(b)  
The pitot line disconnected from drain fitting No. 1.

 S 842-037
 (4)  Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the hose that you disconnected from the top left pitot-static probe.

 (b)  
Replace the cap on the hose.

 S 432-046
 (5)  Connect the air supply:
 (a)  
Remove the cap from the pitot hose that you disconnected from the top right pitot-static probe.

 (b)  
Connnect the dry filtered air supply.

 S 862-047
 (6)  Flush the first officer's pitot system at these locations:
 (a)  
The pitot hose disconnected from air data computer No. 2.

 (b)  
The pitot line disconnected from drain fitting No. 10 which is at the right side of the E1 rack.

 S 032-048
 (7)  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.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-11-01

 ú ú 09 Page 202 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 432-065
 (8)  Connect the air supply:
 (a)  
Remove the cap from the pitot hose that you disconnected from the bottom left pitot-static probe.

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

 S 862-066
 (9)  Flush the auxiliary No. 2 pitot system at these locations:
 (a)  
The pitot hose disconnected from the combined standby
 altimeter/airspeed indicator.

 (b)  
The pitot line disconnected from drain fitting No. 7 which is at the forward end of the nose wheel well.

 S 032-067
 (10) Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the hose that you disconnected from the bottom left pitot-static probe.

 (b)  
Replace the cap on the hose.

 S 862-076
 (11) Flush the captain's static system at these locations:
 (a)  
The static hose disconnected from air data computer No. 1.

 (b)  
The static line disconnected from drain fitting No. 2 which is at the left side of the E1 rack.

 (c)  
The static line disconnected from drain fitting No. 11 which is at the forward end of the nose wheel well.

 (d)  
The static line disconnected from the bottom right pitot-static probe.

 S 032-077
 (12) Disconnect the air supply:
 (a)  
Disconnect the dry filtered air supply from the hose that you disconnected from the top left pitot-static probe.

 (b)  
Replace the cap on the hose.

 S 432-078
 (13) Connect the air supply:
 (a)  
AIRPLANES WITH SOURCE SELECT VALVES; Remove the cap from the hose that you disconnected from the first officier's static source selector valve.

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

 S 862-086
 (14) Flush the first officer's static system at these locations:
 (a)  
The static hose disconnected from air data computer No. 2.

 (b)  
The static line disconnected from drain fitting No. 9 which is at the right side of the E1 rack.

 (c)  
The static line disconnected from drain fitting No. 6 which is at the forward end of the nose wheel well.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-11-01
 ú ú 08 Page 203 ú Mar 15/99

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  The static hose disconnected from the bottom left pitot static probe.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 導航 NAVIGATION 1(37)