Thales FMGS - Climb

MULTIPHASE PROCEDURES
8 ENGINE-OUT
OP CLB
ALT
AP1
1FD2
A/THR
NAV
THR CLB
LVR MCT
8.4. CLIMB
If an engine failure
occurs when FMGS is in
CLIMB phase, EO mode
is activated and:
− LVR MCT flashes on FMA,
CLB
ACT MODE EO
MANAGED CLR*
CI
EO LRC PRED TO FL150
MANAGED UTC DIST
217/--- ---- ----
EXPEDITE ---- ----
ACTIVATE NEXT
{APPR PHASE PHASE>
− Both MCDUs switch
automatically to the PERF
CLB page,
− Vertical mode reverts to OP
CLB if engaged in managed
mode.
 If the aircraft is in climb
above ACC ALT:
Target speed becomes
GREEN DOT.
 If the aircraft has leveled-
off at an intermediate
cruise altitude with the
FMGS still in CLB phase:
Target speed becomes EO
LRC MACH/SPEED.
PERF page
CLB
ACT MODE EO
MANAGED CLR*
CI
EO LRC PRED TO FL150
MANAGED UTC DIST
217/--- ---- ----
EXPEDITE ---- ----
ACTIVATE NEXT
{APPR PHASE PHASE>
− EO CLR *[1R] is displayed,
− MANAGED speed is
displayed,
− CI is defaulted to EO LRC.
EO CLIMB THV001
CRZ OPT REC MAX
FL360 ----- FL310
<REPORT
UPDATE AT
*[ ]
BRG /DIST
303° /23.9 TO LFBO14R
PREDICTIVE
<GPS GPS PRIMARY
REQUIRED ACCUR ESTIMATED
1.0NM HIGH 0.08NM
PROG page
EO REC MAX altitude is displayed.
J43126AA 00
© THALES AVIONICS S.A.
AIRBUS A318/319/320/321