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extended.
Do not use autoland.
Use flaps 20 and VREF 30 + 30 for landing.
This provides better handling qualities when
the slats are not fully extended.
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 9.23
9.23
Descent Checklist
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Notes . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . VREF 30 + 30, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Checklist
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . DOWN
Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20
SLATS DRIVE continued
Deferred Items
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC
9.24
9.24
[777-200]
[777-200ER]
[777-300]
[777-200LR, 777-300ER]
[] SLATS PRIMARY FAIL
Condition: The slats primary mode is failed.
Note: Plan additional time for slower slat operation.
Note: The slats will extend beyond midrange when
the airspeed is below 215 knots. For
go-around, do not exceed 215 knots until the
slats retract to midrange.
Note: The slats will extend beyond midrange when
the airspeed is below 239 knots. For
go-around, do not exceed 239 knots until the
slats retract to midrange.
Note: The slats will extend beyond midrange when
the airspeed is below 246 knots. For
go-around, do not exceed 246 knots until the
slats retract to midrange.
Note: The slats will extend beyond midrange when
the airspeed is below 256 knots. For
go-around, do not exceed 256 knots until the
slats retract to midrange.
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 9.25
9.25
1 Check FMC weight and CG entries.
SPEEDBRAKE EXTENDED
Condition: The speedbrakes are extended and one or
more of these occur:
•The radio altitude is between 15 and 800
feet
•The flap lever is in a landing setting
•A thrust lever is not at idle
[] SPOILERS
Condition: One or more spoiler pairs are failed.
Note: Roll rate may be reduced in flight.
Speedbrake effectiveness may be reduced in
flight and during landing.
[] STAB GREENBAND
Condition: The nose gear pressure switch disagrees
with the stabilizer green band calculated by
the FMC.
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC
9.26
9.26
1 C STAB cutout switch . . . . . . . . . . . . . . CUTOUT
1 R STAB cutout switch . . . . . . . . . . . . . . CUTOUT
[] STABILIZER C
Condition: The center stabilizer control path is failed.
Note: The left control wheel pitch trim switches
may be inoperative.
STABILIZER CUTOUT
Condition: Both stabilizer cutout switches are in
CUTOUT.
[] STABILIZER R
Condition: The right stabilizer control path is failed.
Note: The right control wheel pitch trim switches
may be inoperative.
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 9.27
9.27
1 THRUST ASYM COMP switch. . . . . Off, then AUTO
2 Choose one:
[] THRUST ASYM COMP
Condition: Thrust asymmetry compensation is failed or
OFF.
THRUST ASYM COMP message blanks:
THRUST ASYM COMP message stays shown:
Note: Manual control inputs are required
to compensate for asymmetric
thrust conditions.
December 10, 2007
777 Flight Crew Operations Manual
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波音777快速检查单 Quick Reference Handbook QRH(52)
