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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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 S 424-012
 CAUTION:_______BE CAREFUL WITH THE PANELS. YOU CAN DAMAGE THE PANELS IF YOU HIT THEM OR GET THEM DIRTY.
 (1)  Align the panel and engage each hinge.
 (a)  
Push the lever.

 (b)  
Move the hinge half on the panel to engage with the hinge half on the stowage bin. 1) Move the panel to the outboard position.

 (c)  
Release the lever.


 S 424-008
 (2)  
Connect the lanyard.

 S 424-009

 (3)  
Lift and move the panel inboard until the edge engages with the air outlet extrusion.


 NOTE: The hinges are locked in the inboard position.
____
 S 824-010
 (4)  Use the adjusting screw to align the adjacent panels if it is necessary.
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 25-21-45
 ALL  ú ú 02 Page 403 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 SIDEWALL PANELS - REMOVAL/INSTALLATION
______________________________________
 1.  General_______
 A. This procedure contains two tasks:
 (1)  
The removal of the Sidewall Panels

 (2)  
The installation of the Sidewall Panels


 TASK 25-21-46-004-001
 2.  Sidewall Panel Removal (Fig. 401)______________________
 A. References
 (1)  24-22-00/201, Manual Control
 B. Access
 (1)  Location Zone
 100 Upper Half of Fuselage

 C. Prepare for the Removal
 S 864-004
 (1)  
Remove the electrical power (Ref 24-22-00/201).

 S 014-002

 (2)
Remove the passenger seats if it is necessary for access.


 D. Procedure
 S 014-026
 CAUTION:_______BE CAREFUL WITH THE PANELS. YOU CAN CAUSE DAMAGE TO THE SURFACES OF THE PANEL IF YOU HIT THEM OR GET THEM DIRTY.
 (1)  Remove the trim strips
 (a)  
Remove the trim strip down on each side of the panel until it is clear from the panel.

 (b)  
Remove the carpet risers from below the panel.


 S 024-006
 (2)  
Hold the sidewall panel and remove the screws at the shockmounts.

 S 024-007

 (3)  
Move the panel down until the top edge of the panel disengages from the air outlet extrusion.

 (4)  
Remove the electrical connector from the sidewall light.

 (5)  
Remove the panel.


 S 034-008
 S 024-010
 TASK 25-21-46-404-011
 3.  Sidewall Panel Installation (Fig. 401)___________________________
 A. References
 (1)  24-22-00/201, Manual Control
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 25-21-46
 ALL  ú ú 02 Page 401 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ELECTRICAL
CONNECTOR

WASHER SCREW
SIDEWALL
SEE PANEL

A-A

Sidewall Panel Installation
Figure 401

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 25-21-46
 ALL  ú ú 02 Page 402 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 B. Access
 (1)  Location Zones
 100 Upper Half Fuselage

 C. Procedure
 S 424-027
 CAUTION:_______BE CAREFUL WITH THE PANELS. YOU CAN CAUSE DAMAGE TO THE SURFACES OF THE PANEL IF YOU HIT THEM OR GET THEM DIRTY.
 (1)  
Install the panel.

 S 434-013

 (2)  
Connect the electrical connector.

 S 424-015

 (3)  
Put the top edge of the panel into the air outlet extrusion.


 
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