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CABIN ALTITUDE AUTO
Condition: TCAS has failed.
Condition: TCAS is in standby mode.
[]GND PROX SYS
OVERSPEED
PILOT RESPONSE
[]TAIL STRIKE
TCAS
TCAS OFF
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
15.4
15.4
Condition: TCAS cannot display RA guidance on the affected
PFD.
Condition: Terrain position data has been lost.
Note: Position data for the ND terrain map and look-ahead
terrain alerts are lost. Ground proximity alerts which
occur are valid.
Condition: Windshear alerts may not be provided.
Note: Some or all windshear alerts are not available.
Windshear alerts which occur are still valid.
TCAS RA CAPTAIN, F/O
[]TERR POS
[]WINDSHEAR SYS
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers Chapter MAN
Table of Contents Section 0
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary MAN.TOC.0.1
MNAoNn.–0 NMoanremuvaerls -MTabalen oefu Cvoentresn ts . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.1
Approach to Stall Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.1
Rejected Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.1
Terrain Avoidance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.4
Traffic Avoidance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.5
Upset Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.7
Windshear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.1.9
Flight Patterns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.2.1
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.2.1
ILS Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.2.2
Instrument Approach Using VNAV . . . . . . . . . . . . . . . . . . . MAN.2.3
Instrument Approach Using V/S or FPA . . . . . . . . . . . . . . . . MAN.2.4
Circling Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.2.5
Visual Traffic Pattern . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.2.6
Go–Around and Missed Approach . . . . . . . . . . . . . . . . . . . . MAN.2.7
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
MAN.TOC.0.2 D615Z003 Boeing Proprietary
Maneuvers -
Table of Contents
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers Chapter MAN
Non–Normal Maneuvers Section 1
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary MAN.1.1
MAN.1 Maneuvers-Non–Normal Maneuvers
Approach to Stall Recovery
The following is immediately accomplished at the first indication of stall
buffet or stick shaker.
Note: *At high altitudes it may be necessary to decrease pitch attitude
below the horizon to achieve acceleration.
Rejected Takeoff
The captain has the sole responsibility for the decision to reject the takeoff.
The decision must be made in time to start the rejected takeoff maneuver
by V1. If the decision is to reject the takeoff, the captain must clearly
announce “REJECT,” immediately start the rejected takeoff maneuver, and
assume control of the airplane. If the first officer is making the takeoff, the
first officer must maintain control of the airplane until the captain makes a
positive input to the controls.
Pilot Flying Pilot Monitoring
• Advance the thrust levers to maximum
thrust.
• Smoothly adjust the pitch attitude* to
avoid ground contact or obstacles.
• Level the wings (do not change flaps or
landing gear configuration).
• Retract the speedbrakes.
• Verify maximum
thrust.
• Monitor altitude and
airspeed.
• Call out any trend
toward terrain contact.
When ground contact is no longer a factor:
• Adjust the pitch attitude to accelerate
while minimizing altitude loss.
• Return to a speed appropriate for the
configuration.
December 15, 2006
787 Flight Crew Operations Manual
Maneuvers -
Non–Normal Maneuvers
Copyright © The Boeing Company. See title page for details.
MAN.1.2 D615Z003 Boeing Proprietary
Prior to 80 knots, the takeoff should be rejected for any of the following:
　
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