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landing position, or when either thrust lever is not
closed.
[]SLATS DRIVE
[]SLATS PRIMARY FAIL
SPEEDBRAKE EXTENDED
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
9.10
9.10
Condition: Increased spoiler drag due to loss of pressure in
center hydraulic system and low altitude cruise.
RAM AIR TURBINE switch. . . . . . Push and hold for 1 second
[Reduces drag by enabling center hydraulic system to power and stow two
spoiler pairs.]
Fly LRC speed.
[Improves range.]
Condition: Two spoiler pairs are inoperative.
Note: Roll rate may be reduced in flight. Speedbrake
effectiveness may be reduced in flight and during
landing.
If landing using flaps 25:
Note: Use flaps 25 and VREF25 +5 for landing.
[Flap effectiveness is reduced.]
If landing using flaps 30:
Note: Use flaps 30 and VREF30 +5 for landing.
[Flap effectiveness is reduced.]
Condition: One or more spoiler panels are inoperative.
Note: Roll rate may be reduced in flight. Speedbrake
effectiveness may be reduced in flight and during
landing.
[]SPOILER DRAG
[]SPOILER PAIRS
[]SPOILERS
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 9.11
9.11
Condition: Nose gear pressure switch disagrees with computed
stabilizer greenband.
FMC WEIGHT and CG Entries. . . . . . . . . . . . . . . . . . . . . Check
[An incorrect entry may cause an incorrect stab greenband calculation.]
Condition: Uncommanded stabilizer motion is detected or
stabilizer is inoperative.
# STABILIZER CUTOUT switches (Both). . . . . . . . . . CUTOUT
[Prevents subsequent uncommanded or inappropriate stabilizer motion.]
# Do not exceed current airspeed.
[Nose down elevator authority is limited.]
Stabilizer is inoperative. Pitch trim remains available in the
normal flight control mode.
GND PROX FLAP OVRD . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
Note: Use flaps 20 and VREF30 + 20 for landing.
[Provides sufficient elevator authority for landing.]
Do not accomplish the following checklist:
FLIGHT CONTROLS
Condition: Both stabilizer cutout switches are in CUTOUT.
[]STAB GREENBAND
[]STABILIZER
STABILIZER CUTOUT
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
9.12
9.12
Condition: Left stabilizer control path is inoperative.
L2 stabilizer CUTOUT switch. . . . . . . . . . . . . . . . . . . CUTOUT
[Prevents subsequent uncommanded or inappropriate stabilizer motion.]
Note: Left control wheel pitch trim switches may be
inoperative.
Condition: Right stabilizer control path is inoperative.
R2 stabilizer CUTOUT switch. . . . . . . . . . . . . . . . . . . CUTOUT
[Prevents subsequent uncommanded or inappropriate stabilizer motion.]
Note: Right control wheel pitch trim switches may be
inoperative.
Condition: Some stall protection functions are inoperative.
Note: Any stall indications should be considered valid.
[]STABILIZER L2
[]STABILIZER R2
[]STALL PROTECTION
December 15, 2006
787 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Flight Instruments, Displays Section 10
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary TOC.10.1
Table of Contents
[N]NAC.I1R0 NSoPnE-NEorDm aUl CNheRckEliLstsI-AFlBighLt EIn st.r u.m . e.n t.s ,. D. i.s p.l a.y .s . . . . . . . . . . . . . . . . . . . 10.1
[] ALTN ATTITUDE CAPT, F/O . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
BARO SET DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
CHKL INCOMPLETE NORM . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
CHKL NON- NORMAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
[] EFIS/DSP PANEL L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
[] HUD SINGLE OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.2
HUD SYS CAPT, F/O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.2
[] HUD TAKEOFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.2
u LOSS OF ALL DISPLAYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.4
SGL SOURCE APPROACH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.5
[] SGL SOURCE ATTITUDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.6
　
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