曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

JAMMED OR RESTRICTED FLIGHT CONTROLS . . . . . . . . . 0.18
LOSS OF THRUST ON BOTH ENGINES . . . . . . . . . . . . . . . . 0.20
RADIO TRANSMIT CONTINUOUS(STUCK
MICROPHONE SWITCH) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.22
SMOKE/FUMES REMOVAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.24
STABILIZER TRIM INOPERATIVE . . . . . . . . . . . . . . . . . . . . . . 0.26
TAILSTRIKE ON TAKEOFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.28
UNCOMMANDED RUDDER/YAW OR ROLL . . . . . . . . . . . . 0.30
VOLCANIC ASH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.34
WINDOW DAMAGE - DCPCS AIRPLANES . . . . . . . . . . . . . . . 0.36
WINDOW DAMAGE - CPCS AIRPLANES . . . . . . . . . . . . . . . . 0.38
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.0.2
Non-Normal Checklists -
Unannunciated Checklists
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 0.1
0.1
NNC.0 Non-Normal Checklists-Unannunciated
Condition: During a ground start, and abort engine start
conditions occurs.
If the ENGINE START switch is in GRD:
Motor the engine for 60 seconds.
ENGINE START switch . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If the ENGINE START switch is in OFF:
After N2 decreases below 20%:
ENGINE START switch . . . . . . . . . . . . . . . . . . . . . . . GRD
Motor the engine for 60 seconds.
ENGINE START SWITCH . . . . . . . . . . . . . . . . . . . . . .OFF
ABORTED ENGINE START
ENGINE START SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

0.2
0.2
Condition: A concentration of air conditioning smoke/fumes is
identified.
OXYGEN MASKS AND SMOKE GOGGLES
(if required) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
CREW COMMUNICATIONS
(if required) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH
RECIRCULATION FAN SWITCH . . . . . . . . . . . . . . . . . . . . .OFF
[Eliminates possible source of smoke/fumes.]
If smoke/fumes stop:
Continue flight with the recirculation fan switch OFF.
If smoke/fumes continue:
ISOLATION VALVE SWITCH . . . . . . . . . . . . . . . . . . . CLOSE
R PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If smoke/fumes stop:
Continue flight with the R PACK switch OFF and
ISOLATION VALVE switch CLOSE.
If smoke/fumes continue:
R PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
L PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If smoke/fumes stop:
Continue flight with the L PACK switch OFF and
ISOLATION VALVE switch CLOSE.
If smoke/fumes continue:
L PACK SWITCH. . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Plan to land at nearest suitable airport.
Continued on next page
AIR CONDITIONING SMOKE/FUMES
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 0.3
0.3
Continued from previous page
Accomplish the SMOKE/FUMES REMOVAL checklist, if
required.
Condition: Pitch attitude not consistent with existing phase of
flight, altitude, thrust, and weight, or noise and/or low
frequency buffeting.
Crosscheck ground speed and winds provided by the IRS
and FMC to determine airspeed accuracy if indicated
airspeed is questionable.
Note: Erroneous or unreliable airspeed indications may be
caused by blocked or frozen pitot-static system(s), or
a severely damaged or missing radome.
AIRSPEED UNRELIABLE
AIRPLANE ATTITUDE/THRUST . . . . . . . . . . . . . . . . . . ADJUST
Maintain airplane control. Attitude and thrust information
is provided in the Performance-Inflight section.
PITOT STATIC HEAT . . . . . . . . . . . . . . . . . . . . . . . . .CHECK ON
MACH/AIRSPEED INDICATORS . . . . . . . . . . . CROSS CHECK
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

0.4
0.4
Condition: Automatic pressurization mode has failed or the
cabin altitude is not under control.
Increasing thrust may ensure adequate air supply to control
cabin altitude.
ENGINE BLEED AIR SWITCHES . . . . . . .ON (ONE AT A TIME)
PACK SWITCHES . . . . . . . . . . . . . . . . AUTO (ONE AT A TIME)
　
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