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[Prevents water from entering airplane through outflow valve.]
Ditching position. . . . . . . . . . . . . . . . . . . . . . . . . . . Transmit
Review the after touchdown procedure:
• Set both FUEL CONTROL switches to CUTOFF
• Override and pull the APU fire switch
• Advise the cabin to evacuate.
Do not accomplish the following checklists:
• OUTFLOW VLV L
• OUTFLOW VLV R
• PACK L
• PACK R
• CABIN ALTITUDE AUTO
• PACK L+R
Continued on next page
December 15, 2006
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Copyright © The Boeing Company. See title page for details.
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Continued from previous page
When on final approach:
Landing gear lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20 or 30
Advise the cabin to brace for touchdown.
December 15, 2006
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Copyright © The Boeing Company. See title page for details.
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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
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Copyright © The Boeing Company. See title page for details.
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Condition: Engine start is needed after a shutdown with no fire or
apparent damage.
If X–START is shown:
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .START
[Allows electrical power to starter.]
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . . . .RUN
If an abort start condition as listed in normal procedures
occurs:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . CUTOFF
START selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
If X–START is not shown:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . . . . . . .RUN
If an abort start condition as listed in normal procedures
occurs:
FUEL CONTROL switch. . . . . . . . . . . . . . . . . . . CUTOFF
Engine may accelerate to idle very slowly, especially at high
altitudes. The time from fuel control switch to RUN to
stabilized idle may be as long as two and a half minutes.
Slow acceleration may be incorrectly interpreted as a hung
start or engine malfunction. If N2 is steadily increasing and
EGT remains within limits, the start is progressing normally.
If engine starts and runs normally:
GND PROX FLAP OVRD. . . . . . . . . . . . . . . . . . . . . . . . .OFF
TRANSPONDER MODE selector. . . . . . . . . . . . . . . . TA/RA
Condition: (TBD)
U ENG IN–FLIGHT START L, R
U ENG LIM/SURGE/STALL L, R
December 15, 2006
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Copyright © The Boeing Company. See title page for details.
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Intentionally
Blank
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Copyright © The Boeing Company. See title page for details.
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Condition: Engine has severe damage, vibration, or has
separated.
# Autothrottle ARM switch. . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Allows thrust lever to remain where manually positioned.]
　
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