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E.  Passenger cabin partitions are provided in the airplane to separate different classes of accommodation and to form compartments and closets as required (Ref 25-24-0).
F.  Attendants' stations are provided near the forward and rear entry doors. Each station accommodates two persons, and includes a double seat, service unit, boarding light, and panel (Ref 25-25-0).
G.  The passenger cabin floor is covered with carpeting except in the galley and entry door areas where it is covered with a vinyl mat (Ref 25-27-0).
H.  Wide-Body, Carry-All, or ATI Interior Compartments are installed above the passenger seats along both sides of the passenger cabin (Ref 25-24-311, 25-24-511, or 25-24-313, ATI Compartments).
I.  In the Cargo/Passenger airplanes, NIP Bins are installed above the passenger seats along both sides of the passenger cabin (Ref 25-24-311, Overhead Stowage Compartments).
J.  Miscellaneous items of passenger equipment are installed at various locations in the passenger cabin (Ref 25-29-0).
K.  The airplane is equipped with galley units providing facilities for storage and preparation of food (Ref 25-31-0).
L.  The passenger cabin is equipped with lavatories which are similar but slightly different in arrangement (Ref 25-40-0).
5C8 
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Passenger Compartment Arrangement  5C8 
25-20-0  Figure 1 (Sheet 1)  Jun 20/85 
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5C8  Passenger Compartment Arrangement 
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Passenger Compartment Arrangement  5C8 
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PASSENGER CABIN ARRANGEMENT LIMITATIONS - DESCRIPTION AND OPERATION
1.  General
A.  Passenger cabin conversion may be affected by the addition or removal of seats, passenger service units, partitions and auxiliary equipment necessary for passenger accommodation. The conversion limits result from seat spacing limitations and entrance, exit, and aisle restrictions set forth in the directives of applicable regulatory agencies and Boeing document D6-10881.
B.  The applicable regulations must be reviewed when revising passenger cabin arrangements to ensure compliance in the following areas:
(1)  
Access from the main aisle to the entry and galley doors.

(2)  
Main aisle width.

(3)  
Access from the main aisle to the overwing exits.

(4)  
Seat arrangement adjacent to overwing exits.

(5) 
 Seat-to-bulkhead clearances.

551 
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PASSENGER CABIN LINING AND INSULATION - DESCRIPTION AND OPERATION
EFFECTIVITY
Wide-Body Look and Carry-All Compartment Interior
1. General
A.  The passenger cabin lining and insulation is designed to reduce the noise level, stabilize cabin temperature, and provide a decorative finish. The cabin lining and insulation consists of the sidewall lining, the curved ceiling and lowered ceiling panels, and the insulation installed to body structure throughout the passenger cabin. Information on the lining and insulation of all doors is included in the appropriate sections of Chapter 52, Doors.
2.  Sidewall Lining
A.  The sidewall lining components include the window panels, carpet riser panels, air return grilles, and doorway lining panels (Fig. 1).
(1)  
A window panel consists of a formed aluminum panel with a stain resistant decorative covering. A roll-type window shade, plastic inner windowpane and the window reveal are attached to the outboard side of the window panel. A light for illumination of the sidewall is mounted in the window panel near the top. The window panels are secured at the top by the sidewall extrusion and by the carpet riser panel along the bottom edge. At each side the window panel is attached with vibration absorbing fasteners to the body structure. These fasteners are hidden by a trim strip which slides into the gap between window panels.

(2)  
A window shade is made of a flexible decorative material with one end attached to a spring-loaded roller and the other end attached to a stiffener. The roller is installed in brackets mounted on the outboard side of the window panel assembly (Fig. 2). A spring-loaded shoe in either end of the stiffener rides in a groove in the window trim and a plastic handle is attached to the stiffener.
　
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