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Autothrottle Disconnect . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.10
787 Flight Crew Operations Manual
4.TOC.0.2 Boeing Proprietary
Automatic Flight -
Table of Contents
Automatic Flight Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.11
Automatic Flight Takeoff and Climb . . . . . . . . . . . . . . . . . . 4.20.11
HUD Takeoff (Optional) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.12
Automatic Flight Takeoff Profile . . . . . . . . . . . . . . . . . . . . . 4.20.13
Automatic Flight En Route . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.13
Automatic Flight Approach and Landing . . . . . . . . . . . . . . . 4.20.14
Automatic Flight Approach Profile (ILS) . . . . . . . . . . . . . . . 4.20.17
Go–Around . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.18
Automatic Flight Go–Around Profile . . . . . . . . . . . . . . . . . . 4.20.19
Automatic Flight Windshear Recovery . . . . . . . . . . . . . . . . . . . 4.20.19
Flight Envelope Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.20
EICAS Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.30.1
Automatic Flight EICAS Messages . . . . . . . . . . . . . . . . . . . . . . . 4.30.1
787 Flight Crew Operations Manual
Automatic Flight Chapter 4
Controls and Indicators Section 10
Boeing Proprietary 4.10.1
4.10 Automatic Flight-Controls and IndicatorsMode Control Panel (MCP)
Autopilot Flight Director System Controls
Push (either switch can engage the autopilot) –
• if either flight director switch is ON, the autopilot engages in the selected
flight director mode(s)
• if both flight director switches are OFF, the autopilot engages in:
• heading hold (HDG HOLD) or track hold (TRK HOLD) as the roll
mode, or if bank angle is greater than five degrees, attitude hold (ATT)
• vertical speed (V/S) or flight path angle (FPA) as the pitch mode.
Illuminated (white) – all operating autopilots are engaged.
1 Autopilot (A/P) Engage Switches
2 Autopilot Engaged Light
GLARESHIELD PANEL
DOWN
UP
30
VS/FPA HOLD APP
LOC/FAC
A/P
HOLD
LNAV
A/T FLCH
CLB/CON
A/P
A/T ARM
L R
OFF
IAS MACH
IAS
UL
200
250
A/P DISENGAGE
XFR
UL RL
HDG 200
200
AUTO
5
BANK
LIMIT
HDG TRK V/S FPA
V/S
ALTITUDE
17000
12000
+2000
VNAV
OFF
ON
F/D
OFF
ON
F/D
SEL
AUTO 1000
XFR XFR
UL
PRELIMINARY
LNAV
A/T FLCH
CLB/CON
A/P
A/T ARM
L R
OFF
IAS MACH
IAS
UL
200
200
A/P DISENGAGE
VNAV
OFF
ON
F/D
XFR
MODE CONTROL PANEL (MCP)
4
3
1
PRELIMINARY
2
787 Flight Crew Operations Manual
Automatic Flight -
Controls and Indicators
4.10.2 Boeing Proprietary
The left flight director switch activates the flight director steering indications on
the left PFD and HUD. The right flight director switch activates the flight director
steering indications on the right PFD and HUD.
ON –
• On the ground with both flight director switches OFF, the first flight
director switch positioned ON arms the flight director in the takeoff
go–around (TO/GA) roll and pitch modes. The flight mode annunciation
appears on both PFDs and HUDs. Positioning the second switch ON
displays the flight direction steering indications on the second PFD and
HUD.
• In flight, with the autopilot disengaged and both flight director switches
OFF, the first flight director switch positioned to ON engages the flight
director in:
• heading hold (HDG HOLD) or track hold (TRK HOLD ) as the roll
mode, or if bank angle is greater than five degrees, attitude hold (ATT)
• vertical speed (V/S) or flight path angle (FPA) as the pitch mode.
• In flight, with the autopilot engaged and both flight director switches
OFF, the first flight director switch positioned to ON engages the flight
director in the currently selected autopilot mode(s).
OFF –
• the flight director steering indications are not displayed
• the flight director steering indications are displayed on the PFDs and
HUDs if a TO/GA switch is pushed when airspeed is greater than 80 knots
on takeoff, or on a go–around with the flaps not retracted.
Pull down –
• prevents autopilot engagement
　
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