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NOTE: When GPS mode is active, no VOR/DME/ADF data is
used for navigation.
TMUMMRA01-T04 LEVEL 1
EFFECTIVITY 34-36-00 Page 8
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 166
ALL
TMUMMRA01-P04 LEVEL 1
MMR SYSTEM PRESENTATION - GPS PRINCIPLE - USER SEGMENT
EFFECTIVITY 34-36-00 Page 9
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 167
ALL
MMR SYSTEM PRESENTATION
COMPONENTS
The components are two ILS antennas, 2 GPS antennas
and two MMR units.
The MMR system is also connected to:
- Primary Flight Display (PFD) and Navigation
Display (ND) for display.
- Electronic Flight Instrument System (EFIS)
control unit for display control.
- Flight Management and Guidance Computer (FMGC)
for ILS auto-tuning and GPS position.
- Multipurpose Control Display Units (MCDU) for
ILS manual tuning.
- Captain and First Officer Radio Management
Panels (RMP) for ILS back-up tuning.
- Audio Control Panels (ACP) for ILS audio
signal.
- Air Data and Inertial Reference Unit for
GPIR data.
TMUMMRA01-T05 LEVEL 1
EFFECTIVITY 34-36-00 Page 10
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 168
ALL
MMR SYSTEM PRESENTATION - COMPONENTS
TMUMMRA01-P05 LEVEL 1
EFFECTIVITY 34-36-00 Page 11
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 169
ALL
MMR SYSTEM PRESENTATION
ILS INDICATING
The ILS data appears on the PFD as soon as the ILS
pushbutton switch on the EFIS control panel has been
pressed in and on the ND when ROSE/ILS mode has been
selected.
ILS information is displayed in magenta.
The ILS1 information is displayed on PFD1 and ND2.
The ILS2 information is displayed on PFD2 and ND1.
TMUMMRA01-T06 LEVEL 1
EFFECTIVITY 34-36-00 Page 12
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 170
ALL
MMR SYSTEM PRESENTATION - ILS INDICATING
TMUMMRA01-P06 LEVEL 1
EFFECTIVITY 34-36-00 Page 13
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 171
ALL
MMR SYSTEM PRESENTATION
GPS INDICATING
The GPS data is displayed on the MCDUs and on the NDs.
- GPS data on MCDU (GPS MONITOR page):
* GPS position (Lat, Long)
* True Track
* GPS altitude
* Figure of Merit
* Ground Speed
* Number of satellites tracked
* Mode.
- GPS message on ND:
* Availability of the GPS Primary navigation function.
TMUMMRA01-T07 LEVEL 1
EFFECTIVITY 34-36-00 Page 14
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 172
ALL
TMUMMRA01-P07 LEVEL 1
MMR SYSTEM PRESENTATION - GPS INDICATING
EFFECTIVITY 34-36-00 Page 15
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 173
ALL
SELF EXAMINATION
The satellite orbital planes have an inclination of:
A - 60°.
B - 55° to the Equator.
C - 45° to the Equator.
The control segment is composed of:
A - 3 monitor stations.
B - 5 monitor stations.
C - 4 monitor stations and one master
control station.
TMUMMRA01 LEVEL 1
EFFECTIVITY 34-36-00 Page 16
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 174
ALL
34 - NAVIGATION
34-36-00 MMR DESCRIPTION/OPERATION
CONTENTS:
General
ILS Function
GPS Function
LGCIU
CFDIU
Users
Indicating
Self Examination
TMUMMRC01 LEVEL 3
EFFECTIVITY 34-36-00 Page 1
Nov 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 175
ALL
MMR DESCRIPTION/OPERATION
GENERAL
The Multi Mode Receiver (MMR) system includes:
- 2 MMR units,
- 1 Glide Slope (G/S) antenna,
- 1 Localizer (LOC) antenna,
　
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