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longer displayed or the thrust lever is closed.
[Decrease oil pressure in an atttempt to stop filter bypass.]
If ENG OIL FILTER 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 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):
Note: Use flaps 30 and VREF30 for landing and flaps 20
for go–around.
Do not accomplish the following checklist:
AUTOTHROTTLE
[]ENG OIL FILTER L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.11
7.11
Condition: Engine oil pressure is low.
Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
Retard slowly until ENG OIL PRESS message is no
longer displayed or the thrust lever is closed.
[Stabilizes air flow through engine.]
If ENG OIL PRESS 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 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):
Note: Use flaps 30 and VREF30 for landing and flaps 20
for go–around.
Do not accomplish the following checklist:
AUTOTHROTTLE
[]ENG OIL PRESS L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
7.12
7.12
Condition: Engine oil temperature is high.
Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . .Move to MID Positon
[Allows oil to cool.]
If oil temperature above red line limit:
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Close
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 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):
Note: Use flaps 30 and VREF30 for landing and flaps 20
for go–around.
Do not accomplish the following checklist:
AUTOTHROTTLE
[]ENG OIL TEMP L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.13
7.13
Condition: Thrust reverser control system has lost air/ground
protection to prevent inadvertent deployment in
flight.
Condition: Reverse thrust lever is not stowed in flight.
Condition: Fault is detected that may prevent normal deployment
of the affected reverser.
Note: Engine thrust reverser will not deploy or reverse
thrust will be limited to idle on landing.
Condition: Fault is detected in the affected engine reverser
system.
Condition: Engine control is limiting affected engine thrust to
prevent N1, N2 or N3 from exceeding the RPM
operating limit.
Condition: Both engines were shutdown on the ground by the
fuel control switches or fire switches.
　
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