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(TBD)
Circling Approach
Note: Autopilot use is recommended until intercepting the landing
profile.
MCP Altitude selector .........................................................................Set
Accomplish an instrument approach, establish suitable visual
reference, and level off at MDA(H).
Verify ALT or VNAV ALT mode annunciates.
MCP Altitude selector ............................. Set Missed Approach Altitude
HDG SEL/TRK SEL switch .............................................................Push
Verify HDG SEL or TRK SEL mode annunciates.
Intercepting the landing profile:
Autopilot disengage switch .........................................................Push
787 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
SP.4.10 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Supplementary Procedures Chapter SP
Communications Section 5
Boeing Proprietary SP.5.1
SP.5 Supplementary Procedures-Communications
Flight Deck Communications System (Datalink)
The following procedures are one means which may be used to verify
Pre-Departure Clearance, Digital-Automatic Terminal Information
Service (D-ATIS), Oceanic Clearances, Weight and Balance and Takeoff
Data messages transmitted via the COMPANY format.
Pre-Departure Clearance
The flight crew shall manually verify (compare) the filed flight plan versus
the digital pre-departure clearance and shall initiate voice contact with Air
Traffic Control if any question/confusion exists between the filed flight
plan and the digital pre-departure clearance.
Digital-Automatic Terminal Information Service
The flight crew shall verify that the D-ATIS altimeter setting numeric
value and alpha value are identical. If the D-ATIS altimeter setting numeric
value and alpha value are different, the flight crew must not accept the
D-ATIS altimeter setting.
Oceanic Clearances
The flight crew shall manually verify (compare) the filed flight plan versus
the digital oceanic clearance and initiate voice contact with Air Traffic
Control if any questions/confusion exists between the filed flight plan and
the digital oceanic clearance.
Weight and Balance
The flight crew shall verify that the Weight and Balance numeric and
alphabetic values are identical. If the Weight and Balance numeric and
alphabetic values are different, the flight crew must not accept the Weight
and Balance data.
Takeoff Data
The flight crew shall verify that the Takeoff Data numeric and alphabetic
values are identical. If the Takeoff Data numeric and alphabetic values are
different, the flight crew must not accept the Takeoff Data message.
787 Flight Crew Operations Manual
Supplementary Procedures -
Communications
SP.5.2 Boeing Proprietary
Intentionally
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787 Flight Crew Operations Manual
Supplementary Procedures Chapter SP
Electrical Section 6
Boeing Proprietary SP.6.1
SP.6 Supplementary Procedures-Electrical
Electrical Power Down
The following procedure is accomplished to remove all electrical power
from the airplane.
Before accomplishing the following steps, verify, EMER LIGHTS, and
PACK switches are off and HYD PRESS SYS L+C+R message is
displayed.
APU selector and/or EXTERNAL POWER switch(es) ................... OFF
BATTERY switch ............................................................................. OFF
787 Flight Crew Operations Manual
Supplementary Procedures -
Electrical
SP.6.2 Boeing Proprietary
Electrical Power Up
The following procedure is accomplished to permit safe application of
electrical power.
BATTERY switch .............................................................................. ON
C1 and C2 ELEC pump selectors .....................................................OFF
DEMAND pump selectors ................................................................OFF
WIPER selectors ...............................................................................OFF
Landing gear lever.............................................................................. DN
ALTN FLAPS selector ......................................................................OFF
Electrical power ........................................................................ Establish
If external power is desired:
L FWD EXT PWR AVAIL light – Illuminated
L FWD EXT PWR switch – Push
If R FWD EXT PWR AVAIL light is illuminated:
R FWD EXT PWR switch – Push
If APU power is desired:
Note: CCS boot-up requires up to 90 seconds on battery power,
and up to 3.5 minutes when on external power. APU start
　
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