787QRH快速检查单(41)

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D615Z003 Boeing Proprietary
8.16
8.16
Condition: Smoke is detected in door 4 upper crew rest
compartment.
Cabin crew communications. . . . . . . . . . . . . . . . . . . Establish
If smoke is persistent:
Plan to land at the nearest suitable airport.
[]SMOKE REST UPR DR 4
December 15, 2006
787 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Flight Controls Section 9
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary TOC.9.1
Table of Contents
[N]NAC.U9 NToOn-N SoPrmEaEl CDheBckRliAstsK-FlEig h t .C .o .n t.r o.l s. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.1
[] CRUISE FLAPS SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.1
[] FLAPS DRIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.1
[] FLAPS PRIMARY FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.2
[] FLAP/SLAT CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.2
[] FLIGHT CONTROL MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.3
[] FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.4
FLT CONTROLS LOCKED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.4
[] PITCH DOWN AUTHORITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.4
[] PITCH UP AUTHORITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.5
[] PRI FLIGHT COMPUTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.6
[] ROLL LEFT AUTHORITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.7
[] ROLL RIGHT AUTHORITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.8
[] ROLL/YAW ASYMMETRY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.8
[] SLATS DRIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.9
[] SLATS PRIMARY FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.9
SPEEDBRAKE EXTENDED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.9
[] SPOILER DRAG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10
[] SPOILER PAIRS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10
[] SPOILERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10
[] STAB GREENBAND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.11
[] STABILIZER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.11
STABILIZER CUTOUT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.11
[] STABILIZER L2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.12
[] STABILIZER R2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.12
[] STALL PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.12
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.9.2 D615Z003 Boeing Proprietary
Non-Normal Checklists -
Flight Controls
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 9.1
9.1
NNC.9 Non-Normal Checklists-Flight Controls
Condition: A fault is detected in the automatic speedbrake
system.
Note: Do not arm speedbrake lever.
[Prevents inadvertent inflight extension.]
Note: Manually extend speedbrakes after landing.
Condition: The cruise flaps system is in the incorrect position.
Note: Do not use FMC fuel predictions.
Condition: Flap drive mechanism has failed.
Do not use alternate flaps.
[Asymmetry protection is not provided in alternate mode.]
GND PROX FLAP OVRD . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
Note: Do not use FMC fuel predictions with flaps extended.
If flap position UP or 1:
Note: Position flap lever to 1 and use VREF30 + 40 for
landing.
If flap position between 1 and 5 or at 5:
Note: Use current flaps and VREF30 + 40 for landing.
If flap position between 5 and 20:
Note: Use current flaps and VREF30 + 20 for landing.
If flap position 20 or greater:
Note: Use current flaps and VREF20 for landing.
Do not accomplish the following checklist:
FLAPS PRIMARY FAIL
[]AUTO SPEEDBRAKE
[]CRUISE FLAPS SYS
[]FLAPS DRIVE
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
　
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