500  Body Sections 
May 15/67  Figure 202  12-31-0 
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ZONE DIAGRAMS – MAINTENANCE PLANNING
General
A.  This section is provided for reference purposes only. The information is derived from, and virtually identical to, the ZONE DIAGRAM section in the Maintenance Planning Document, D6-17594-1.
B.  The 737 Zone Diagram is comprised of seven major zones covering the fuselage, wings, nacelles and empennage. Further identification breakdown is achieved by use of areas in conjunction with major zones which denote specific compartments, equipment bays, doors, engines, etc.
2.  Zone and Area Identification
A.  The zone and area is identified by a number consisting of a first digit indicating the zone followed by a dash and a number of one or two digits which indicate area.
B.  Thus 1-2 is read: zone 1, area 2 which identifies the upper half of the fuselage and the right side of the control cabin.
3.  Zone Location (Fig. 201) General Zone Diagram – (Covers entire aircraft) Zone 1 – Upper Half of the Fuselage Zone 2 – Lower Half of the Fuselage Zone 3 – Left Wing Zone 4 – Right Wing Zone 5 – Left Nacelle Zone 6 – Right Nacelle Zone 7 – Empennage
533 
Aug 15/73  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  12-31-1 Page 201 

General Zone Diagram  533 
12-31-1  Figure 201 (Sheet 1)  May 01/75 
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533  General Zone Diagram 
May 01/75  Figure 201 (Sheet 2)  12-31-1 
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General Zone Diagram  533 
12-31-1  Figure 201 (Sheet 3)  May 01/75 
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533  General Zone Diagram 
May 01/75  Figure 201 (Sheet 4)  12-31-1 
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General Zone Diagram  533 
12-31-1  Figure 201 (Sheet 5)  Aug 15/73 
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533  General Zone Diagram 
May 01/75  Figure 201 (Sheet 6)  12-31-1 
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500  Body Section 41 Access Doors and Panels 
Feb 20/91  Figure 201 (Sheet 1)  12-31-11 
Page 201 
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General Zone Diagram  500 
12-31-11  Figure 201 (Sheet 5)  Aug 15/68 
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PANEL NO.  TITLE  BONDING RESISTANCE 
MAX OHMS 
1101  EXTERNAL POWER RECEPTACLE DOOR  0.1 
1103  FORWARD ACCESS DOOR  0.1 
1104  FORWARD TOILET DOOR  0.1 
1201*  ELECTRONICS EQUIPMENT ACCESS DOOR  0.1 
1601*  FORWARD AIRSTAIR DOOR  0.1 
3101*  NOSE WHEEL WELL DOOR  2M 
3102*  NOSE WHEEL WELL DOOR  2M 
3103  NOSE WHEEL WELL PANEL 
3104  NOSE WHEEL WELL PANEL 
3105  NOSE WHEEL WELL PANEL 
3106  NOSE WHEEL WELL PANEL 
4201*  FORWARD ENTRY DOOR  0.1 
4701*  FORWARD GALLEY DOOR  0.1 

*  THIS NUMBER IS NOT MARKED ON AIRPLANE AND IS GIVEN FOR SERVICE INFORMATION ONLY
NOTE:  Bonding resistance values are maximum values which allow for the possibility of oxidation at the bonding interface. Lower values can be obtained after bonding joint has been cleaned.
500  Body Section 41 Access Doors and Panels 
Jan 20/82  Figure 201 (Sheet 3)  12-31-11 
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BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

BODY SECTION 43 ACCESS DOORS AND PANELS
REF DRAWING 65-45211 FOR ACCESS DOORS AND PANELS

508  Body Section 43 Access Doors and Panels 
Feb 20/91  Figure 201 (Sheet 1)  12-31-21 
　
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