Thales FMGS - Page 257

FLIGHT PHASES
APPROACH 17
AIRBUS A318/319/320/321
© THALES AVIONICS S.A.
J43126AA 00
VAPP should be entered as a SPD constraint at the FAF in order to
stabilize approach at this point.
FROM THV001 {}
UTC SPD/ALT
IN-BND 0639 / -----
BRG175° 8
FD14R 0702 *141/ 2710
TRK145° 3-3.0°
20V02 0704 " / *1860
C145° 5-3.0°
MD14R 0706 141/ 540
C145° 5NM
MD105{ ---- ---/ *900
DEST UTC DIST EFOB
LFBO14R 0706 16 7.0
£$
VERT REV AT FD14R
EFOB=7.1 EXTRA=5.9
DES SPD LIM
250/FL100
SPD CSTR ALT CSTR
146 [ ]
ACCESS
<WIND DATA STEP ALTS>
<RETURN
DEST APPR
QNH FLP RETR FINAL
1018 F=171 VOR14R
TEMP SLT RETR MDA
18° S=191 950
MAG WIND CLEAN
140°/10 O=215
TRANS ALT LOG CONF
5000 CONF3*
VAPP VLS
141 136 FULL
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PHASE>