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Condition: One engine is at approach idle and the other engine is
at minimum idle.
[]ENG FUEL FILTER L, R
[]ENG FUEL VALVE L, R
ENG IDLE DISAGREE
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.7
7.7
Condition: Engine start is needed after a shutdown with no fire or
apparent damage.
If X–START is shown:
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
[Allows electrical power to starter.]
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . . . RUN
If an abort start condition as listed in normal procedures
occurs:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . CUTOFF
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
If X–START is not shown:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . . . RUN
If an abort start condition as listed in normal procedures
occurs:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . CUTOFF
Engine may accelerate to idle very slowly, especially at high
altitudes. The time from fuel control switch to RUN to
stabilized idle may be as long as two and a half minutes.
Slow acceleration may be incorrectly interpreted as a hung
start or engine malfunction. If N2 is steadily increasing and
EGT remains within limits, the start is progressing normally.
If engine starts and runs normally:
GND PROX FLAP OVRD. . . . . . . . . . . . . . . . . . . . . . . . .OFF
TRANSPONDER MODE selector. . . . . . . . . . . . . . . . TA/RA
U ENG IN–FLIGHT START L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
7.8
7.8
Condition: Engine indications are exceeding limits.
# Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
# Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
Retard until ENG LIMIT EXCEED message is no longer
displayed or the thrust lever is closed.
[Stabilizes air flow through engine.]
If ENG LIMIT EXCEED message remains displayed:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . CUTOFF
APU selector
(If APU available). . . . . . . . . . . . . . . . . . . . .START, then ON
[Provides an additional source of electrical power.]
TRANSPONDER MODE selector. . . . . . . . . . . . . . TA ONLY
[Prevents climb commands which can exceed single engine performance
capability.]
Plan to land at the nearest suitable airport.
If indications stabilized/EGT decreasing:
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Advance
Advance slowly. Check that RPM and EGT follow
thrust lever movement.
[Attempts to restore normal control of engine operation.]
Operate engine normally or at a reduced thrust level
which is surge and stall free.
If landing using flaps 20:
GND PROX FLAP OVRD. . . . . . . . . . . . . . . . . . . . . . . OVRD
Note: Use flaps 20 and VREF20 for landing and flaps 5 for
go–around.
Continued on next page
[]ENG LIMIT EXCEED L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.9
7.9
Continued from previous page
If landing using flaps 30 (performance permitting):
Note: Use flaps 30 and VREF30 for landing and flaps 20
for go–around.
Do not accomplish the following checklist:
AUTOTHROTTLE
Condition: Engine control is operating in alternate mode and
commanded N1 exceeds maximum N1.
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
Retard until N1 remains within appropriate limits.
Condition: (TBD)
Condition: Engine anti-ice capability is degraded.
Note: Avoid icing conditions.
[]ENG LIMIT PROT L, R
U ENG LIM/SURGE/STALL L, R
[]ENG LPC ANTI-ICE L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
7.10
7.10
Condition: Affected engine oil filter contamination has caused
filter bypass.
Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
Retard slowly until ENG OIL FILTER message is no
　
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