A 737-300/400/500MAINTENANCE MANUAL
Air China Group ~........................................................................................................
| PAGE DATE CODE | PAGE DATE CODE | PAGE DATE CODE || | | || | | ||CHAPTER 6 TAB | | || | | ||DIMENSIONS AND AREAS | | || | | ||EFFECTIVE PAGES | | ||SEE LAST PAGE OF LIST | | ||FOR NUMBER OF PAGES | | || | | || | | ||6-CONTENTS | | || 1 MAR 15/96 BEJ | | || 2 BLANK | | || | | ||06-00-01 | | || 201 MAR 15/96 01 | | || 202 JUN 25/84 01 | | || 203 JUN 25/84 01 | | || 204 JUL 15/91 02 | | || 205 MAR 15/96 01 | | || 206 MAR 15/96 01 | | || | | ||06-13-00 | | || 201 JUL 12/01 03 | | || 202 JUL 12/01 02 | | || 203 JUL 12/01 03 | | || 204 BLANK | | || | | ||06-25-00 | | || 201 NOV 12/01 02 | | || 202 NOV 12/01 02 | | || | | ||06-32-00 | | || 201 NOV 15/91 01 | | || 202 MAR 15/99 01 | | || | | ||06-42-00 | | || 201 NOV 12/01 02 | | || 202 NOV 12/01 02 | | || | | ||06-52-00 | | || 201 NOV 15/91 01 | | || 202 JUL 15/98 01 | | || | | ||06-62-00 | | || 201 MAR 15/92 01 | | || 202 MAR 15/92 01 | | || | | || | | || | | || | | || | | || | | || | | || | | || | | || | | || | | || | | |2..................................…..................................…..................................1
R = REVISED, A = ADDED OR D = DELETED CHAPTER 06 F = FOLDOUT PAGE EFFECTIVE PAGES 17 PAGE 1 JUL 12/02 LAST PAGE
D6-37537
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 06 - DIMENSIONS AND AREAS
TABLE OF CONTENTS
_________________
Chapter
Section Subject_______ Subject ____ Effectivity
_______ Page ___________
DIMENSIONS AND AREAS 06-00-00
____________________ DIMENSION AND AREAS 06-00-01 Maintenance Practices 201 ALL PRINCIPAL DIMENSIONS AND AREAS 06-13-00 Maintenance Practices 201 ALL General Principal Dimensions 201
BODY STATIONS 06-20-00
_____________ BODY STATION DIAGRAM 06-25-00 Maintenance Practices 201 ALL
VERTICAL STABILIZER AND RUDDER 06-30-00
______________________________ STATIONS
________
VERTICAL STABILIZER AND RUDDER 06-32-00
STATION DIAGRAM
Maintenance Practices 201 ALL
HORIZONTAL STABILIZER AND ELEVATOR 06-40-00
__________________________________ STATIONS
________
HORIZONTAL STABILIZER AND ELEVATOR 06-42-00
STATION DIAGRAM
Maintenance Practices 201 ALL
WING STATIONS 06-50-00
_____________ WING STATION DIAGRAM 06-52-00 Maintenance Practices 201 ALL
ENGINE AND NACELLE STATIONS 06-60-00
___________________________ ENGINE AND NACELLE STATION DIAGRAM 06-62-00 Maintenance Practices 201 ALL
6-CONTENTS
BEJ Page 1 Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
DIMENSIONS AND AREAS - MAINTENANCE PRACTICES
____________________________________________
1. General_______
A. This chapter gives the principal dimensions for the wing, ailerons, flaps, horizontal stabilizer surfaces, vertical stabilizer surfaces, and body. It also gives areas for the wing and tail surfaces. There are station diagrams for the body, wing, vertical tail surfaces, engine nacelle and access doors and panels.
TASK 06-00-01-222-001
2. Reference Planes and Lines (Fig. 201)__________________________
A. General
(1)
The airplane is divided into stations, waterlines, and buttock lines. They are measured in inches. They will help you quickly identify the location of components, the center of gravity and the weight distribution.
(2)
Standard Abbreviations and Definitions
(a) Fuselage
B STA,BS, or STA Body (Fuselage) Station. A plane that is perpendicular to the fuselage centerline. It is measured from a point 130.00 inches forward of the nose.
BBL or BL Body (Fuselage) Buttock Line. A vertical plane that is parallel to the vertical centerline plane, BBL 0.00. It is found by its perpendicular distance from the fuselage centerline plane. (It is a measurement of width.)
BRP Body (Fuselage) Reference Plane. A plane that is perpendicular to the BBL plane and goes through BWL 208.10, the top of the main deck floor beams.
BWL or WL Body (Fuselage) Waterline. A plane that is perpendicular to the BBL plane, parallel to the fuselage centerline. It is measured from a parallel imaginary plane, BWL 0.00, 148.5 inches below the lowest fuselage surface.
LBL Left Buttock Line
RBL Right Buttock Line
(b) Wing
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
