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ENG REV LIMITED L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.13
ENG REVERSER L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.13
ENG RPM LIMITED L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.13
ENG SHUTDOWN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.13
ENG SHUTDOWN L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.14
[] ENG START CUTOUT L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.14
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.7.2 D615Z003 Boeing Proprietary
Non-Normal Checklists -
Engines, APU
[] ENG START INHIBIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.14
[] ENG STARTERS L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.15
[] ENG SURGE L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.15
u ENG SVR DAMAGE/SEP L, R . . . . . . . . . . . . . . . . . . . . . . . . . 7.16
ENG THRUST L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.17
u VOLCANIC ASH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.18
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.1
7.1
NNC.7 Non-Normal Checklists-Engines, APU
Condition: During a ground start, an abort engine start condition
occurs.
# FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . CUTOFF
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
Motor the engine for 30 seconds.
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
Condition: APU operation has exceeded a limit.
APU selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Condition: APU has automatically shut down.
APU selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Attempts to reset APU controller.]
APU selector. . . . . . . . . . . . . . . . . . . . . . . . . . .START, then ON
U ABORTED ENGINE START L, R
[]APU LIMIT
[]APU SHUTDOWN
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
7.2
7.2
Condition: Engine speed for both engines is below idle.
# 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.]
Airspeed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Above 250 KTS
[Ensures best windmill start capability.]
APU selector
(If APU available). . . . . . . . . . . . . . . . . . . . . . .START, then ON
[Backs up automatic APU start.]
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+R+C 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.
U DUAL ENG FAIL/STALL
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 7.3
7.3
Condition: Autostart has failed to start the engine.
# FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . CUTOFF
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
Condition: Fault is detected in the affected engine control
system.
Condition: Control for the affected engine is operating in
alternate mode.
Autothrottle DISCONNECT switch. . . . . . . . . . . . . . . . . PUSH
[Allows thrust levers to remain where manually positioned.]
Thrust lever (Both). . . . . . . . . . . . . . . . Retard to MID position
[Prevents exceeding thrust limits when switching to alternate mode.]
　
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