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时间:2011-04-01 08:32来源:蓝天飞行翻译 作者:航空
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SEE B 
CONTROL CABIN 
RECIRCULATION FAN  TEMPERATURE 
PASSENGER CABIN  SENSORS 
RECIRCULATION FAN  HOT AIR 
CHECK VALVE  (LEFT PACK EXAMPLE) 
MIXING CHAMBER  COLD AIR 
(LEFT PACK EXAMPLE) 
GROUND SERVICE 
CONNECTION  CHECK VALVE 
(LEFT PACK EXAMPLE) 
SEE  C  FWD HOT AIR BLEED TO CONTROL CABIN  (LEFT SIDE ONLY) MIX MUFF 

A

Main Distribution Manifold
Figure 1 (Sheet 1)

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 21-21-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

Main Distribution Manifold
Figure 1 (Sheet 2)

G94038
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CONDENSATE DRAIN FROM PLENUM  BAND CLAMPS 
DUCT AND CHECK VALVE ASSEMBLY 
PRESSURE SKIN 
SWING CHECK VALVE CONNECT HOLE  SEE  D  DRAIN HOLE  FWD 

GROUND SERVICE CONNECTION ACCESS DOOR  FAIRING 
FWD  LATCH 

Main Distribution Manifold Figure 1 (Sheet 3)

 G94094
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 D.  Each filter assembly is outboard of the recirculation fan(s), and contains either a high efficiency one-piece filter, or a two-piece filter (a prefilter and a particulate HEPA filter).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 CHECK VALVE (COLD AIR) - REMOVAL/INSTALLATION
_____________________________________________
 1.  General_______
 A.  Two tasks are supplied in this procedure. The first task is the removal of the check valve in the outlet duct from the air conditioning pack. The second task is the installation of the check valve.
 B.  The two check valves are installed in the distribution bay just upstream of the mix muff.
 TASK 21-21-04-004-002
 2.  Remove the Check Valve (Cold Air) (Fig. 401)_________________________________
 A.  References
 (1)  
12-31-01/201, Zone Diagrams

 (2)  
24-22-00/201, Manual Control

 (3)  
36-05-00/201, Pneumatic System


 B.  Access
 (1)  Location Zone (AMM 12-31-01/201)
 210 Air-Conditioning Distribution Bay

 C.  Prepare for the Removal of the Check Valve
 S 864-003
 (1) Supply electrical power to the airplane (AMM 24-22-00/201).
 S 864-004
 WARNING:_______REMOVE THE PRESSURE FROM THE PNEUMATIC SYSTEM. PRESSURE IN THE PNEUMATIC SYSTEM CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  
Remove the pressure from the pneumatic system (AMM 36-05-00/201).

 S 864-005

 (3)  
Set these switches on the air conditioning module (P5-10 panel) to the OFF position:

 (a)  
L PACK

 (b)  
R PACK

 


 D.  Procedure
 S 014-001
 (1)  
Remove the center panel on the aft bulkhead in the forward cargo compartment to get access to the check valve.
 
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