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MFD
PFD or
EICAS
PFD
MFD MFD
MFD AUX
HUD HUD
PFD EICAS MFD
INBD
DU DU
OUTBD
NORM
PFD/MFD
OUTBD
DU DU
INBD
NORM
PFD/MFD
1
2
2
PRELIMINARY
787 Flight Crew Operations Manual
Flight Instruments, Displays -
System Description
10.20.10 Boeing Proprietary
Inboard Display Switching
Display Select Panel MFD Selection
AUX PFD MFD EICAS MFD PFD
MFD
AUX
MFD
MFD
CHKL
INFO
COMM ND
SYS CDU
L R
MFD
SYS CDU INFO
CHKL COMM ND
LOWER MFD
SYS CDU INFO
CHKL COMM ND
LOWER MFD
CHKL
INFO
COMM ND
SYS CDU
L R
MFD
1 Only the display light of the last
selected MFD switch is illuminated.
Either the left or right display light
may be illuminated, but not both.
1
PRELIMINARY
787 Flight Crew Operations Manual
Flight Instruments, Displays -
System Description
Boeing Proprietary 10.20.11
EFIS Control Panel Multiple ND Control
ND ND
Each EFIS control panel controls the ND on the same side. If an ND is
displayed on both MFD windows of the lower display unit, the 2 normal-display
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
ND
ND
ND
ND
NDs combine to form a single full-display ND. The EFIS control panel used
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
to first select the ND on the lower DU is used to control the full-display ND.
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
RADIO BARO
MINS
IN HPA
BARO
FPV MTRS
RANGE
ND
WXR
MAP MENU
WXR TFC TERR
CTR
RST STD
PRELIMINARY
787 Flight Crew Operations Manual
Flight Instruments, Displays -
System Description
10.20.12 Boeing Proprietary
EICAS Transfer Switching
Multifunction Keypads (MFK)
[TBD]
Standby Flight Instruments
The standby flight instruments include:
• integrated standby flight display
• standby magnetic compass.
The EICAS transfer switches toggle the EICAS display between
the Captain inboard DU and the First Officer inboard DU.
AUX PFD PFD AUX
MFD MFD
MFD MFD
CANL/RCL
EICAS
CHKL
INFO
COMM ND
SYS CDU
L R
MFD
ENG
CANL/RCL
EICAS
CHKL
INFO
COMM ND
SYS CDU
L R
MFD
ENG
MFD
or
EICAS
MFD
or
EICAS
PRELIMINARY
787 Flight Crew Operations Manual
Flight Instruments, Displays -
System Description
Boeing Proprietary 10.20.13
Integrated Standby Flight Display (ISFD)
The ISFD displays attitude, airspeed, altitude, ILS, and magnetic heading
information. The ISFD receives airspeed and altitude from a dedicated pitot and
static air data module. Attitude information is provided by internal inertial
sensors. ILS information is provided by the left ILS receiver. The display receives
its heading information from the same source as the captain’s primary flight
display. Heading information is not available in polar regions.
Note: The standby magnetic compass must be used to validate heading
information.
Detection of a momentary out-of-limit ISFD condition may cause the attitude
display to blank and the WAIT ATT or ATT:RST message to display. When the
ATT:RST message displays, pushing the Attitude Reset switch resets the horizon
line with the airplane symbol.
On the ground, pushing the Attitude Reset switch must be accomplished with the
airplane stationary. In flight, pushing the Attitude Reset switch must be
accomplished with the airplane in wings level, non-accelerated flight. During
attitude reset, the ATT 10s message displays. Failure to maintain straight and level
flight for 10 seconds may result in an ATT:RST message. If attitude reset is
unsuccessful, the ATT:RST message remains displayed and the attitude will not
　
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