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The radio navigation aids enable
the crew to navigate and monitor
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aircraft position.
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The A320 is equipped with two
Vors, 2 Dmes, 2 IL s s, one or
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two AD FS depending on the
airplane.
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GPS equipped aircraft have no AD
FS.
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Each DME is in reality A5
channel time sharing unit.
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One channel is associated with
the VOR, one with the ILS and
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the others are used for
navigation.
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The FMGC can automatically tune
the VORDME and ILS for position,
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updating and display purposes.
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Note that the ADF cannot be auto
tuned and is not used for
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navigation by the FMGC.
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The radio navigation itself is
controlled by both FMG CS and
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can be monitored through MCDU
pages.
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Either MCDU via the radio
navigation page enables the crew
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to manually tune a specific NAV
aid, including the ADF, FM, GC.
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Auto tuning continues normally
in the background.
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Note that when an ILS approach
is selected, ILS one is
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displayed on PFD one and ND 2.
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ILS 2 is displayed on PFD 2 and
ND one.
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As you have seen in the EFIS
chapter, the mode selector
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enables the pilot to select
different ND modes to display
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flight plan and navigate data.
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Plan mode is recommended when
entering and checking the flight
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plan.
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However, NAVAID data cannot be
displayed in this mode.
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In all the other modes, ROWS
ILS, ROWS VOR, ROWS NAV and ARC,
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the navaids can be displayed
provided the ADFVOR selectors
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have been switched to VOR or ADF
position.
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Here as an example, the ROWS VOR
mode is selected with ADF ONE
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and VOR 2.
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The ADF is shown as a green
pointer here.
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ADF ONE, VO, Rs are white
pointers in this example VOR
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two.
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Note also that the Receiver one
data is displayed on the left
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side of the ND and the Receiver
two data on the right side.
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The associated NAV Aid data is
displayed at the bottom of the
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ND in their respective colours
and sides.
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Presented here are all the
available modes for the
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navigation display.
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In the unlikely event of a
double FMGC failure, the Backup
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tuning mode provides radio
navigation redundancy to the
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crew.
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The backup tuning mode is
accessed via the Radio
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Management Panels RMP for NAVAID
tuning.
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RMP one standby NAV keys are
associated with VORD ME1 and ADF
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one, while RMP 2 keys are
associated with VORD ME2 and ADF
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2.
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Either RMP One or two can tune
the ILS.
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To access the backup tuning
mode, the NAV key has to be
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pressed.
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When the backup tuning mode is
selected, that is, the NAV key
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illuminated, the control of the
associated receivers is
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transferred to the RMP and the
NAV AID tuning capability of
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both FM GCS is lost.
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This is indicated on the MCDU by
a change to the radio navigation
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page, which shows only the
titles in dull white.
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To return the control to the
FMGC, the NAV key has to be
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pressed again.
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Once backup tuning has been
selected, the crew must select
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the desired type of NAV, aid,
BORILS or ADF.
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The DDRMI is on the main
instrument panel.
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The DDRMI Digital Distance and
Radio Magnetic Indicator
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displays raw data from ADFVOR
and DME sources and presents a
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traditional radio magnetic
indicator and bearing pointer
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presentation.
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Two bearing pointers are
provided, each readily
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identifiable by its shape with
its radio source.
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Each can display either VOR or
ADF information depending on
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selector position.
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Each pointer has an associated
control knob.
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The left knob selects either VO
R1 or ADF one.
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The right knob selects VO R2 or
ADF 2.
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If installed here, VO R1 and VO
R2 are selected.
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The compass card displays the
bearing information from Adiru 1
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VOR 1 Pointer and data are shown
on the navigation display
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display BOR two data.
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The left side of the ND
navigation display shows
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information from receiver one
and the right side data from
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receiver 2.
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Note the symbol next to the VOR
title.
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It is a reduced scale
representation of the number one
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VOR single needle pointer.
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Since the VOR data and the
pointer is displayed, both
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receivers consider the VOR
signal as valid.
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On the second line, the VOR
identifier appears.
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On the third line, the DME
distance appears in green.
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To see the NAV aids
automatically tuned by the FMGC,
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we have to call the RAD NAV
radio navigation page.
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Call the RAD NAV page.
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You can see on the radio
navigation page that the FMGC
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has automatically tuned the VOR
Lal on both receivers.
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The identifiers are shown on the
RAD NAV page and on the bottom
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of the navigation display.
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Note that the identifiers on the
radio navigation page are in
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small font.
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Now we will manually tune VOR
#2.
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The identifier Mel is already
typed into the scratch pad
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inserted by selecting line key
one right?
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The VOR identifier on the MCDU
is in large font, indicating a
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manual selection on the
navigation display.
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This is confirmed by a tiny
underlined M beside the VOR two
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data location.
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Because a valid signal has not
been received from the VOR, the
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associated data and pointer are
not shown.
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The number 2 radio is now
receiving a valid signal from
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the VOR.
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The associated pointer and data
are displayed on the navigation
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display along with the M, again
indicating that the VOR has been
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manually tuned.
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Since the VOR is not equipped
with the DME, the DME indication
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is replaced by green dashes.
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Now select the ILS switch on the
EFIS control panel.
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On the PFD, you can check the
ILS identifier, ICRR and the
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frequency and the course.
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The course is also indicated on
the navigation display.
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The check and the selection of
the NAV aids is now complete.
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The objective of the navigation
accuracy check is to compare the
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raw data from the tuned NAV aids
with the corresponding flight
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management computer data.
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This check also has to be
performed whenever the following
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cases occur.
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The progress page displays low
accuracy NAV accuracy.
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Downgrade message appears on the
MCDU and on the ND prior to
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beginning a descent.
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To perform this check you have
to use the selected navaids and
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display them on the navigation
display.
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We have set the ND range to 80.
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The VOR SPR has been manually
tuned on receiver one and the
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VOR PAS on receiver 2.
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Note that the VOR PAS is the
next two waypoint on the flight
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plan.
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There are two ways to do this
check.
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The first method is to compare
the two waypoint distance, which
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is flight management computer
data with the corresponding NAV
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and DME distance.
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The second method is to insert a
VORDME identifier in the bearing
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distance 2 field on the progress
page and to compare the computed
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bearing distance with the raw
data on the navigation display.
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We have typed the VORDME
identifier SPR in the scratch
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pad for you.
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Insert SPR in the bearing
distance field.
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The progress page now displays
the computed bearing and
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distance to the selected NAV
aid.
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The distance is shown on the
navigation display and on the
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progress page can be compared.
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Whatever method is used.
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If the error is less than one
nautical mile, the check is
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positive and the flight
management position is reliable.
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00:11:37,820 --> 00:11:41,934
The SOP recommends to use the
navigation display in arc or NAV
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mode and managed lateral
guidance.
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If the error is greater than one
nautical mile, you can consider
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that the flight management
position is not reliable.
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In such a case, the SOP requires
you to use raw data for
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navigation and to monitor it.
13140
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