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32-41-02
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A
747-400 MAINTENANCE MANUAL
S 864-021
(9)
Set the parking brake.
S 864-022
(10)
Remove pressure from hydraulic systems No. 1, 2 and 4 if it is not necessary (AMM 29-11-00/201).
S 864-025
(11)
Remove electrical power, if it is not necessary (AMM 24-22-00/201).
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747-400 MAINTENANCE MANUAL
BRAKE METERING VALVE ASSEMBLY - REMOVAL/INSTALLATION
____________________________________________________
1. General
_______
A. This procedure contains two tasks:
(1)
The removal of the brake metering valve assembly (referred to as the valve assembly)
(2)
The installation of the valve assembly.
B.
There are two valve assemblies on the airplane. One is in the wheel well for the right wing landing gear. The other is in the wheel well for the left wing landing gear.
C.
Each valve assembly contains a primary metering valve, an alternate metering valve and a wheel despin actuator. Bolts hold these parts together into one assembly. You will replace the assembly as a unit.
D.
You must remove hydraulic pressure before you remove the valve assembly. You will do the operational test of the hydraulic brake system after you install the valve assembly.
TASK 32-41-03-004-001
2. Brake Metering Valve Assembly Removal (Fig. 401)
_____________________________________
A. Standard Tools and Equipment
(1)
Wheel chocks
B.
References
(1)
AMM 09-11-00/201, Towing
(2)
AMM 29-11-00/201, Main Hydraulic Supply System
(3)
AMM 32-00-30/201, Landing Gear Door Locks
(4)
AIPC 32-42-78 Fig. 1
C.
Access
(1)
Location Zone
135 Wing Landing Gear Well, LH
136 Wing Landing Gear Well, RH
D.
Prepare for the Removal
S 494-044
WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1)
Install the ground locks in all landing gear (AMM 09-11-00/201).
(2)
Install chocks at each wheel.
(3)
Release the parking brake.
S 494-003
S 864-004
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
WING LANDING GEAR WHEEL WELL
CONTROL FWD QUADRANT
SEE B
SEE A
BRAKE CABLES
BRAKE METERING VALVE ASSEMBLY
SEE C
A
BRAKE METERING VALVE ASSEMBLY SEE D
B
Brake Metering Valve Assembly Installation Figure 401 (Sheet 1)
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32-41-03
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
35. NUT
34. WASHER
CONTROL QUADRANT
RIGGING PIN
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