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时间:2010-06-11 07:40来源:蓝天飞行翻译 作者:admin
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Condition: The ANTISKID INOP light illuminated indicates a
system fault is detected by the antiskid system.
AUTO BRAKE SELECT SWITCH . . . . . . . . . . . . . . . . . . . . .OFF
Brake with caution.
Condition: The AUTO BRAKE DISARM light illuminated indicates
the auto brake has disconnected after being set.
On ground:
AUTO BRAKE SELECT SWITCH . . . . . . . . . . . . . . . . . .OFF
If the AUTO BRAKE DISARM light remains illuminated:
DO NOT TAKEOFF.
Inflight:
AUTO BRAKE SELECT
SWITCH . . . . . . . . . . . . . . . . . . . . . . OFF THEN RESELECT
If the AUTO BRAKE DISARM Light re-illuminates:
AUTO BRAKE SELECT SWITCH . . . . . . . . . . . . . . . .OFF
Use manual brakes.
Condition: The brake accumulator has no nitrogen precharge.
Accumulator braking is not available.
Note: If hydraulic system indications are normal, brake
operation is unaffected.
ANTISKID INOPERATIVE
AUTO BRAKE DISARM
BRAKE PRESSURE INDICATOR ZERO PSI
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

14.2
14.2
Condition: The landing gear lever cannot be placed to the UP
position in the normal manner due to one or more of
the following:
• failure of the landing gear lever lock solenoid
• failure of the air/ground system
Note: Do not use FMC fuel predictions.
LANDING GEAR lever . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
If the takeoff configuration warning remains silent after the
flaps are fully retracted and the thrust levers are beyond the
vertical position:
Note: This condition indicates a failure of the landing
gear lever lock solenoid.
LANDING GEAR OVERRIDE trigger . . . . . . . . . . . . . . . Pull
Landing gear lever . . . . . . . . . . . . . . . . . . . . . . . . . UP & off
Continued on next page
GEAR LEVER WILL NOT MOVE UP
AFTER TAKEOFF
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 14.3
14.3
Continued from previous page
If the takeoff configuration warning sounds when flaps are
fully retracted:
Note: This condition indicates a failure of the air/ground
system.
LANDING GEAR AIR/GND RELAY
AND LIGHTS C/B (P6) . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
Plan to land at the nearest suitable airport.
CAUTION: Do not operate the speedbrakes in flight.
------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . . . . . . . . VREF___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . Completed
------------------------DEFERRED ITEMS ------------------------------
==> APPROACH
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Continued on next page
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

14.4
14.4
Continued from previous page
If the takeoff configuration warning sounds when flaps are fully
retracted: (continued)
------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN detent
Landing gear lever . . . . . . . . . . . . . . . . . . . . . . . . . . . .Down
LANDING GEAR AIR/GND RELAY
AND LIGHTS C/B (P6) . . . . . . . . . . . . . . . . . . . . . . . . . .Reset
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
LANDING GEAR AIR/GND RELAY
AND LIGHTS C/B (P6) . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___, green light
Manually deploy the speedbrakes immediately upon
touchdown.
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 14.5
14.5
Condition: The landing gear lever will not move from the UP
position, or all landing gear remain up after
attempting manual gear extension.
----------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Total fuel quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
Manual gear extension may require up to 10 minutes to
 
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