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Note: Present latitude and longitude are shown on the ALTN
NAV RADIO page.
Note: Tune the left ILS receiver by entering frequency and
course on the left tuning and control panel. ILS will
display on the Captain’s PFD.
Note: Refer to Performance–Inflight chapter for VREF speed
and other applicable performance information.
LANDING ALTITUDE selector. . . . . . . . . . . Pull, set manually
[From LANDING ALTITUDE checklist.]
Do not accomplish the following checklist:
LANDING ALTITUDE
Condition: The FMC calculated holding pattern exceeds the
maximum protected airspace limits.
Decrease airspeed or advise ATC you are unable to comply
with required holding airspace limits.
[]FMC
[]FMC HOLD AIRSPACE
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
11.2
11.2
Condition: LNAV is armed and the airplane is not on an intercept
heading to the active leg.
Condition: A message is in the FMC message window.
Condition: VNAV is selected, and gross weight, cost index or
cruise altitude are not entered.
FMC PERF INIT page. . . . . . . . . . . . . . . . . . . . . . . . . . . . Select
Ensure all required data is entered.
Condition: Airplane is not on FMC origin runway when either
engine’s thrust is in the takeoff range.
Condition: The FMC is unable to achieve the required time of
arrival within the allowable time error.
Condition: The FMC calculation of airplane position is based on
conflicting data.
Condition: GPS has failed.
FMC INTERCEPT HDG
FMC MESSAGE
[]FMC PERF UNAVAIL
FMC RUNWAY DISAGREE
FMC UNABLE RTA
FMC VERIFY POSITION
GPS
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 11.3
11.3
Condition: FMC estimated fuel at the destination is less than the
entered RESERVES fuel.
The INSUFFICIENT FUEL message may be caused by an
engine fuel leak. For indications of an engine fuel leak,
check:
• total fuel remaining on EICAS compared to planned fuel
remaining
• fuel flow indications, for an engine with excessive fuel
flow
• individual tank quantities
• totalizer compared to calculated quantities (PROGRESS
page 2/3). The TOTALIZER value is the sum of the
individual tank quantities. The CALCULATED value is the
totalizer value at engine start minus fuel used (calculated
using fuel flow rates and time).
If there is an indication of an engine fuel leak:
Accomplish the FUEL LEAK checklist.
If FUEL DISAGREE message is displayed without any
indication of an engine fuel leak:
Obtain a more direct route to the destination, or divert to
an alternate with shorter routing.
Condition: During inertial reference system alignment, excessive
airplane motion is detected.
Airplane must be stopped to allow IRS alignment to
complete.
When IRS ALIGN MODE memo message is no longer
displayed:
Continue normal operation.
[]INSUFFICIENT FUEL
[]IRS MOTION
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
11.4
11.4
Condition: The airplane may not follow an LNAV turn because
bank angle is limited by available thrust or buffet.
If unable to remain within protected airspace, advise ATC.
Condition: Backup sources for airspeed and altitude are being
used instead of air data.
Avoid abrupt control inputs.
[From FLIGHT CONTROL MODE checklist. Airplane response is changed
by simplified elevator feel and rudder ratio systems.]
Note: Altitude is from GPS and is approximately equal to
MSL altitude. Altimeter cannot be used above
transition level to accurately maintain flight levels.
Note: Airspeed is calculated using angle of attack. Airspeed
errors of up to 15 KIAS may exist at approach speeds.
GRND PROX FLAP OVRD. . . . . . . . . . . . . . . . . . . . . . . . OVRD
[From FLIGHT CONTROL MODE checklist.]
Note: Inoperative items:
• envelope protection functions
• autopilot
• flight directors
• autothrottles
• PFD flap maneuvering speeds; refer to Flap
Maneuvering Speed table in Performance–Inflight
chapter.
[Inoperative items envelope protection functions and autopilot from
FLIGHT CONTROL MODE checklist.]
Note: Yaw damper is degraded.
[From FLIGHT CONTROL MODE checklist.]
Note: Manual control inputs are required to compensate for
　
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