FLIGHT PHASES
APPROACH
5
AIRBUS A318/319/320/321
© THALES AVIONICS S.A.
J43126AA 00
7.2. BEFORE APPROACH ACTIVATION
The following actions should be performed at the appropriate time, as
per SOPs (initial approach or before).
EFIS display
Select as necessary for
approach:
−
Mode / Range,
−
CSTR on,
−
ILS or LS (as installed) on.
Radio navaids
Check according to selection on
RAD NAV page.
Energy circle
REQUIRED DISTANCE TO LAND
is computed:
−
During DESCENT and
APPROACH phases when
within 180 NM of destination,
and,
−
when in selected lateral
mode (HDG or TRK).
For all A/C under these
conditions REQUIRED DISTANCE
TO LAND is shown on ND by
energy circle as a dashed green
arc (ARC or ROSE mode).
This distance is computed from
the energy state.
For A/C without GPS: additional
data are displayed on PROG
page [Line 5]:
−
REQD DIST TO LAND,
−
DIR DIST TO DEST.
RADIO NAV
VOR1/FREQ FREQ/VOR2
&
LON
/113.60
115.10/BIG
CRS
CRS
[ ]
[ ]
ILS /FREQ
CHAN/ MLS
IRR/110.30
[ ]/[ ]
CRS SLOPE CRS
F273
-.-
[ ]
ADF1/FREQ FREQ/ADF2
[ ]/[ .]
277.0
/CHT
ADF 2 BFO}
APPROACH
THV001
CRZ OPT REC MAX
----- -----
FL393
<REPORT
UPDATE AT
*[ ]
BRG /DIST
293°
/
16.7
TO
EGLL27R
REQD DIST TO LAND= 12
NM
DIR DIST TO DEST= 161
NM
REQUIRED ACCUR ESTIMATED
1.00
NM
HIGH
0.28NM
A/C without GPS
Summary of Contents for FMGS
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