733QRH快速检查单(37)

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OUTFLOW VALVE SWITCH . . . . . . . . . . . . . . . . OPEN
Position outflow valve to full open. This causes
the cabin airflow to carry smoke/fumes aft.
Note: On airplanes with DCPCS, the outflow valve
can take up to 20 seconds to open.
Plan to land at the nearest suitable airport.
If packs are off and smoke/fumes source is confirmed to be
on the flight deck:
CAUTION: Window should not be opened unless the
source is confirmed to be originating on the
flight deck.
NORMAL HOLDING AIRSPEED . . . . . . . . . . . . ESTABLISH
[High airspeed may prevent opening the window.]
FIRST OFFICER'S SLIDING WINDOW . . . . . . . . . . . . OPEN
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

8.12
8.12
Condition: A fire is detected in the main wheel well.
Observe extend limit speed (270K/.82M)
LANDING GEAR LEVER . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Note: Do not use FMC fuel predictions with landing gear
extended.
If the landing gear must be retracted for airplane
performance, leave the landing gear extended for 20
minutes after the WHEEL WELL fire warning light has
extinguished.
LANDING GEAR LEVER (if required)
(235 Kts maximum) . . . . . . . . . . . . . . . . . . . . . . . . UP & OFF
Plan to land at the nearest suitable airport.
WHEEL WELL FIRE
June 3, 2005
737 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Flight Controls Section 9
Copyright © The Boeing Company. See title page for details.
 TOC.9.1
Table of Contents
NNAC.L9 NLo nF-LNoArmPaSl C UhePck LlisAts-NFlDighItN CGon tr o.l s. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.1
AUTO SLAT FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.2
FEEL DIFFERENTIAL PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . 9.2
FLAP LOAD RELIEF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.2
FLIGHT CONTROL LOW PRESSURE . . . . . . . . . . . . . . . . . . . . . 9.3
JAMMED OR RESTRICTED FLIGHT CONTROLS . . . . . . . . . . 9.4
LEADING EDGE FLAPS TRANSIT . . . . . . . . . . . . . . . . . . . . . . . 9.8
MACH TRIM FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.12
RUNAWAY STABILIZER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.12
SPEED BRAKE DO NOT ARM . . . . . . . . . . . . . . . . . . . . . . . . . . 9.13
SPEED TRIM FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.13
STABILIZER OUT OF TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.13
STABILIZER TRIM INOPERATIVE . . . . . . . . . . . . . . . . . . . . . . 9.14
STANDBY RUDDER ON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.16
TRAILING EDGE FLAP ASYMMETRY . . . . . . . . . . . . . . . . . . . 9.18
TRAILING EDGE FLAP DISAGREE . . . . . . . . . . . . . . . . . . . . . 9.20
TRAILING EDGE FLAPS UP LANDING . . . . . . . . . . . . . . . . . . 9.24
UNCOMMANDED RUDDER/YAW OR ROLL . . . . . . . . . . . . 9.28
YAW DAMPER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.31
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.9.2
Non-Normal Checklists -
Flight Controls
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 9.1
9.1
NNC.9 Non-Normal Checklists-Flight Controls
Condition: Leading edge devices and trailing edge flaps cannot
be extended.
Burn off fuel to reduce touchdown speed.
Set VREF 40 + 55 knots.
[If tire placard speed is exceeded, tire failure may occur.]
Check the appropriate Non-Normal Configuration Landing
Distance table in the ADVISORY INFORMATION section of
the Performance-Inflight chapter.
Maintain flaps up maneuvering speed until on final.
Limit bank angle to 15° until reaching flaps up maneuvering
speed.
----------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
GROUND PROXIMITY FLAP/GEAR
INHIBIT switch (as installed) . . . . . . . . . . FLAP/GEAR INHIBIT
GROUND PROXIMITY FLAP
INHIBIT switch (as installed) . . . . . . . . . . . . . . . .FLAP INHIBIT
Landing data . . . . . . . . . . VREF 40 + 55 knots, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
　
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