曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

# Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Close
[Assists in recognition of affected engine.]
# FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . CUTOFF
# ENGINE FIRE switch. . . . . . . . . . . . . . . . . . . . . . . . . . . .PULL
[Shuts off fuel and hydraulic fluid.]
If high airframe vibration occurs and continues after engine
shutdown:
Without delay, reduce airspeed and descend to a safe
altitude which results in an acceptable vibration level.
If high vibration returns and further airspeed reduction
and descent is not practical, increasing the airspeed may
reduce the vibration.
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.
If landing using flaps 30 (performance permitting):
Continued on next page
U ENG SVR DAMAGE/SEP L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 0.9
0.9
Continued from previous page
If landing using flaps 30 (performance permitting): (continued)
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
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Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
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Condition: Fuel jettison is required.
FUEL JETTISON ARM switch. . . . . . . . . . . . . . . . . . . .ARMED
If desired FUEL TO REMAIN different than displayed FUEL
TO REMAIN:
FUEL TO REMAIN selector. . . . . . . . . . . Pull, set manually
FUEL JETTISON NOZZLE switches (Both). . . . . . . . . . . . .ON
Do not accomplish the following checklists:
FUEL PUMP CENTER L
FUEL PUMP CENTER R
When fuel jettison complete:
FUEL JETTISON NOZZLE switches (Both). . . . . . . . . .OFF
FUEL JETTISON ARM switch. . . . . . . . . . . . . . . . . . . . .OFF
U FUEL JETTISON
December 15, 2006
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Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 0.11
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Intentionally
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December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
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Condition: An in flight fuel leak is suspected or confirmed.
One or more of the following may be evidence of a fuel leak:
• visual observation of fuel spray from strut/engine
• excessive engine fuel flow
• total fuel quantity decreasing at an abnormal rate
• FUEL DISAGREE message on EICAS
• FUEL IMBALANCE message on EICAS
• FUEL QTY LOW message on EICAS
• INSUFFICIENT FUEL message on EICAS.
CENTER FUEL PUMP switches (Both). . . . . . . . . . . . . . . .OFF
CROSSFEED switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
BALANCE switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Identify an engine fuel leak by observing a left or right main
fuel tank quantity decreasing faster than the other.
An increase in fuel imbalance of approximately 1000 lbs or
more in 30 minutes should be considered a fuel leak.
Conditions permitting, visually check for engine fuel leak.
If left and right main tank quantities decrease at same rate:
Fuel leak may be from center tank to center wing area. Do
not use center tank fuel.
If FUEL DISAGREE message displayed:
PROGRESS page 2/4. . . . . . . . . . . . . . . . . . . . . . . Select
CALCULATED. . . . . . . . . . . . . . . . . . . . . . . . . Select Use
　
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