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is inhibited automatically until boot-up is complete. CCS
boot-up completion is shown by (TBD).
APU L and R GEN switches – ON
APU selector – START, then ON
Note: Depending on the power source and CCS status, the EICAS
displays may not be available to alert the crew if a fault is
encountered during APU start. The APU will still shut down
automatically and the FAULT light on the APU panel will
illuminate.
787 Flight Crew Operations Manual
Supplementary Procedures Chapter SP
Engines, APU Section 7
Boeing Proprietary SP.7.1
SP.7 Supplementary Procedures-Engines, APU
Engine Start
The APU must be shutdown.
Verify the area behind the airplane is clear of equipment and personnel
prior to increasing thrust on operating engine.
Thrust lever (operating engine) ................................................. Advance
Increase thrust until TBD% N2 above idle.
Accomplish normal engine start.
787 Flight Crew Operations Manual
Supplementary Procedures -
Engines, APU
SP.7.2 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Supplementary Procedures Chapter SP
Flight Instruments, Displays Section 10
Boeing Proprietary SP.10.1
SP.10 Supplementary Procedures-Flight Instruments, Displays
QFE Operation
This procedure is accomplished when ATC altitude assignments are
referenced to QFE altimeter settings.
Note: Do not use LNAV and/or VNAV below transition altitude/level.
Altitudes in the navigation database are not referenced to QFE.
Use only raw data for navigation.
CDU APPROACH REF page .........................................................Select
LANDING REF key ....................................................................Push
Verify QFE selected.
[This sets the landing altitude to zero.]
Altimeters ........................................................................................... Set
Set altimeters to QFE when below transition altitude/level.
If the QFE altimeter setting is beyond the range of the altimeters, QNH
procedures must be used with QNH set in the altimeters.
787 Flight Crew Operations Manual
Supplementary Procedures -
Flight Instruments, Displays
SP.10.2 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Supplementary Procedures Chapter SP
Flight Management, Navigation Section 11
Boeing Proprietary SP.11.1
SP.11 Supplementary Procedures-Flight Management, Navigation
Alignment/Position Update
If a position update is desired during an automatic realignment (on
ground only):
CDU – SET
When dash prompts appear on the SET INERTIAL POS line of
the POS INIT page, enter the most accurate position.
If a manual alignment is desired (on ground only):
TBD switch – OFF 30 seconds, then ON
Wait an additional 30 seconds.
CDU – SET
Enter the most accurate position on the SET INERTIAL POS
line of the POS INIT page if either of the following is displayed
on the SET INERTIAL POS line:
• a latitude/longitude position is displayed.
Alignment requires from six to fifteen minutes depending on
latitude (six minutes at the equator, ten minutes average).
FMS Position Update
When the FMC message VERIFY POSITION is displayed, the FMC
position may require updating.
POS REF page ................................................................................Select
POS REF is the second page of POS INIT.
Compare the FMS positions with the displayed GPS, RADIO, and
INERTIAL positions.
Select the most appropriate source for FMC position updating.
UPDATE ARM key ........................................................................Select
The ARM prompt changes to ARMED and NOW prompts appear
to the right of the remaining position sources.
787 Flight Crew Operations Manual
Supplementary Procedures -
Flight Management, Navigation
SP.11.2 Boeing Proprietary
Appropriate source UPDATE NOW key ......................................... Push
Navaid Inhibit
Note: GPS position updates are allowed for all United States National
Airspace approach operations. Outside of this region, GPS
position updates are allowed during approaches only if the FMC
database and approach charts are referenced to the WGS-84
reference datum. GPS updates should be inhibited for all other
approach operations, unless other appropriate procedures are
used.
To inhibit GPS:
POS REF page .......................................................................... Select
POS REF is the second page of POS INIT.
GPS NAV key ............................................................................. Push
　
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