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* Flap control cables (WFA, WFB)
* Flap follow-up cables (WFFA, WFFB)
* Stabilizer control cables (STA, STB)
* Speedbrake control cables (SBA, SBB)
* Spoiler control cables (WSA, WSB).
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL CABLES
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FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL CABLES
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL CABLES
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Purpose
The flight control panel has hydraulic control switches and
caution lights for several of the flight control systems.
Location
The flight control panel is in the flight compartment on the P5
forward overhead panel.
Flight Control Switch
Each flight control switch has these positions:
* STDBY RUD position: Removes system pressure from
ailerons, elevators, elevator feel computer, and rudder.
Turns on the standby pump and pressurizes the standby
power control unit.
* OFF position: Removes system pressure from ailerons,
elevators, elevator feel computer, and rudder.
* ON position: System pressure is on to the ailerons,
elevators, elevator feel computer, and rudder. The ON
position is normal with the guard closed.
Flight Control Low Pressure Light
Each flight control low pressure light monitors the pressure to
the ailerons, elevators, elevator feel computer, and rudder.
Each flight control low pressure light monitors the position of
the standby rudder shutoff valve when the flight control switch is
in the STDBY RUD position.
Flight Spoiler Switch
Each flight spoiler switch has these positions:
* OFF position: Removes system pressure from the flight
spoilers.
* ON position: System pressure is on to the flight spoilers. The
ON position is normal with the guard closed.
Yaw Damper Switch and Warning Light
The yaw damper switch controls the yaw damper system
operation. The yaw damper warning light comes on when the
system is disengaged. See the yaw damper system section for
more information. (SECTION 22-23)
Standby Hydraulic Low Quantity and Low Pressure Lights
The standby hydraulic low quantity light comes on when the
standby reservoir quantity is low. The standby hydraulic low
pressure light comes on when the standby system pressure is
low. See the standby hydraulic system section for more
information. (SECTION 29-22)
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL PANEL
EFFECTIVITY
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Alternate Flaps Arm Switch and Control Switch
The alternate flaps arm switch and the alternate flaps control
switch are used for alternate flaps operation. See the TE flap
system section for more information about the alternate flaps
switches and the functional description of alternate operation.
(SECTION 27-51) See the LE flap and slat control system
section for more information about alternate operation.
(SECTION 27-81)
Flight Control Panel Warning Lights
The feel differential pressure light comes on when there is a
difference between the system A and system B metered
pressures in the elevator feel computer. See the elevator and
tab control system section for more information about the
elevator feel computer functional description. (SECTION 27-31)
The speed trim fail light comes on when the speed trim function
in the flight control computers (FCCs) is not available. See the
digital flight control system section for more information.
(SECTION 22-11)
The mach trim fail light comes on when the mach trim function
in the flight control computers (FCCs) is not available. See the
digital flight control system section for more information.
(SECTION 22-11)
The autoslat fail light comes on when the autoslat function is not
available. See the LE autoslat system section for more
　
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