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(a)  If the class divider was moved to a new location, do these steps to attach the support clevis [11] to the top of the stowage bin.
1)  Put each support clevis [11] in its position on the studs on the top of the stowage bins.
2)  Install the nuts [12] that attach the support clevis [11] to the studs on the stowage bins.
(b)  
Put the header assembly [1] in its position.

(c)  
Install the washers [9] as necessary to center the header assembly [1] between the fittingson the support clevis [11].

(d)  
Install the bolt [8] and nut [10] to attach the header assembly [1] to the support clevis [11].

NOTE: Put the washers [9] that are not used to align the header assembly [1] under the nut [10].

(e)  
Connect the electrical connectors, if applicable.

(f)
Do these steps to install the curtain [3] in the header assembly [1]: CAUTION: BE CAREFUL WITH THE CURTAINS. THE CURTAINS CAN BECOME DAMAGED AND DIRTY EASILY. 1) Move the sliders [4] into the curtain track to install the curtains [3] in the header assembly [1]. 2) Install the screw [5], washer [6], and nutplate [7] in the end of the header

assembly [1].
3) Close the tiebacks around the curtains [3].

D.  Put the Airplane Back to Its Usual Condition
SUBTASK 25-24-11-410-001
(1) Install the ceiling panel(s) you removed for this task. To install the ceiling panel, do this task: Ceiling Panel - Installation, TASK 25-21-45-400-801.
------------------------- END OF TASK ---------------------------
EFFECTIVITY: 003‐004, 008‐011  25-24-11 PAGE 403 
AUG 25/11 
AAR PROPRIETARY - Do not copy without express permission of AAR 

B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-11 PAGE 404 
AUG 25/11 
AAR PROPRIETARY - Do not copy without express permission of AAR 

PARTITIONS -REMOVAL/INSTALLATION
1. General
A.  In this procedure, class dividers may be referred to as partitions.
B.  This procedure has these tasks:
(1) 
 Partition Removal,

(2)
Top Attachment Removal,

(3) 
 Bottom Attachment Removal,

(4) 
 Partition Installation,

(5)
 Bottom Attachment Installation,

(6)
Top Attachment Installation,

TASK 25-24-16-840-801
2. Partition Removal
(Figure 401)
A.  General
B.  Location Zones
Zone Area

200  Upper Half of Fuselage
C.  Procedure
SUBTASK 25-24-16-020-018
(1)  Do this task: Top Attachment Removal, TASK 25-24-16-000-805.
SUBTASK 25-24-16-020-019
(2)  Do this task: Bottom Attachment Removal, TASK 25-24-16-000-806.
SUBTASK 25-24-16-020-020
　
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