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BOEING 737 MAINTENANCE MANUAL
CHAPTER 6 TAB PAGE DATE CODE PAGE DATE CODE PAGE DATE CODE PAGE DATE CODE EFFECTIVE PAGES SEE LAST PAGE OF LIST FOR NUMBER OF PAGES CONTENTS 6 1 FEB 20/87 5152 BLANK 6- 00 201 MAY 20/82 500202 APR 15/66 500203 MAY 20/82 500204 APR 15/66 500205 APR 15/66 500206 APR 15/66 500 6- 12-0 201 NOV 15/67 500202 APR 15/66 500203 MAY 01/99 500204 NOV 15/67 500 6- 22-0 201 AUG 15/68 515202 BLANK 6- 23-0 201 AUG 15/68 515202 BLANK 6- 31-0 201 FEB 20/87 500202 BLANK 6- 41-0 201 NOV 15/67 500202 BLANK 6- 51-0 201 MAY 20/82 500202 BLANK 6- 61-0 201 AUG 15/71 500202 BLANK
* = REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE C8 CHAPTER 6 EFFECTIVE PAGES MAY 01/99 PAGE 1
CHAPTER 6 DIMENSIONS AND AREAS TABLE OF CONTENTS Subject Subject No. DIMENSIONS AND AREAS........................................................................................... Maintenance Practices 6-00 ABBREVIATIONS PRINCIPAL DIMENSIONS PRINCIPAL DIMENSIONS AND AREAS ................................................................... Maintenance Practices 6-12-0 BODY STATIONS BODY STATION DIAGRAMS (STD PASSENGER)................................................... Maintenance Practices 6-22-0 BODY STATION DIAGRAMS (PASSENGER/CARGO CONVERTIBLE) .................. Maintenance Practices 6-23-0 VERTICAL STABILIZER AND RUDDER STATIONS VERTICAL STABILIZER AND RUDDER STATION DIAGRAMS............................... Maintenance Practices 6-31-0 HORIZONTAL STABILIZER AND ELEVATOR STATIONS HORIZONTAL STABILIZER AND ELEVATOR STATION DIAGRAMS ..................... Maintenance Practices 6-41-0 WING STATIONS WING STATION DIAGRAMS ..................................................................................... Maintenance Practices 6-51-0 ENGINE AND NACELLE STATIONS ENGINE AND NACELLE STATION DIAGRAMS ....................................................... Maintenance Practices 6-61-0
515 Feb 20/87 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Contents 6 Page 1
DIMENSIONS AND AREAS 1. General A. This chapter contains information on principle dimensions for the wing, ailerons, flaps, horizontal stabilizer surfaces, vertical stabilizer surfaces, and body; areas for the wing and tail surfaces; and station diagrams for the wing, vertical tail surfaces, and engine nacelle. B. Abbreviation terms used in defining the dimension, areas and stations are listed in the following paragraphs. 2. Abbreviations A. The airplane is divided into reference planes, designated as stations, waterlines and buttock lines, measured in inches. This provides a means of quickly identifying the location of components, the center of gravity and the distribution of the weight. (See figure 201.) B. Body B STA Body Station. The plane perpendicular and measured parallel to the body centerline from a point 130 inches forward of the nose. BBL Body Buttock Line. The plane measured perpendicular to the body vertical centerline plane, BBL 0.00. BWL Body Waterline. The plane measured perpendicular to a horizontal plane located 148.5 inches below the body, BWL 0.00. BRP Body Reference Plane. The horizontal plane, Body Waterline 208.1, at the top surface of the floor beams. C. Vertical Stabilizer Fin Sta Vertical Stabilizer Station. The plane perpendicular to the centerline of the vertical stabilizer rear spar. Distance is measured from Fin Station 0.00, the intersection of the leading edge line extension and the fin waterline 0.00. 500 May 20/82 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 6-00 Page 201
Fin WL Vertical Stabilizer Waterline. A horizontal plane measured parallel to a Body Waterline. Fin Waterline 0.00 is Body Waterline 300.50. Fin LE Sta Vertical Stabilizer Leading Edge Station. A plane perpendicular to the vertical stabilizer leading edge, measured from the fin leading edge station 0.00, the intersection of the leading edge line extension and the vertical stabilizer waterline 0.00. Rud Sta Rudder Station. A plane perpendicular to the rudder hinge centerline, measured from Rudder Station 0.00, the intersection of the rudder hinge centerline and vertical stabilizer waterline 0.00. D. Horizontal Stabilizer Stab Sta Horizontal Stabilizer Station. A plane perpendicular to stabilizer chord plane and plane of stabilizer rear spar, measured from stabilizer station 0.00, the intersection of the leading edge and stabilizer buttock line 0.00. SCP Stabilizer Chord Plane. A plane through the trailing and leading edges of the stabilizer airfoil. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737 AMM 飞机维护手册 DIMENSIONS AND AREAS
