787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Warning Systems -
Controls and Indicators
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC 15.10.7
Alerts Displayed on the PFD
NO AUTOLAND (amber) – Displayed when the airplane descends below 200
feet radio altitude during an approach in which the autopilot is flying a FMC
computed glidepath.
Indicates the minimum control speed for operation with a large thrust asymmetry.
ENG FAIL (red) – ENGINE FAIL alert is occurring.
PULL UP (red) – PULL UP alert is occurring.
SPEEDBRAKE (red) – SPEEDBRAKE alert is occurring.
WINDSHEAR (red) –
• predictive WINDSHEAR AHEAD alert or immediate WINDSHEAR alert
is occurring
• all other GPWS alerts inhibited
1
Autopilot Engaged Alert
2
Thrust Asymmetry Minimum Speed
3
Time Critical Warnings
000
400
600
6
1
1
2
2
6
NO AUTOLAND
10 10
20 20
10 10
0
200
20
80
180
WINDSHEAR
9
0
1
12
100
80
140
160
PRIMARY FLIGHT DISPLAY
1
3
2
August 14, 2009
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