MULTIPHASE
ENGINE-OUT 7
Pictures below show the ND display when engine failure occurs.
After ENG failure
Before ENG failure
If engine failure occurs after the EO SID diversion point:
−
Both MCDUs switch automatically to the PERF page,
−
No temporary flight plan is created but EOSID track is displayed on
ND (NAV, ARC or PLAN mode) with a continuous yellow line.
PERF page
TAKE OFF
V1 FLP RETR
EO
141
F=
150
CLR*
VR SLT RETR TO SHIFT
141
S=
192
V2 CLEAN FLAPS/THS
143
O=
216
2/UP0.6
TRANS ALT DRT TO-FLX TO
5000
F55
THR RED/ACC ENG OUT ACC
1990
/3490
1990
NEXT
PHASE>
CRZ FL ABOVE MAX FL
−
EO CLR* [1R] is displayed,
−
ENG OUT ACC altitude [5R] is
displayed.
%
EO
TAKE OFF
THV001
CRZ OPT REC MAX
FL360
-----
FL218
<REPORT
UPDATE AT
*[ ]
BRG /DIST
303° /23.9
TO
LFBO14R
PREDICTIVE
<GPS
GPS PRIMARY
REQUIRED ACCUR ESTIMATED
1.0
NM
HIGH
0.08NM
CRZ FL ABOVE MAX FL
PROG page
−
Title page becomes EO TAKE OFF,
%
−
OPT FL is dashed,
−
REC MAX becomes one engine
REC MAX altitude.
Proceed according to SOPs for Acceleration / Flap retraction &
Thrust reduction.
AIRBUS A318/319/320/321
© THALES AVIONICS S.A.
J43126AA 00
Summary of Contents for FMGS
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