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valid.
ILS
Applicable to:
The aircraft has two ILS receivers.
(For tuning instructions, Refer to DSC-34-30-10 GENERAL).
‐ PFD1 and ND2 display ILS1 information.
‐ PFD2 and ND1 display ILS2 information.
‐ The flight crew can display the same ILS information on each PFD by pressing the ILS pushbutton
on the onside EFIS control panel (deviation scales and deviation indexes come on).
‐ The NDs display ILS information, if the flight crew selects the ROSE ILS mode on the EFIS control
panel (Refer to DSC-31-45 ROSE ILS MODE).
ILS
Applicable to:
The aircraft has two ILS receivers. Each ILS receiver is integrated in a modular avionics unit called
MMR (Multi Mode Receiver) (ILS1 receiver in MMR1, ILS2 receiver in MMR2).
(For tuning instructions, Refer to DSC-34-30-10 GENERAL).
‐ PFD1 and ND2 display ILS1 information.
‐ PFD2 and ND1 display ILS2 information.
‐ The flight crew can display the same ILS information on each PFD by pressing the ILS pushbutton
on the onside EFIS control panel (deviation scales and deviation indexes come on).
‐ The NDs display ILS information, if the flight crew selects the ROSE ILS mode on the EFIS control
panel (Refer to DSC-31-45 ROSE ILS MODE).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
NAVIGATION
RADIO NAV - NAVAIDS
A318/A319/A320/A321 FLEET DSC-34-30-20 P 2/4
FCOM 19 AUG 10
ILS
Applicable to:
,
,
MSN,,,,
The aircraft has two ILS receivers. Each ILS receiver is integrated in a modular avionics unit called
MMR (Multi Mode Receiver) (ILS1 receiver in MMR1, ILS2 receiver in MMR2).
(For tuning instructions, Refer to DSC-34-30-10 GENERAL).
PFD1 and ‐ ND2 display ILS1 information.
‐ PFD2 and ND1 display ILS2 information.
‐ The flight crew can put the same ILS information on each PFD by pressing the LS button on the
EFIS control panel (the green bars come on).
‐ The NDs display ILS information, if the flight crew selects the ROSE LS mode on the EFIS control
panel (Refer to DSC-31-45 ROSE ILS MODE).
ADF
Applicable to:
The aircraft has one ADF system.
(For tuning instructions, Refer to DSC-34-30-10 GENERAL).
‐ The ND displays ADF information, depending on the position of the ADF/VOR selectors on the
EFIS control panel (Refer to DSC-31-45 ROSE MODES).
‐ The DDRMI �� also displays ADF bearing, depending on the position of the ADF/VOR selector
(on the DDRMI).
ADF
Applicable to:
, ,
MSN,,,,
The aircraft has two ADF systems.
(For tuning instructions, Refer to DSC-34-30-10 GENERAL).
‐ The ND displays ADF information, depending on the position of the ADF/VOR selectors on the
EFIS control panel (Refer to DSC-31-45 ROSE MODES).
‐ The DDRMI �� also displays ADF1 and ADF2 bearings, depending on the position of the
ADF/VOR selector (on the DDRMI).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
NAVIGATION
RADIO NAV - NAVAIDS
A318/A319/A320/A321 FLEET DSC-34-30-20 P 3/4
FCOM 19 AUG 10
DME
Applicable to: ALL
The aircraft has two DMEs.
The frequency that is automatically set on the DME corresponds to the one that is set on the VOR or
ILS.
The NDs and the DDRMI can display VOR DME information, and the PFDs can display ILS DME
information (Refer to DSC-31-40-A TRAJECTORY DEVIATION - ILS APPROACH).
MARKER BEACON
Applicable to: ALL
One marker beacon system is included in VOR receiver 1.
The PFD displays the outer, middle, and inner marker signals (Refer to DSC-31-40-A TRAJECTORY
DEVIATION - ILS APPROACH).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
NAVIGATION
RADIO NAV - NAVAIDS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-34-30-20 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
NAVIGATION
RADIO NAV - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-34-30-30 P 1/4
FCOM 19 AUG 10
DIGITAL DISTANCE AND RADIO MAGNETIC INDICATOR (DDRMI)
Applicable to:
(1) Compass card
ADIRU 1 normally supplies the signal that positions the compass card. ADIRU3 supplies it,
when selected by the ATT HDG SWITCHING selector.
(2) Bearings pointers
Indicate the magnetic bearing to the station received by VOR 1 (dashed pointer) and VOR 2
(double pointer).
Note: Depending on the quality of the VOR beacon's signal, and mainly at distances greater
than 25 nm from the station, the processing of the signal, on aircraft equipped with
COLLINS or BENDIX VOR may lead to bearing pointer oscillations.
(3) VOR 1(2) flags
　
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