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highlight box does not return to the top or bottom of the display when it reaches
the bottom or top respectively.
Each CDU page is composed of active and inactive areas. The highlight box only
displays over an active area. When the highlight box is displayed, an action may
be performed such as data entry or line key selection.
CLOCKWISE COUNTERCLOCKWISE
ROTATION ROTATION
HIGHLIGHT BOX MOVEMENT USING THE
CURSOR CONTROL SELECTOR PRELIMINARY
787 Flight Crew Operations Manual
Flight Management, Navigation -
Controls and Indicators
11.10.10 Boeing Proprietary
Additional manual manipulation of the highlight box is provided by the four
corners on the CCD touch pad that, when touched, result in the highlighting of the
corresponding 1L, 1R, 6L, or 6R line select key position.
An enter or line key selection may be performed utilizing any of the following:
• pushing the ENTER key on the onside multifunction keypad
• pushing the Cursor Select Switch on the onside multifunction keypad
• pushing the Cursor Select Switch on the onside CCD
Automatic Highlight Box Positioning
To facilitate data entry during preflight an autotabbing feature has been
implemented to guide the pilot through the data entry process. When data is
entered into a field in which autotabbing has been enabled, the hightlight box
automatically moves to the next appropriate entry field. Autotabbing only
operates when entering a page from a line select key and does not operate when a
function key is used to enter a page. Autotabbing is enabled on the following FMC
pages:
• ROUTE 1/X
• PERF INIT
• TAKEOFF REF
• TAKEOFF REF 1/2
The pilot can still move the highlight box with either the CCD or the CCS to any
active area within a page even if that area is not on the immediate autotabbing
sequence. This action does not disable autotabbing regardless of the position of
the highlight box. As long as a valid entry is made on a field that is in the
autotabbing sequence, autotabbing immediately takes over the highlight box
repositioning again.
If a valid entry is made in a field that is not in the autotabbing sequence, the
highlight does not move and the pilot must move it manually to the next desired
field. Whenever a delete is performed, the pilot must also manually move the
highlight box to the next desired field.
Autotabbing only operates in the display area adjacent to the line selection keys
and does not include the CDU function keys. Autotabbing is discontinued after the
FMS preflight is complete.
787 Flight Crew Operations Manual
Flight Management, Navigation -
Controls and Indicators
Boeing Proprietary 11.10.11
CDU Page Components
Subject or name of data displayed on page.
ACT (active) or MOD (modified) indicates whether page contains active or
modified data.
Data input is mandatory.
Title of data on line below.
Displays –
• prompts
• selectors
• data associated with line title.
Large font indicates crew entered or verified data. Small font indicates FMC
computed data.
Left number is page number. Right number is total number of related pages. Page
number is blank when only one page exists.
1 Page Title
2 Boxes
3 Line Title
4 Line
5 Page Number
CDU DISPLAY
KBFI
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D E S T
R U N W A Y F L T N O
R O U T E C O R O U T E
RO U TE
RO U TE
RTE 1
<REPORT
<REQUEST
<PRINT
<RTE 2
ALTN>
RTE COPY>
ACTIVATE>
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787 Flight Crew Operations Manual
Flight Management, Navigation -
Controls and Indicators
11.10.12 Boeing Proprietary
Data input is optional.
Display pages, select modes, and control displays. Caret “<” or “>” is before or
after prompt.
Displays alphanumeric entries, or line selected data.
Inertial System
Inertial Reference System (IRS)
Illuminated (white) – airplane battery powers IRS.
Note: ON BAT light illuminates only when IRS has been aligned on airplane or
ground power, and primary power is subsequently removed or failed
(battery power only remains).
ON – applies power to the associated IRS.
OFF – removes power from the associated IRS.
Note: IRS switches must be pulled out before moving to the OFF position.
Tuning and Control Panel
The transponder, weather radar and alternate navigation functions may be
　
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