MULTIPHASE
ENGINE-OUT 7
Pictures below show the ND display when engine failure occurs.
fter 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
1.0NM 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
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