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Heading/track selector ....................................................................Rotate
Set desired track in the HDG/TRK window.
Altitude Hold
Altitude HOLD switch ..................................................................... Push
Verify ALT is displayed in the pitch mode annunciator.
Flight Level Change, Climb or Descent
ALTITUDE selector .......................................................................Rotate
Set the desired altitude in the MCP ALTITUDE window.
FLCH switch .................................................................................... Push
Verify FLCH SPD is displayed in the pitch mode annunciator.
IAS/MACH selector .......................................................................Rotate
Set the desired speed in the IAS/MACH window.
787 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
Boeing Proprietary SP.4.3
Vertical Speed, Climb or Descent
ALTITUDE selector ...................................................................... Rotate
Set the desired altitude in the MCP ALTITUDE window.
VERTICAL SPEED/FLIGHT PATH ANGLE reference switch......Push
Verify V/S is displayed in the vertical speed/flight path angle
window.
VERTICAL SPEED/FLIGHT PATH ANGLE switch .....................Push
Verify V/S is displayed in the pitch mode annunciator.
VERTICAL SPEED/FLIGHT PATH ANGLE selector ................ Rotate
Set the desired vertical speed in the VERTICAL SPEED/FLIGHT
PATH ANGLE window.
If a climb is desired:
Select climb thrust limit on the CDU THRUST LIM page.
Flight Path Angle, Climb or Descent
ALTITUDE selector ...................................................................... Rotate
Set the desired altitude in the MCP ALTITUDE window.
VERTICAL SPEED/FLIGHT PATH ANGLE Reference switch ....Push
Verify FPA is displayed in the vertical speed/flight path angle
window.
VERTICAL SPEED/FLIGHT PATH ANGLE switch .....................Push
Verify FPA is displayed in the pitch mode annunciator.
VERTICAL SPEED/FLIGHT PATH ANGLE selector ................ Rotate
Set the desired flight path angle in the VERTICAL
SPEED/FLIGHT PATH ANGLE window.
If a climb is desired:
Select climb thrust limit on the CDU THRUST LIM page.
787 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
SP.4.4 Boeing Proprietary
Autothrottle Operation
AUTOTHROTTLE ARM switches ................................................ARM
If the pitch mode is TO/GA:
TO/GA switch ............................................................................. Push
Verify that THR REF is displayed in the autothrottle mode
annunciator. THR REF changes to HOLD at 80 knots.
If the pitch mode is ALT, V/S, FPA, G/S, or no pitch mode:
AUTOTHROTTLE engage switch ............................................. Push
Verify that SPD is displayed in the autothrottle mode
annunciator.
If a constant speed is desired:
IAS/MACH selector ............................................................Rotate
Set the desired speed in the IAS/MACH window.
If climb or continuous thrust is desired:
CLB CON switch................................................................... Push
Verify that THR REF is displayed in the autothrottle mode
annunciator.
If FLCH or VNAV is desired:
FLCH or VNAV switch ......................................................... Push
Verify that THR REF, THR, SPD, IDLE, or HOLD as
appropriate is displayed in the autothrottle mode annunciator.
If TO/GA is desired:
TO/GA switch ........................................................................ Push
The pitch mode will change to TO/GA. Verify that THR or
THR REF is displayed in the autothrottle mode annunciator.
787 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
Boeing Proprietary SP.4.5
If the pitch mode is VNAV PTH, VNAV ALT, VNAV SPD, or FLCH
SPD:
AUTOTHROTTLE engage switch .............................................Push
Verify THR REF, THR, SPD, IDLE, or HOLD as appropriate is
displayed in the autothrottle mode annunciator.
787 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
SP.4.6 Boeing Proprietary
Instrument Approach Using VNAV
Note: This procedure is not authorized using QFE.
Note: Operational approval required for the use of an MDA(H) as a
DA(H). If required to remain at or above MDA(H) during the
missed approach, missed approach must be initiated at least 50
feet above MDA(H).
Recommended roll modes for final approach:
• RNAV or GPS approach: LNAV
　
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