787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Flight Management, Navigation -
Flight Management System
Operation
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC 11.31.33
Takeoff and Climb (Engine Out)
Condition: before a sensed engine failure and above VNAV activation altitude.
Result: VNAV SPD commands a climb at V2+15 to V2+25 knots. Autothrottle
annunciation is THR REF and the thrust limit is takeoff.
1
Takeoff
Select and execute
ENG OUT
Actual speed reaches
VREF + 78 automatic change
from takeoff thrust limit
to continuous (CON) thrust limit
FMC maintains takeoff thrust and
speed V2 to V2 + 15
V2 + 15 TO V2 + 25
EO acceleration height or first
movement of flap lever
Sensed engine failure
VNAV activates (400 ft. above runway)
400 FT
Note: VNAV page title may be
LIM SPD CLB when target
speed is limited by flap
placard speed.
ACT EO CLB
FL250
223
<ALL ENG
CRZ ALT
EO SPD
ACT VREF + 80 CLB
FL250
250
<ALL ENG
ENG OUT>
CRZ ALT
SEL SPD
ENG OUT>
EO SID
loaded
automatically
5
4
3
6
1
2
August 14, 2009
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