Boeing 787 Quick Reference Handbook page 250

Maneuvers -
Non–Normal Maneuvers
AUTOMATIC FLIGHT
Pilot Flying
• Press either TO/GA switch.**
• Verify TO/GA mode annunciation.
• Verify thrust advances to GA
power.
• Retract speedbrakes.
• Monitor system performance***.
• Do not change gear or flap
configuration until windshear is no
longer a factor.
• Monitor vertical speed and altitude.
• Do not attempt to regain lost
airspeed until windshear is no
longer a factor.
Note: Aft control column force increases as the airspeed decreases. In
all cases, the pitch attitude that results in intermittent stick
shaker or initial buffet is the upper pitch attitude limit. Flight at
intermittent stick shaker may be required to obtain positive
terrain separation. Smooth, steady control will avoid a pitch
attitude overshoot and stall.
Note: * Maximum thrust can be obtained by advancing the thrust
levers full forward if the EECs are in the normal mode. If terrain
contact is imminent, advance thrust levers full forward.
Note: ** If TO/GA is not available, disconnect autopilot and
autothrottle(s) and fly manually.
WARNING: *** Severe windshear may exceed the performance
MAN.1.12
787 Flight Crew Operations Manual
capability of the AFDS. The pilot flying must be
prepared to disconnect the autopilot and
autothrottle(s) and fly manually.
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
Pilot Monitoring
• Assure maximum* thrust.
• Verify all required actions
have been completed and
call out any omissions.
• Monitor vertical speed and
altitude.
• Call out any trend toward
terrain contact, descending
flight path, or significant
airspeed changes.
December 15, 2006