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时间:2011-04-01 19:06来源:蓝天飞行翻译 作者:航空
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 A. Access
 (1)  Location Zone
 100 Upper Half of Fuselage

 B. Procedure
 S 422-038
 (1)
Slide the shade's pivot end into the window shade bracket.

 S 432-039

 (2)  
With the shade at the bottom of the hatch panel opening, wind the shade up using the flat end of the shade.


 NOTE: This provides the tension to roll the shade to the down
____
 position.

 S 432-040
 (3)  
Push down of the catch to hold the flat end of the shade in place.

 S 432-041

 (4)  
Make sure the shade operates properly in the hatch panel before installing the hatch panel to the hatch.

 S 432-042

 (5)  
Install the hatch panel to the hatch using the eight screws (AMM 52-21-00/401).


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 25-21-12
 ALL  ú ú 01 Page 213 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 422-043
 (6) Install the hatch in the airplane (AMM 52-21-00/401).
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 25-21-12
 ALL  ú ú 01 Page 214 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 SIDEWALL LINING PANELS (AFT ENTRY AND AFT SERVICE DOORWAYS) -
________________________________________________________________ REMOVAL/INSTALLATION
____________________
 1.  General_______
 A.  This procedure contains two tasks:
 (1)  
The removal of the Sidewall Lining Panels

 (2)  
The installation of the Sidewall Lining Panels


 B.  These procedures apply to the sidewall lining attached to the structure around the aft entry and aft service door openings.
 TASK 25-21-25-004-001
 2.  Sidewall Lining Panels Removal (Aft Entry and Service Doorways)(Fig. 401)______________________________
 A.  Access
 (1)  Location Zone
 108 Aft Half of Cabin

 B.  Remove the Sidewall Lining Panels
 S 014-002
 (1)  
Remove the passenger equipment if it is necessary to get access to the sidewall lining.

 S 014-003

 (2)  
Remove the rubber seal installed around the door opening.

 S 014-004

 (3)  
Remove the seal retainer if it is applicable.

 S 024-005

 (4)  
Remove the lining that is aft of the door.


 (a)  Move the lining forward and remove it.
 S 024-006
 (5) Remove the lining around the top part of the door opening.
 (a)  Move the lining down and inboard, and remove the lining.
 S 014-007
 (6)  
Remove the aid handle that is forward of the entry door if installed.

 S 014-008

 (7)  
Remove the quarter-turn fasteners that attach the clearance cover to the forward structure of the door.

 S 024-009

 (8)  
Remove the lining that is forward of the door.


 (a) Move the lining aft and inboard and remove it.
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 25-21-25
 ALL  ú ú 01 Page 401 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

B-B


LINING

AFT ENTRY DOORWAY SHOWN AFT SERVICE DOORWAY OPPOSITE
Sidewall Lining Panels Installation (Aft Entry and Service Doorways)
Figure 401

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