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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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 TASK 21-21-12-004-002
 2.  Duct and Check Valve Assembly Removal (Fig. 401)_____________________________________
 A.  Access
 (1)  Location Zone
 210 Air Conditioning Distribution Bay

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

 S 034-003

 (2)  
Remove the band clamps and disconnect the flexible duct from the duct and check valve assembly.

 S 034-004

 (3)  
Disconnect the condensate drain from the duct and check valve assembly.

 S 034-005

 (4)  
Remove the bolts, washers and seals from the lower flange of the duct and check valve assembly.

 (5)  
Discard the seals.

 (6)  
Remove the duct and check valve assembly.


 S 034-006
 S 024-007
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-21-12
 ALL  ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SEE A CABIN OVERHEAD DISTRIBUTION DUCT TO PASSENGERTO CONTROL CABIN
FROM FORWARD TO PASSENGER CABIN CARGO COMPARTMENT AIR COLLECTOR
ACCESS TO 
RECIRCULATION FAN 
AIR FILTERS (2) 
CONTROL CABIN 
RECIRCULATION FAN  TEMPERATTURE 
PASSENGER CABIN  SENSORS 
CHECK VALVE RECIRCULATION FAN  HOT AIR (LEFT PACK TYP) 
COLD AIR 
GROUND SERVICE  (LEFT PACK TYP) 
CONNECTION  CHECK VALVE 
SEE  B  (LEFT PACK TYP) 
FWD  CONTROL CABIN HOT AIR BLEED TO  (LEFT SIDE ONLY) MIX MUFF 

A

Duct and Check Valve Assembly
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-21-12
 ALL  ú ú 01 Page 402 ú Feb 20/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
FLEXIBLE DUCT
CONDENSATE DRAIN
RUBBER STOP
ADJUSTMENT SCREWS
PRESSURE
SKIN
GASKET GAP
SWING
CHECK VALVE

CONNECT HOLE
A 737-300/400/500MAINTENANCE MANUAL 
BAND CLAMPS 
DUCT AND CHECK VALVE ASSEMBLY 
SEE  C  FAIRING DRAIN HOLE  BOLT WASHER SEAL SPRING LOWER FLANGE FWD

GROUND SERVICE CONNECTION ACCESS DOOR  FAIRING 
LATCH 
FWD  C
Duct and Check Valve Assembly Figure 401 (Sheet 2) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 21-21-12
 ALL  ú ú 03 Page 403 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 21-21-12-404-008
 3.  Duct and Check Valve Assembly Installation (Fig. 401)__________________________________________
 A. Consumable Materials
 (1)  
A00027 Adhesive - RTV 174 or RTV 102

 (2)  
C00048 Primer - RTV 1200, Dow Corning

 (3)  
B00148 Solvent - Methyl Ethyl Ketone (MEK), TT-M-261


 B. References
 (1)  AMM 21-00-00/201, Air Conditioning
 C. Access
 (1)  Location Zone
 210 Air Conditioning Distribution Bay

 D. Prepare for the Installation
 S 034-009
 (1)  Remove the gasket and the adhesive with a putty knife or an equivalent tool.
 S 114-017
 WARNING:_______DO NOT GET SOLVENT IN YOUR MOUTH OR EYES, OR ON YOUR SKIN. DO NOT BREATHE THE FUMES FROM THE SOLVENT. PUT ON PROTECTIVE SPLASH GOGGLES AND GLOVES WHEN YOU USE THE SOLVENT. KEEP THE SOLVENT AWAY FROM SPARKS, FLAME, AND HEAT. SOLVENTS ARE POISONOUS AND FLAMMABLE AND CAN CAUSE INJURY OR DAMAGE.
 (2)  Clean the mating surfaces with the solvent, Series 90 (AMM 20-30-90/201).
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 空调 AIR CONDITIONING 1(29)