SUBTASK 25-24-16-420-028
(3) Make sure that the partition is vertical and, if applicable, that it is perpendicular to the seat tracks.
------------------------- END OF TASK ---------------------------
TASK 25-24-16-400-805

7.  Top Attachment Installation
(Figure 401, Figure 402, Figure 404)
A.  General
(1)  This task includes the steps to install the top attachment(s).
B.  Location Zones
EFFECTIVITY:

25-24-16
003‐004, 008‐011
PAGE 405 AUG 25/11
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Zone Area
200 
Upper Half of Fuselage
C. Procedure
SUBTASK 25-24-16-420-031
(1) Do these steps to connect the inboard top support attachment (Figure 404):
(a) Lift the fitting assembly [40] and engage the latches in the stowage bin/PSU extrusion.
------------------------- END OF TASK ---------------------------
EFFECTIVITY: 003‐004, 008‐011  25-24-16 PAGE 406 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-16 PAGE 407 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-16 PAGE 408 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-16 PAGE 409 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-16 PAGE 4010 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 003‐004, 008‐011  25-24-11 PAGE 405 
AUG 25/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

Passenger Seat Installation
Figure 401 (Sheet 2 of 3)/25-22-01-990-801

EFFECTIVITY: 003‐004  25-22-01 PAGE 406 JUNE 10/11 
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B737‐700

SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL

EFFECTIVITY: 008‐011  25-22-01 PAGE 407 JUNE 10/11 
AAR PROPRIETARY - Do not copy without express permission of AAR