06-00-01
ALL ú ú 01 Page 205 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
06-00-01
ALL ú ú 01 Page 206 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 DIMENSIONS AND AREAS(3)
