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时间:2011-04-02 16:53来源:蓝天飞行翻译 作者:航空
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Put a new seal plate over the ports of the control module.

 S 422-036

 (2)  
Put the servo valve over the seal plate and install the four capscrews.

 S 432-037

 (3)  
For the servo valves with the Suffix A after the serial number, tighten the screws 65 to 70 pound-inches.

 S 432-038

 (4)  
For the servo valves without the Suffix A, tighten the screws 95 to 100 pound-inches.

 S 432-039

 (5)  
Connect the electrical plug and attach it to the servo valve with lockwire.

 (6)  
Do a test on the control module (AMM 32-43-01/501).


 S 722-040
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 32-43-46
 ALL  ú ú 01 Page 208 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 32-43-46-002-041
 9. Pressure Switch Removal (Fig. 201)
_______________________
 NOTE: This applies to the pressure switch of the solenoid shutoff valve and
____
 the pressure switch of the servo valve.

 A. References
 (1)  
29-15-00/201, Hydraulic Systems

 B.
Access

 (1)  
Location Zone
 101 Control Cabin - Left
 216 Left Main Wheel Well
 217 Right Main Wheel Well


 C.
Remove the Pressure Switch


 S 842-042
 (1)  
Release the parking brake.

 S 842-043

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


 S 032-044

 (3)  
Disconnect the electrical plug from the pressure switch.

 (a)  
Seal the plug and the receptacle with plugs.


 S 022-045
 (4)  
Remove the pressure switch and discard the O-ring and the backup rings.

 (a)  
Seal the port with a cap.


 TASK 32-43-46-402-046
 10. Pressure Switch Installation
____________________________
 NOTE: This applies to the pressure switch of the solenoid shutoff valve and
____
 the pressure switch of the servo valve.

 A. Consumable Materials
 (1)  
D00400 Fluid - Hydraulic, BMS 3-11

 B.
References

 (1)  
24-22-00/201, Manual Control

 (2)  
29-15-00/201, Hydraulic Systems

 (3)  
32-43-01/501, Automatic Braking System

 C.
Access

 (1)  
Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right
 216 Left Main Wheel Well
 217 Right Main Wheel Well

 

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 32-43-46
 ALL  ú ú 01 Page 209 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 D. Procedure
 S 422-047
 (1)
Install the new O-ring and the backup rings on the pressure switch.

 (a)  
Lubricate the O-ring and backup rings with BMS 3-11 during installation.


 S 422-048
 (2)  
Install the pressure switch in the module.

 (a)  
Tighten the switch to a torque of 90 to 110 pound-inches.


 S 722-049
 (3)  
Do a test on the pressure switch.

 (a)  
Do a check on the switch connector receptacle between pins 2 and 3 for continuity.

 (b)  
Install the electrical plug and the lockwire.

 (c)  
Do a test on the control module (Ref 32-43-01/501).


 S 842-050
 (4)  
Pressurize hydraulic system B (AMM 29-15-00/201).

 S 842-051

 (5)  
Set the parking brake.

 (6)
Remove the pressure from hydraulic system B (AMM 29-15-00/201).

 (7)  
Close the AUTOBRAKE CONTR circuit breaker on the P6-3 panel.

 (8)
Remove the electrical power if it is not needed (AMM 24-22-00/201).
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 3(87)