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COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE
(REF 29-31-00, FIG. 101) SWITCH - SYS R PRESS, S32 (REF 29-31-00, FIG. 101) SWITCH - SYS R ACMP PRESS, S30 (REF 32-44-00, FIG. 101) SWITCH - PARK BRAKE, S459 (REF 29-11-00, FIG. 101) SWITCH - RESERVE BRAKE, S10390
(REF 32-44-00, FIG. 101) VALVE - ACCUMULATOR ISOLATION (REF 32-30-00, FIG. 101) VALVE, MAIN GEAR SELECTOR (REF 32-42-00, FIG. 101) VALVE, AUTOBRAKE SHUTTLE, L&R TRANSDUCER, HYD BRAKE SOURCE, TS90 2 1 R MAIN GEAR WHEEL WELL 32-41-00
(REF 29-11-00, FIG. 101)VALVE - ALTERNATE BRAKE SELECTOR VALVE - SYSTEM ISOLATION, M10118 (REF 29-11-00, FIG. 101) VALVE - STANDPIPE SELECTOR, V10117 (REF 32-44-00, FIG. 101) VALVE AND MOTOR - PARKING BRAKE, V41 2 1 R MAIN GEAR WHEEL WELL 32-41-04
VALVE ASSEMBLY - BRAKE METERING 2 2 FWD BULKHEAD L (R) MAIN GEAR WHEEL WELL, 32-41-03
* SEE WM EQUIPMENT LIST
Component Index
Figure 101 (Sheet 2)
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SHT 2 FWD BLKHD) VALVE MODULES (MAIN GEAR WHEEL WELL NORMAL & ALTERNATE BRAKE METERING BSEE
CABLES BRAKE
113AL
DOOR, 821 FWD CARGO
PEDAL MECHANISM BRAKE BUS ASEE BRAKE PEDALS FIRST OFFICER'S LEFT & RIGHT GEAR DOORS MAIN LANDING
HOUSING CONTROL RODS (REF) RUDDER SYSTEM BRAKE PEDALS CAPTAIN'S
HOUSING
(REF) CONTROL RODS RUDDER SYSTEM
(2 PLACES) CONTROL RODS BRAKE SYSTEM (REF) RODS BUS (2 PLACES) CONTROL RODS BRAKE SYSTEM
Figure 102 (Sheet 1) Component Location A BRAKE PEDAL BUS MECHANISM (REF) CABLES CONTROL
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CONTROL CABLES
(REF)
QUADRANT
(PART OF MODULE)
BRAKE METERING VALVE ASSEMBLY DE-SPIN ACTUATOR (PART OF VALVE ASSEMBLY)
ROD ASSEMBLY
WHEEL WELL
(REF)
FORWARD BULKHEAD (REF) INPUT CRANK (REF)
BRAKE METERING VALVE ASSEMBLY
(LEFT SIDE INSTALLATION SHOWN;
RIGHT SIDE INSTALLATION SIMILAR)
B
ALTERNATE BRAKE HYDRAULIC BRAKE SELECTOR VALVE CHARGING LINE SOURCE TRANSDUCER
SEE D
(REF) SEEC
PARKING BRAKE ALTERNATE
ACCUMULATOR SOURCE
(REF) SELECT VALVE PRESSURE SWITCH,
HYDRAULIC
S415 BRAKE SOURCE TRANSDUCER, TS90
C ALTERNATE BRAKE SELECTOR VALVE
D
Component Location Figure 102 (Sheet 2)
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P1 PANEL BRAKE SOURCE P3 PANEL
LIGHT, L491 BRAKE PRESSURE
SEE E INDICATOR, N10
SEE F RESERVE
BRAKES
ON
FLT COMPT
BRAKE LIGHT, L491 SOURCE
a
BRAKE 4 PRESS
BRAKE SOURCE LIGHT, L491
PSI X 1000 30
E
21
BRAKE
BRAKE PRESSURE
DISCONNECT
INDICATOR, N10
HYDRAULIC LINE (REF)
F
HYDRAULIC BRAKE
SEE G
FWD
HYDRAULIC BRAKE FWD
(REF) WHEEL AND TIRE BRAKE DISCONNECT G
Component Location
Figure 102 (Sheet 3)
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HYDRAULIC BRAKE SYSTEM - MAINTENANCE PRACTICES
______________________________________________
1. General
_______
A. This procedure contains two tasks. The first task is a procedure to bleed the main gear landing brakes. The second task is a test for proper operation of the antiskid module hydraulic fuses.
TASK 32-41-00-872-001
2. Procedure to Bleed the Main Landing Gear Wheel Brake System
___________________________________________________________
A. General
(1)
When a brake assembly is replaced, the new brake should be prefilled before installation on the airplane and it is not necessary to bleed the brakes.
B.
Consumable Materials
(1)
D00153 Hydraulic Fluid - BMS 3-11, Type IV
C.
References
