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 (d) Horizontal Stabilizer
 ELEV STA  Elevator Station. A plane that is perpendicular to the elevator hinge centerline. It is measured from the intersection of the elevator hinge centerline and stabilizer buttock line 0.00.
 FS STA  Front Spar Station. A plane that is perpendicular to the horizontal stabilizer front spar. It is measured from the Front Spar Station 0.00, the intersection of the front spar and trace of body buttock line 0.00 at the horizontal stabilizer reference plane.
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 HSBL

SCP
LE STA
RS STA
STAB STA
(e) Nacelle NAC BL
A 737-300/400/500MAINTENANCE MANUAL
Stabilizer Buttock Line. A plane that is perpendicular to the horizontal stabilizer reference plane and parallel to the trace of the fuselage centerline. It is measured from stabilizer buttock line 0.00, the intersection of horizontal stabilizer reference plane and body buttock line 0.00.
Stabilizer Chord Plane. A plane through the trailing and leading edges of the stabilizer airfoil.
Leading Edge Station. A plane that is perpendicular to the horizontal stabilizer leading edge. It is measured from the Stabilizer Leading Edge Station 0.00, the intersection of the leading edge line extension and stabilizer buttock line 0.00.
Rear Spar Station. A plane that is perpendicular to the horizontal stabilizer rear spar. It is measured from the Rear Spar Station 0.00, the intersection of the rear spar and the trace of body buttock line 0.00 at the horizontal stabilizer reference plane.
Stabilizer Station. A plane that is perpendicular to the stabilizer rear spar and horizontal stabilizer reference plane. Stabilizer station 0.00 is at the intersection of the leading edge extension, body buttock line 0.00 and the horizontal stabilizer reference plane.
Nacelle Buttock Line. A plane parallel to a wing buttock line. Nacelle buttock line 0.00 is equivalent to wing buttock line 191.00
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A
737-300/400/500MAINTENANCE MANUAL
 PRINCIPAL DIMENSIONS AND AREAS - MAINTENANCE PRACTICES
______________________________________________________
 1.  General_______
 A.  Dimensions are included for the wing, ailerons, flaps, horizontal stabilizer surfaces, vertical stabilizer surfaces and body. Areas are included for the wing and stabilizer surfaces.
 TASK 06-13-00-222-001
 2.  Principal Dimensions and Areas (Fig. 201)______________________________
 A.  General
 (1)
Dimensions

 (2)
Overall Airplane

 -Length -- 109 feet-7 inches (33.4 m) (737-300)
 -Width -- 94 feet-10 inches (28.91 m)
 -Height (vertical stabilizer tip, top of the fairing to the ground) -- 36 feet-6 inches (11.13 m)

 (3)
Wing

 -Root Chord (theoretical, at the body centerline) -- 288.09 inches
 (7.32 m)
 -Basic Chord (theoretical) -- 186.72 inches (4.74 m)
 -Tip Chord (theoretical) -- 63.83 inches (1.62 m)
 -Planform Taper Ratio
 -Dihedral (wing reference plane with respect to the body reference plane) -- 6 degrees
 -Sweepback (25 percent chord line) -- 25 degrees
 -Aspect Ratio -- 9.16
 -Mean Aerodynamic Chord (basic wing only) -- 134.46 inches
 (3.41 m)
 -Body Station at 0% MAC -- 625.60

 (4)
Horizontal Stabilizer

 -Span -- inches
 -Tip chord (theroretical) -- 60 inches (1.52 m)
 -Sweepback (25 percent chord line) -- 30 degrees
 -Dihedral (horizontal stabilizer reference plane with respect to the body reference plane) -- 7 degrees
 -Aspect Ratio -- 4.04

 (5)
Vertical Stabilizer

 -Height -- inches
 -Root Chord (theroretical, leading edge at body station
 971.81 -- 205 inches (5.21 m)
 -Sweepback (25 percent chord line) -- 35 degrees
 -Aspect Ratio -- 1.81
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