曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Autothrottle DISCONNECT switch. . . . . . . . . . . . . . . . . PUSH
[Allows thrust levers to remain where manually positioned.]
Thrust levers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Close
Conditions permitting, operate engines at idle.
[Reduces possible engine damage and/or flameout by decreasing EGT.]
ENGINE ANTI–ICE selectors (Both). . . . . . . . . . . . . . . . . . .ON
[Increases bleed air extraction to improve engine stall margin.]
Recirculation FANS switches (Both). . . . . . . . . . . . . . . . .OFF
[Increases bleed air extraction to improve engine stall margin by putting
packs into high flow.]
APU selector
(If APU available). . . . . . . . . . . . . . . . . . . . . . .START, then ON
[Provides an electrical power source in the event one or both engines flame
out.]
Note: Volcanic ash can cause non–normal system reactions
such as:
• engine malfunctions, increasing EGT, engine stall
or flameout
• decrease or loss of airspeed indications
• EQUIP COOLING OVRD indications
• FIRE CARGO FWD or AFT indications.
Continued on next page
U VOLCANIC ASH
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.19
7.19
Continued from previous page
If engines flamed out or stalled, or EGT rapidly approaching
or exceeding limit:
FUEL CONTROL switches
(Both). . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF, then RUN
[Attempts to clear stall condition and allows engines to be put into start
mode.]
RAM AIR TURBINE switch. . . . . . . . . . . . . . . . . . . . . PUSH
Push and hold for 1 second.
[Backs up automatic deployment of the RAT.]
For a dual engine in-flight start, do not manually abort the
start if EGT indication turns red. Autostart allows EGT to
exceed the in-flight start limit, however autostart aborts
the start before EGT becomes too high for continued
engine operation.
Airspeed. . . . . . . . . . . . . . . . . . . . . . . . . . Above (TBD) KTS
[Ensures best windmill start capability.]
Engines may accelerate to idle very slowly, especially at
high altitudes. Slow acceleration may be incorrectly
interpreted as a hung start or engine malfunction. If N3 is
steadily increasing and EGT remains within limits, the
start is progressing normally. Any further cycling of the
fuel control switches will result in longer start times.
When HEAT PITOT L+C+R message no longer displayed:
PRIMARY FLIGHT COMPUTERS
DISCONNECT switch. . . . . . . . . . . . . .DISC, then AUTO
[Restores flight control normal mode following reversion to
secondary mode caused by loss of pitot heat.]
Autopilot can be re–engaged when flight control
normal mode is restored.
Plan to land at the nearest suitable airport.
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
7.20
7.20
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Fire Protection Section 8
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary TOC.8.1
Table of Contents
NNBC.O8 NToTn-LNEor m1a,l 2C hDecIkSlisCtsH-F irEe NPrGote c t.i o.n . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
BOTTLE DISCH APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
BOTTLE DISCH CARGO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
[] DET FIRE APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
DET FIRE CARGO AFT, FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
[] DET FIRE ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.1
[] FIRE APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
[] FIRE CARGO AFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
[] FIRE CARGO FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.3
[] FIRE ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.4
u FIRE ENG TAILPIPE L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.5
[] FIRE WHEEL WELL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.6
[] OVERHEAT ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.8
[] SMOKE EQUIP CLG AFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.9
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
787QRH快速检查单(36)
