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A 737-300/400/500MAINTENANCE MANUAL
(5.23 M)
Principal Dimensions
Figure 201
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A
737-300/400/500MAINTENANCE MANUAL
(6)
Fuselage
-
Height of the body reference plane (top of the floor beam WL 208.10) above the ground at the main gear -- 102.10 inches
(2.59 m)
-
Height (constant cross section) Above the body reference plane -- 98.4 inches (2.5 m) Below the body reference plane -- 59.60 inches (1.51 m)
-
Height to the centerline of the windows above the body reference plane -- 38 inches (0.97 m)
-Length -- 1267 inches (32.18 m) (737-300)
(7)
Areas
(a)
Wing (basic) -- 980.0 square feet (910.37 square meters)
(b)
Horizontal Stabilizer Surfaces (total, with the area in the fuselage) -- 338 square feet (313.98 square meters)
(c)
Vertical Stabilizer Surfaces (total) -- 224.35 square feet
(208.41 square meters)
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A
737-300/400/500MAINTENANCE MANUAL
BODY STATION DIAGRAM - MAINTENANCE PRACTICES
____________________________________________
1. General
A. The body station diagram gives the location of the major structural openings in the fuselage (Fig. 201).
B. For detail data and location of structural components related with these openings, refer to the Structural Repair Manual.
TASK 06-25-00-202-003
2. Body Station Diagram (Fig. 201)____________________
A. Procedure
S 222-002
(1) See Fig. 201 for the body station diagram.
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WL 148.5
PRESSURELEVEL
SECTION
WL 306.5
WL 246.1 WINDOWSUPPER RADII
737-300(LEFT SIDE VIEW)
Body Station DiagramFigure 201
A 737-300/400/500MAINTENANCE MANUAL
A
737-300/400/500MAINTENANCE MANUAL
VERTICAL STABILIZER AND RUDDER STATION DIAGRAM - MAINTENANCE PRACTICES
______________________________________________________________________
1. General_______
A. The vertical stabilizer and rudder station diagram gives the location of the structural components on the vertical stabilizer and rudder.
TASK 06-32-00-202-003
2. Vertical Stabilizer and Rudder Station Diagram (Fig. 201)______________________________________________
A. Procedure
S 222-002
(1) See Fig. 201 for the vertical stabilizer and rudder station diagram.
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