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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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 (1)  The actuator chassis and the hinge quadrants must be removed from the door before you install the actuators.
 B. Access
 (1)  Location Zones
 100 Upper Half of Fuselage

 C. Procedure
 S 422-008
 (1)  Attach the actuators to the hinge quadrants and chassis with pins.
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 25-24-36
 ALL  ú ú 01 Page 201 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
STRIKER 
DOOR 
HINGE 
QUADRANT 


LATCH COVER 
SEE  B  CHASSIS ACTUATOR  ACTUATOR  ATTACHMENT 
FASTENER 
(3 LOCATIONS) 
BULLNOSE 
HORIZONTAL  LATCH 
TRIM STRIP  ASSEMBLY 
SEE  A  C 
LATCH PAWL 
STRIKER 
BULLNOSE 
SUPPORT 
TORQUE 
TUBE  DOOR 
HORIZONTAL 
TRIM STRIP 
LATCH COVER 
BRACKET 

Overhead Stowage Bin Door Installation 
Figure 201 (Sheet 1) 

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 ALL  ú ú 01 Page 202 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
STOWAGE BIN


Overhead Stowage Bin Door Installation
Figure 201 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 422-009
 (2)  
Install the actuator chassis assemblies on the stowage bin sidewall and tighten the bolts.

 S 422-067

 (3)  
Connect the door to the hinge quadrants with screws and tighten the screws.

 S 822-011

 (4)  
Close the door and make sure the strikers are aligned with the center of the latch covers.


 (a)  Align the door on the hinge quadrants if it is necessary.
 S 822-012
 (5)  With the door closed, push on the center of the door.
 (a)  Make sure the door latched and the striker locked with the latch pawl.
 S 422-068
 (6)  Carefully open the door and tighten the bolts that attach the actuator chassis to the stowage bin sidewall.
 TASK 25-24-36-002-014
 4.  Hinge Quadrant Removal (Fig. 201).______________________
 A. Access
 (1)  Location Zones
 100 Upper Half of Fuselage

 B. Procedure
 S 012-015
 (1)  
Open the overhead bin door.

 (2)  
Disconnect the actuator from the hinge quadrant.

 (3)  
Hold the door and remove the bolt at the hinge point.

 (4)
Remove the screws that attach the hinge quadrant to the door.

 (5)  
Remove the hinge quadrant.


 S 022-080
 S 022-081
 S 022-018
 S 022-019
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 25-24-36
 ALL  ú ú 01 Page 204 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 25-24-36-402-020
 5.  Hinge Quadrant Installation (Fig. 201)___________________________
 A. Access
 (1)  Location Zones
 100 Upper Half of Fuselage

 B. Procedure
 S 422-058
 
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