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information about the LE autoslat system functional
description. (SECTION 27-83)
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL PANEL
EFFECTIVITY
GUN ALL 27-09-00
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D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-09-00-003
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL PANEL
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL PANEL
EFFECTIVITY
GUN ALL 27-09-00
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D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-09-00-003
THIS PAGE IS INTENTIONALLY LEFT BLANK
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROL PANEL
27-09-00
Page 12
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Purpose
The flight controls hydraulic modular packages have the
components that control the hydraulic pressure to the primary
flight controls and to the flight spoilers.
Location
The flight controls hydraulic modular packages are on the
forward bulkhead of the main landing gear wheel well. The
system A package is on the left and the system B package is on
the right.
Physical Description
Each flight controls hydraulic modular package is a manifold
assembly and contains these components:
* Flight controls shutoff valve
* Spoiler shutoff valve
* Low pressure warning switch
GUN 001-010, 201-999; AIRPLANES WITH 65-44891-1 THRU -7
FCM
* Compensator cartridge.
GUN ALL
The flight controls shutoff valve and spoiler shutoff valve each
have a position indicator/manual override lever with positions 1
and 2.
Functional Description
The flight control shutoff valves have 28v dc motors. The
respective flight control switch on the flight control panel
controls each valve. They are normally open which allows
pressure to the flight controls.
The spoiler shutoff valves have 28v dc motors. The respective
spoiler switch on the flight control panel controls each valve.
They are normally open which allows pressure to the spoilers.
The low pressure warning switch is downstream of the flight
control valve. It turns on an amber light when it senses low
pressure to the flight controls.
GUN 001-010, 201-999; AIRPLANES WITH 65-44891-1 THRU -7
FCM
The compensator cartridge maintains return fluid pressure of
40-70 psi to the aileron, rudder, and elevator PCUs when the
hydraulic system is OFF. This provides wind gust protection for
the control surfaces.
GUN ALL
Training Information Point
The system A and system B flight controls hydraulic modular
package are interchangeable.
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGES
EFFECTIVITY
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D633A101-GUN Jun 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-09-00-004
The flight controls shutoff valves and the spoiler shutoff valves
are interchangeable. You can replace the valve and motor as a
unit or you can replace just the motor.
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGES
EFFECTIVITY
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Page 14
D633A101-GUN Oct 10/2005
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-09-00-004
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGES
FLIGHT CONTROLS MULTIPLE USE SYSTEMS/UNITS - FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGES
EFFECTIVITY
GUN ALL 27-09-00
Page 15
D633A101-GUN Feb 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-09-00-004
Purpose
The flight controls shutoff valves control the system A and B
pressure to the aileron PCUs, elevator PCUs, elevator feel
computer, and the main rudder PCU.
Location
The flight controls shutoff valves are on the right side of each
flight controls hydraulic modular package.
Physical Description
Each flight controls shutoff valve is a spool valve attached by
four bolts to a cavity of the flight controls hydraulic modular
package. A splined cam converts rotary motor action to linear
spool travel.
　
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