500 Body Sections
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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
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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
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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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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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