(1)  
Release the parking brake.

 (2)  
Remove the power from hydraulic systems A and B (AMM 29-15-00/201).

 S 032-031

 (3)  
Disconnect the electrical plug from the control valve.

 (a)  
Seal the receptacle and plugs with caps.

 S 842-029
 S 842-030
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-43-46
 ALL  ú ú 01 Page 205 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AUTOBRAKECONTROL
OVERHEAD MODULE
FLOW  FLOW
FUSE FUSE SEE A
ACCUMULATOR ALT BRAKE
ISOLATION SELECTOR VALVE
VALVE
ANTISKID

ANTISKID
BRAKE METERING SHUTTLE SHUTTLE
VALVE ASSY LEFT VALVES
VALVES
(2 PLACES) ALTERNATE RIGHT
ANTISKID LEFTPARKING BRAKEALTERNATE CONTROL ANTISKIDSHUTOFF VALVEANTISKID VALVECONTROLOUTBDCONTROL
BRAKE AUTOBRAKE
VALVES
VALVE  INBD
FLOW SHUTTLE
FUSES VALVES
BRAKE INBD
RIGHT ANTISKID
FLOW OUTBD
CONTROL VALVES  FUSES
SERVICING GAGE
ACCUMULATOR
WHEEL WELL BRAKE PRESS
AFT BULKHEAD TRANSMITTER BL 0
STA 727
VIEW LOOKING AFT
HYDRAULIC LINE
CONTROL (PRESSURE IN)MODULE
HYDRAULIC LINE (PRESSURE RETURN) SERVO VALVE
O-RING
PRESSURE SWITCH SOLENOID
RETAINERSHUTOFF VALVE
PRESSURE SWITCH
O-RING
RETAINER
HYDRAULIC LINE
RETAINER
(PRESSURE TO BRAKES)
FILTERSEAL PLATE O-RING
ELECTRICAL
RETAINER CONNECTOR (EXAMPLE)
O-RINGSOLENOID
SHUTOFF CAP RETAINER
VALVE SCREW
(4 LOCATIONS) CAP
SERVO
COVER SCREW VALVE
1
ABEX MODULES (4 LOCATIONS) A 1
Autobrake Pressure Control Module Component Locations
Figure 201 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-43-46
 ALL  ú ú 01 Page 206 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ELECTRICAL 
CONNECTOR  PRESSURE  PACKING RETAINER (QTY 2)  CONNECTOR ELECTRICAL 
SWITCH 
UNION  PACKING 
PACKING 

PACKING
PRESSURE SWITCH
ELECTRICAL
RETAINER (QTY 2) CONNECTOR
PACKING
HYDRAULIC LINE
UNION PACKING
VALVE
MODULE UNION PACKING
GASKET
GASKET
ELECTRICAL CONNECTOR
PACKING
WASHER (4 LOCATIONS)
SOLENIOD
BOLT VALVE
(4 LOCATIONS)
SERVO VALVE FWD ASSEMBLY
WASHER
(4 LOCATIONS)
BOLT
(4 LOCATIONS)
A2
2
TEXTRON MODULES
Autobrake Pressure Control Module Installation Figure 201 (Sheet 2)
G26156
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-43-46
 ALL  ú ú 01 Page 207 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 022-032
 (4)  Remove the mounting screws and lift the control valve from the module.
 S 022-033
 CAUTION: WHEN YOU REMOVE THE CONTROL VALVE AND THE SEAL PLATE, MAKE SURE
_______ THAT NO CONTAMINANTS GO INTO THE OPEN PORTS ON THE MODULE. CONTAMINANTS IN THE MODULE CAN CAUSE DAMAGE TO IT.
 (5)  Remove the seal plate from the module.
 TASK 32-43-46-402-034
 8. Autobrake Pressure Control Module Servo Valve Installation
___________________________________________________________
 A. References
 (1)  
32-43-01/501, Automatic Braking System

 B.
Access

 (1)  
Location Zone
 216 Left Main Wheel Well
 217 Right Main Wheel Well

 C.
Procedure

 S 422-035
 (1)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 3(86)