S 024-008
(7) Remove the hose assembly.
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A
737-300/400/500
MAINTENANCE MANUAL
SEE A
V-1
CLAMP
HOSE ASSEMBLY
CLAMP SEE B 0.50
INCH
0.00 SEE D
6.00 INCHES V-2 1.25
INCH
1.05
CLAMP V-4
V-30.90
INCH
0.70
CLAMP
SEE C
RIGHT SIDE VIEW OF LEFT GEAR SHOWN (HARNESS INSTALLATION ON RIGHT GEAR OPPOSITE EXCEPT WHEN NOTED)
Main Gear Electrical Harness Installation
Figure 401 (Sheet 1)
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A
737-300/400/500MAINTENANCE MANUAL
GRAVEL PROTECTION SHIELD
0.50
INCH
0.00
CLAMP
HOSE
FWD
V-2
RIGHT GEAR
1.30
INCHES (LEFT)1.10
1.60
INCHES (RIGHT)1.40
(ROTATED 180`)
A
CONNECTOR
0.5
INCH
0.3
0.2
INCH
0.1
B
GRAVEL PROTECTION SHIELD
CLAMP
HOSE
V-2
0.50
INCH
0.00
LEFT GEAR
RATCHET CLAMP
9.00 INCHES
TAPE RATCHET CLAMP
0.50 INCH
1.25
INCH
CLAMP 1.05
V-3
C
Main Gear Electrical Harness Installation
Figure 401 (Sheet 2)
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A 737-300/400/500MAINTENANCE MANUAL
MAIN GEAR SHOCK STRUT (REF)
A
AXLE (REF)
SEE E
HOSE
A
D1
INBD
FWD
B
A
CLAMP AXLE (REF)
CONDUIT
ASSEMBLY
B
J-BOX ASSEMBLY
A
D2
1 AIRPLANES WITHOUT BRAKE TEMPERATURE MONITORING WIRING
2 AIRPLANES WITH BRAKE TEMPERATURE MONITORING WIRING
Main Gear Electrical Harness Installation Figure 401 (Sheet 3)
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A 737-300/400/500MAINTENANCE MANUAL
FITTING CONE
ELBOW
HOSE
CONDUIT ASSEMBLY CLAMP
CONDUIT ASSEMBLY
A-A
(2 LOCATIONS)
J-BOX COVER REMOVED B-B
Main Gear Electrical Harness Installation
Figure 401 (Sheet 4)
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C96965
A 737-300/400/500MAINTENANCE MANUAL
TASK 32-11-87-004-060
3. AIRPLANES WITH BRAKE TEMPERATURE MONITORING WIRING; Main Landing Gear Electrical Harness Removal (Fig. 401)
____________________________________________
A. References
(1)
32-42-11/401, Transducer
B.
Access
(1)
Location Zone
310 Left Main Landing Gear
410 Right Main Landing Gear
C.
Procedure
S 034-056
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