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Thales FMGS - Page 198

Thales FMGS
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FLIGHT PHASES
16 CRUISE
BRG DIST (Line 4)
This function may be used to enter an
en-route alternate airport or crosscheck
FMGCs accuracy with usable navaids.
Line 5:
A/C with GPS:
PREDICTIVE GPS prompt [5L] and,
GPS confidence level [5R].
See Part III: Ch 7.3 – Position
Monitoring.
A/C without GPS:
Display Required Distance to Land and
Direct Distance to Destination when in
HDG/TRK mode and within 180 NM to
DEST and in Cruise, Descent or A
phase.
pproach
Required Distance to Land is also
displayed on ND by the energy circle.
See Part II – Descent
Line 6: ACCURACY
This field enables to monitor navigation accuracy.
See Part III: Ch 7.3 – Position Monitoring.
CRUISE THV001
CRZ OPT REC MAX
FL360 FL360 FL388
<REPORT
UPDATE AT
*[ ]
BRG /DIST
355° /366.5 TO EGLL27R
PREDICTIVE
<GPS GPS PRIMARY
REQUIRED ACCUR ESTIMATED
2.0NM HIGH 0.08NM
CRUISE THV001
CRZ OPT REC MAX
FL360 FL364 FL392
<REPORT
UPDATE AT
*[ ]
BRG /DIST
333° /149.1 TO EGLL27R
REQUIRED ACCUR ESTIMATED
1.0NM HIGH 0.28NM
CRUISE THV001
CRZ OPT REC MAX
FL360 FL364 FL392
<REPORT
UPDATE AT
*[ ]
BRG /DIST
333° /149.1 TO EGLL27R
REQD DIST TO LAND= 72NM
DIR DEST TO DEST= 170NM
REQUIRED ACCUR ESTIMATED
1.0NM HIGH 0.28NM
J43126AA 00
© THALES AVIONICS S.A.
AIRBUS A318/319/320/321

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