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时间:2011-04-12 10:37来源:蓝天飞行翻译 作者:航空
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A
747-400
MAINTENANCE MANUAL

DIFFERENTIAL AND SAFETY VALVE
SEE A
CABLE
LGDR3A (LEFT SIDE)

CABLE LGDR4A (RIGHT SIDE) LGDR3B (LEFT SIDE) LGDR4B (RIGHT SIDE)
WING GEAR DOOR
SAFETY VALVE

DIFFERENTIAL
SEE B FWD
CABLECABLE GDR3A (LEFT SIDE)GDR3B (LEFT SIDE) GDR4A (RIGHT SIDE)GDR4B (RIGHT SIDE)
DIFFERENTIAL AND SAFETY VALVE A
Installation of Differential and Safety Valve for the Wing Gear
Figure 401 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 MAINTENANCE MANUAL
CABLE RETAINER, BOLT AND LOCKWIRE
HYDRAULIC LINES  LGDR4B (RIGHT SIDE) LGDR3B (LEFT SIDE) CABLE 
DRUM  A-A  LGDR3A (LEFT SIDE) LGDR4A (RIGHT SIDE) CABLE 
CABLE PULLEYS 
DIFFERENTIAL OUTPUT ROD  A  GDR3B (LEFT SIDE) GDR4B (RIGHT SIDE) CABLE 

FWD 
BOLT (4 LOCATIONS) 
B DIFFERENTIAL  CABLE GDR3B (LEFT SIDE) GDR4B (RIGHT SIDE) 

Installation of Differential and Safety Valve for the Wing Gear
Figure 401 (Sheet 2)

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A

747-400
MAINTENANCE MANUAL

CABLE TENSION (POUNDS)

120
110
100
90
80
70
60
50
40

AMBIENT TEMPERATURE (`F)
Cable Tension for the Body Gear Alternate Extension System Figure 402
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A
747-400 MAINTENANCE MANUAL
 S 864-009
 (8)  
Open these circuit breakers and attach DO-NOT-CLOSE TAGS:

 (a)  
P6 Main Power Distribution Panel
 1) 6C29 ALT LG EXT WING L
 2) 6C30 ALT LG EXT WING R
 3) 6C31 ALT LG EXT BODY L
 4) 6C32 ALT LG EXT BODY R


 E.
Removal of the Differential and Safety Valve (Fig. 401)


 S 034-023
 (1)
Disconnect these electrical connectors on the electrical actuators:

 (a)  
Connector DM86 for the left actuator.

 (b)  
Connector DM89 for the right actuator.


 S 034-024
 (2)  
Disconnect the hydraulic lines from the safety valve.

 S 494-025

 (3)  
Install caps on the hydraulic lines.

 S 864-026

 (4)  
Put the ground release handle for the doors in the "Unlocked" position.

 S 494-027

 (5)
Put the rig pin AE/GD-5 (LH) or AE/GD-6 (RH) in the bus quadrant.

 S 494-028

 (6)  
Put the rig pin AE/GD-3 (LH) or AE/GD-4 (RH) in the ground release handle.

 S 494-029

 (7)  
Put the rig pin AE/GD-7 (LH) or AE/GD-8 (RH) as applicable in the uplock mechanism for the left or right wing gear.


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 ALL  ú ú 01 Page 406 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-030
 (8)  
On the valve you will remove, install clamps on the cables that are connected to the valve to hold them on side of the turnbuckle away from the valve. This will make sure the cables around the bus quadrant and the uplock mechanism stay in the correct position when you remove the cable that is around the differential.
 
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