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时间:2011-04-02 23:24来源:蓝天飞行翻译 作者:航空
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 S 172-027
 (24) Flush the first officer's static system at these locations:
 (a)  
The static line that you disconnected from drain fitting No. 6 located on the forward end of the nose wheel well.

 (b)  
The static hose that you disconnected from the lower left pitot static probe.


 S 082-071
 (25) Disconnect the air supply:
 (a)
Disconnect the dry filtered from the static hose that you disconnected from the top right pitot-static probe.

 (b)  
Replace the cap on the hose.


 S 482-049
 (26) Connect the air supply:
 (a)  
Locate the port on the manifold in the electronics compartment on the forward right side.

 (b)  
Connect the dry filtered air supply to the manifold.


 S 172-046
 (27) Flush the auxiliary No. 1 static system at these locations:
 (a)  
The static hose disconnected from the cabin altimeter and differential pressure indicator in the P5 panel.

 (b)  
The static hose disconnected from the electronic pressure controller.

 (c)  
The static hose disconnected from the flap load limiter airspeed switch No. 1 (S560).


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 ú ú 06 Page 206 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (d)  
The static line disconnected from drain fitting No. 4.

 (e)  
The static line disconnected from drain fitting No. 12.

 (f)  
The static line disconnected from the lower right pitot static probe.


 S 082-050
 (28) Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the manifold which is in the electronics compartment on the forward right side.

 (b)  
Replace the cap on the manifold.


 S 482-051
 (29) Connect the air supply:
 (a)  
Remove the cap from the auxiliary No. 1 static system hose at the top left pitot-static probe.

 (b)  
Connect the dry filtered air supply to the hose.


 S 172-047
 (30) Flush the auxiliary No. 1 static system at these locations:
 (a)  
The static line disconnected from the lower right pitot-static probe.

 (b)  
The static line disconnected from drain fitting No. 12.


 S 082-052
 (31) Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the auxiliary No. 1 static system hose that you disconnected from the top left pitot-static probe.

 (b)  
Replace the cap on the hose.


 S 482-048
 (32) Connect the air supply:
 (a)  
Remove the cap from the auxiliary No. 2 static system hose that you disconnected from the top right pitot-static probe.

 (b)  
Connect the dry filtered air supply to the hose.


 S 172-053
 (33) Flush the auxiliary No. 2 static system at these locations:
 (a)  
The static hose disconnected from the flap load limiter airspeed switch No. 2 (S562)

 (b)  
The static hose disconnected from the bottom left
 pitot-static probe.


 (c)  
The static line disconnected from drain fitting No. 8.


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 34-11-00
 ú ú 07 Page 207 ú Nov 15/95

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 082-063
 (34) Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the hose that you disconnected from the top right pitot-static probe.

 (b)  
Replace the cap on the hose.


 S 482-064
 (35) Connect the air supply:
 (a)  
Remove the cap from the alternate static system line that you disconnected from the captain's static source selector valve.
 
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