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• windshear warning (two-tone siren followed by
“WINDSHEAR,WINDSHEAR,WINDSHEAR”) or
• unacceptable flight path deviations.
Note: Unacceptable flight path deviations are recognized as
uncontrolled changes from normal steady state flight
conditions below 1000 feet AGL, in excess of any of the
following:
• 15 knots indicated airspeed
• 500 FPM vertical speed
• 5 degrees pitch attitude
• 1 dot displacement from the glideslope
• unusual thrust lever position for a significant period of
time.
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers -
Non–Normal Maneuvers
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary MAN.1.11
Windshear Escape Maneuver
MANUAL FLIGHT
Pilot Flying Pilot Monitoring
• Disconnect autopilot.
• Push either TO/GA switch.
• Aggressively apply maximum*
thrust.
• Disconnect autothrottle(s).
• Simultaneously roll wings level and
rotate toward an initial pitch
attitude of 15°.
• Retract speedbrakes.
• Follow flight director TO/GA
guidance (if available).
• Assure maximum* thrust.
• Verify all required actions
have been completed and
call out any omissions.
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers -
Non–Normal Maneuvers
Copyright © The Boeing Company. See title page for details.
MAN.1.12 D615Z003 Boeing Proprietary
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
capability of the AFDS. The pilot flying must be
prepared to disconnect the autopilot and
autothrottle(s) and fly manually.
AUTOMATIC FLIGHT
Pilot Flying Pilot Monitoring
• Press either TO/GA switch.**
• Verify TO/GA mode annunciation.
• Verify thrust advances to GA
power.
• Retract speedbrakes.
• Monitor system performance***.
• Assure maximum* thrust.
• Verify all required actions
have been completed and
call out any omissions.
• 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.
• Monitor vertical speed and
altitude.
• Call out any trend toward
terrain contact, descending
flight path, or significant
airspeed changes.
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers Chapter MAN
Flight Patterns Section 2
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary MAN.2.1
MAN.2 Maneuvers-Flight Patterns
Takeoff
Thrust set Positive rate of climb
Initial climb speed
Takeoff roll
• V2+15 to V2+25 knots, or
• V2 to V2+15 knots (1 engine)
• Set takeoff thrust by 80 knots
• Monitor airspeed
• Maintain light forward pressure
Note: For an immediate turn after
takeoff, maintain initial
climb speed with takeoff
flaps while maneuvering.
Follow AFDS bank limits.
Thrust reduction height
• Verify climb thrust
(2 engines)
• Manually advance
thrust to stabilize
• Push TO/GA
• Retract gear
V1 VR
• Rotate
Flaps up
• Verify CON thrust (1 engine)
• Do the NNC (as needed)
• Do the After Takeoff checklist
Acceleration height
• Retract flaps on schedule
Above 400 feet RA
• Select or verify roll mode
Engage the autopilot when above minimum
altitude for autopilot engagement.
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers -
Flight Patterns
Copyright © The Boeing Company. See title page for details.
MAN.2.2 D615Z003 Boeing Proprietary
　
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