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• prefaced with white dot
• COMM low messages indented one space
• cannot be canceled by pushing the CANC/RCL switch
Displayed (white) –
• reminder of selected state of controls or systems
• cannot be canceled by pushing the CANC/RCL switch
• EICAS alert messages have display priority over memo messages; some
or all memo messages not displayed on current EICAS message page if
insufficient message lines are available below alert messages
Displayed (white) –
• more than one page of alert or memo messages exists
• indicates number of page selected
Displayed (cyan) –
• new status message exists
• no longer displayed when status display selected
• inhibited from beginning of first engine start until cruise altitude or 30
minutes after lift-off
Displayed (white) –
• when CANC/RCL switch pushed
• remains displayed for one second after switch released
4 Advisory Messages
5 Communication Messages
6Memo Messages
7 Page (PG) Number
8 STATUS Cue
9 RECALL Indication
787 Flight Crew Operations Manual
Warning Systems -
Controls and Indicators
Boeing Proprietary 15.10.3
Display Select Panel
Push – displays system display on selected MFD.
Push – displays status display on selected MFD.
Subsequent pushes –
• displays next page of status messages when additional pages exist
• lower center MFD blanks when last page of status messages displayed
• inboard MFDs return to NAV display after last page of status messages
displayed
Push (when EICAS caution or advisory messages displayed) –
• displays the next page of EICAS messages when additional pages exist
• cancels caution and advisory messages when last page displayed;
warning, memo, and communications messages remain displayed
• cancels red box for any engine parameter previously exceeded when
displayed parameter no longer exceeds the limit
1 System (SYS) Display Switch
2 Status (STAT) Display Switch
3 Cancel/Recall (CANC/RCL) Switch
GLARESHIELD
CHKL
INFO
COMM ND
SYS CDU
L R
MFD
CANL/RCL
EICAS
ENG
PRELIMINARY
3
1
SYSTEMS DISPLAY
2
787 Flight Crew Operations Manual
Warning Systems -
Controls and Indicators
15.10.4 Boeing Proprietary
Push (when no EICAS caution or advisory messages displayed) –
• redisplays all caution and advisory EICAS messages, when non-normal
condition exists
• displays first page of messages when multiple pages exist
• redisplays red box for parameters previously exceeded
Alerts Displayed on the PFD
DON’T SINK (amber) – DON’T SINK alert is occurring.
ENG FAIL (red) – ENGINE FAIL alert is occurring.
FLAPS (amber) – TOO LOW FLAPS alert is occurring.
GEAR (amber) – TOO LOW GEAR alert is occurring.
PULL UP (red) – PULL UP alert is occurring.
SINK RATE (amber) – SINK RATE alert is occurring.
SPEEDBRAKE (red) – SPEEDBRAKE alert is occurring.
TERRAIN (amber) – TERRAIN alert is occurring.
WINDSHEAR (red) –
• predictive WINDSHEAR AHEAD alert or immediate WINDSHEAR
alert is occurring
• all other GPWS alerts inhibited.
1 Alerts on PFD
PFD
PRELIMINARY
-4
20 20
6
2
-200
WINDSHEAR
PRIMARY FLIGHT DISPLAY
100
1
787 Flight Crew Operations Manual
Warning Systems -
Controls and Indicators
Boeing Proprietary 15.10.5
Alerts Displayed on the HUD
Most alerts displayed on the PFD are also displayed on the lower portion of both
HUDs.
MasterWARNING/CAUTION Reset Switches and Lights
Push –
• extinguishes master WARNING lights
• extinguishes master CAUTION lights
• silences the aural that accompanies the EICAS warning messages:
• CABIN ALTITUDE
• CONFIG GEAR, if displayed because landing gear not down and
locked, any thrust lever at idle, and radio altitude less than 800 feet
• FIRE
• PILOT RESPONSE
1 Alerts on HUD
1Master WARNING/CAUTION Reset Switch
PRELIMINARY
HEADS UP DISPLAY
PRELIMINARY 1
WARNING
CAUTION
GLARESHIELD PANEL
2
3
1
PRELIMINARY
787 Flight Crew Operations Manual
Warning Systems -
Controls and Indicators
15.10.6 Boeing Proprietary
Illuminated (red) –
• new EICAS warning message displayed, or
• ENGINE FAIL, PULL UP, or WINDSHEAR alert displayed on PFD
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787机组操作手册Flight Crew Operations Manual 3(112)
