVITY 34-20-00 Page 9
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EFFECTIVITY Page 145
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STANDBY INSTRUMENT COMPONENTS
ADF/RMI (OPTION)
IDENTIFICATION
FIN: 13FN
LOCATION:
ZONE: 211
COMPONENT DESCRIPTION
The ADF Radio Magnetic Indicator (ADF/RMI) installed
on the center instrument panel, uses digital ARINC 429
type inputs.
It receives parameters from ADIRUs and ADFs for the
display of:
- Magnetic or true heading,
- ADF bearings.
TMUADIJ01-T05 LEVEL 3
EFFECTIVITY 34-20-00 Page 10
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 146
ALL
STANDBY INSTRUMENT COMPONENTS - ADF/RMI (OPTION)
TMUADIJ01-P05 LEVEL 3
EFFECTIVITY 34-20-00 Page 11
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MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUADIJ01 LEVEL 3
EFFECTIVITY 34-20-00 Page 12
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34 - NAVIGATION
34-10-00 ADIRS COMPONENTS
CONTENTS:
Air Data Module
AOA Sensors
Static Probes
TAT Sensors
Pitot Probes
ADIRS CDU
ADIRUs
VMO/MMO Switch
TMUADIO03 LEVEL 3
EFFECTIVITY 34-10-00 Page 1
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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