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When at top of descent:
LANDING ALTITUDE selector. . . . . . . . . . . . . . . . . . . PUSH
[Restores automatic selection of the FMC landing altitude.]
Note: After landing, inform ground personnel NOT to
open the cargo door until all passengers and crew
have exited the airplane and fire fighting equipment
is nearby.
[]FIRE CARGO FWD
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
8.4
8.4
Condition: Fire is detected in the engine.
# Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
# Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Close
[Assists in recognition of affected engine.]
# FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . CUTOFF
# ENGINE FIRE switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
[Shuts off fuel and hydraulic fluid and arms the fire extinguishing system.]
# If FIRE ENG message remains displayed:
# ENGINE FIRE switch. . . . . . . . . . . . . . . . . . . . . . . . Rotate
Rotate to the stop and hold for 1 second.
# If, after 30 seconds, FIRE ENG message remains
displayed:
# ENGINE FIRE
switch. . . . . . . . . . . . . . . . . . . . . . .Rotate to Other Bottle
Rotate to the stop and hold for 1 second.
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 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
[]FIRE ENG L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 8.5
8.5
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: An engine tailpipe fire is reported on the ground with
no engine fire warning.
FUEL CONTROL switch (Affected engine). . . . . . . . . CUTOFF
Advise the cabin.
If electrical is available:
START selector (Affected engine). . . . . . . . . . . . . . START
Advise the tower.
If the engine is being motored:
Continue to motor until the tailpipe fire is extinguished.
START selector (Affected engine). . . . . . . . . . . . . . . NORM
U FIRE ENG TAILPIPE L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
8.6
8.6
Condition: Fire is detected in a main wheel well.
Observe gear EXTEND limit speed (270K/.82M).
Landing gear lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DN
[Attempts to remove and extinguish the fire source.]
Plan to land at the nearest suitable airport.
Flight with gear down increases fuel consumption and
decreases climb performance. Refer to Gear Down
performance tables in Performance–Inflight chapter for
flight planning.
If landing gear must be retracted for airplane performance:
When FIRE WHEEL WELL message no longer displayed:
Wait 20 minutes.
[Attempts to ensure that wheel well fire is extinguished.]
Landing gear lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
[]FIRE WHEEL WELL
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 8.7
8.7
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
8.8
8.8
Condition: Overheat is detected in the nacelle.
ENGINE ANTI-ICE selector. . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Attempts to stop the flow of engine anti-ice bleed air through the leak.]
Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
　
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