787QRH快速检查单(26)

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D615Z003 Boeing Proprietary TOC.3.1
Table of Contents
[N]NAC.N3 NToIn–-NICorEma Dl CEheTck WlistIs-NAGnti - I.c e., .R .a i.n . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.1
[] ANTI–ICE ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.1
[] ANTI–ICE LEAK ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.2
ANTI–ICE LOSS ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3
[] ANTI–ICE ON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3
[] ANTI–ICE PACKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3
[] ANTI–ICE WING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3
[] HEAT PITOT C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3
[] HEAT PITOT L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4
[] HEAT PITOT L+C+R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4
[] HEAT PITOT R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4
[] ICE DETECTORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4
ICING ENG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.4
[] OVERHEAT WING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.5
u TAT PROBE ICING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.6
WINDOW HEAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.7
[] WINDOW HEAT L, R FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.8
[] WINDOW HEAT L, R SIDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.8
WING ANTI–ICE OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.8
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.3.2 D615Z003 Boeing Proprietary
Non-Normal Checklists -
Anti-Ice, Rain
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 3.1
3.1
NNC.3 Non-Normal Checklists-Anti-Ice, Rain
Condition: Wing ice detection has failed.
Note: Operate wing anti-ice systems manually.
Condition: Engine anti–ice valve remains closed when
commanded open.
ENGINE ANTI-ICE selector. . . . . . . . . . . . . . . . . OFF, then ON
[Attempts to manually reset controller and open the valve.]
If ANTI-ICE ENG message no longer displayed:
Operate affected engine anti-ice system manually.
[Automatic anti-ice is not available for affected engine.]
If ANTI-ICE ENG message remains displayed:
ENGINE ANTI-ICE selector. . . . . . . . . . . . . . . . . . . . . . .OFF
[Enables display of ICING ENG message if encountering icing
conditions.]
Note: Avoid icing conditions.
[Anti-ice is not available to affected engine because the engine anti-ice
system has failed.]
[]ANTI–ICE DET WING
[]ANTI–ICE ENG L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
3.2
3.2
Condition: High temperature anti–ice bleed air leak is detected in
the affected engine.
The engine anti-ice system automatically isolates heat
source within approximately 2 minutes by closing the
engine anti-ice valve.
Note: Avoid icing conditions.
[Anti–ice is not available to affected engine.]
If, after 2 minutes, ANTI–ICE LEAK ENG message remains
displayed:
Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
Thrust lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retard
Retard slowly until the ANTI–ICE LEAK ENG
message is no longer displayed or the thrust lever is
closed.
[Reduces flow of bleed air through the leak.]
Do not accomplish the following checklist:
AUTOTHROTTLE
If ANTI–ICE LEAK ENG message remains displayed:
TRANSPONDER MODE selector. . . . . . . . . . . . TA ONLY
[Prevents climb commands which can exceed single engine
performance capability.]
Note: Operate engine at idle for remainder of flight.
If landing using flaps 20:
GND PROX FLAP OVRD . . . . . . . . . . . . . . . . . . OVRD
Note: Use flaps 20 and VREF20 for landing and flaps
5 for go–around.
　
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