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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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_____________________________________________ DESCRIPTION AND OPERATION
_________________________
 1.  General_______
 A.  Partitions are provided at doorways, and to form closets and passenger compartments as required (Fig. 1). Where possible, the floor tracks and overhead support structure are used for attachment. This permits adjustment in increments of 1-inch formward or aft for movable partitions. Aft centerline closet is formed between two lavatories and is removed with Lavatories (Ref 25-41-15).
 B.  Outer edges of partitions and compartments are shaped to the sides of the fuselage and inner edges are vertical at the aisle.
 C.  Partition and compartment panels are made up of a fire-resistant nomex honeycomb core with tedlar decorative surfaces.
 D.  Overhead stowage compartments are found throughout the airplane (Fig. 1).
 2.  Windscreens (Fig. 1)___________
 A.  Windscreens are installed in the cabin, just aft of the forward entry or service doors and forward of the aft left entry door as applicable, to provide protection from weather.
 B.  A stowage closet is at the aft end of the cabin between the aft lavatory and galley. The closet has a hinged door.
OVERHEAD STOWAGE BINS
GALLEY NO. 4
(RIGHT SIDE IS SHOWN,  GALLEY NO. 3 (REF)
LEFT SIDE IS OPPOSITE)  (REF) AFT CENTERLINE STOWAGE CLOSET
(REF)
(REF)  FORWARD LEFT WINDSCREEN/STOWAGE

Partition and Compartment Locations
Figure 1

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 25-24-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 3.  Overhead Stowage Bins (Fig. 1)
_____________________
 A.  Overhead stowage for coats and carry-on items, is provided by bins located over the passenger seats along each side of the cabin. The stowage bins are in lengths of 19, 20, 27, 40, 50 or 60 inches.
 B.  Each compartment has an upward opening door, supported in the open position by a hinge linkage actuated by a small spring-loaded dampened actuator.
 4.  Class Divider Partition (Fig. 1)
_______________________
 A.  Class dividers separate different seating class arrangements of the airplane.
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 25-24-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 WINDSCREEN - REMOVAL/INSTALLATION
_________________________________
 1.  General_______
 A. This procedure contains these tasks:
 (1)  
The removal of the windscreen

 (2)  
The installation of the windscreen.


 TASK 25-24-15-004-001
 2.  Windscreen - Removal (Fig. 401)____________________
 A. References
 (1)  AMM 24-22-00/201, Manual Control
 B. Access
 (1)  Location Zone
 107 Fwd Half of Cabin
 108 Aft Half of Cabin

 C. Procedure
 S 864-002
 (1)  
Remove the electrical power (AMM 24-22-00/201).

 S 034-022

 (2)  
Disconnect the wire bundle at the outboard edge of the windscreen.

 S 014-024

 (3)  
Open the lower doors in the windscreen cabinet to get access to the floor track attachment.

 S 014-025

 (4)
Remove the nuts from the cabinet on the floor track attachment.

 (5)
Lift the cabinet and the windscreen from the floor track studs.

 (6)  
Remove the loose fittings from the floor tracks.


 S 024-026
 S 024-028
 TASK 25-24-15-404-049
 3.  Windscreen - Installation (Fig. 401)_________________________
 A. References
 (1)  AMM 24-22-00/201, Manual Control
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