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A 737-300/400/500MAINTENANCE MANUAL …..................................1 R = REVISED, A = ADDED OR D = DELETED CHAPTER 53 F = FOLDOUT PAGE EFFECTIVE PAGES 17 B PAGE 2 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D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 53 - FUSELAGE TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ FUSELAGE 53-00-00 ________ Description and Operation 1 ALL MAIN FRAME 53-10-00 __________ Description and Operation 1 ALL FRAMES AND BULKHEADS 53-11-00 Description and Operation 1 ALL STRINGERS AND OTHER LONGITUDINAL 53-12-00
MEMBERS Description and Operation 1 ALL PANEL - KEEL BEAM BLOWOUT 53-12-11
Removal/Installation 401 ALL STRUCTURE AROUND OPENINGS 53-13-00 Description and Operation 1 ALL LOWER DOORSILL SCUFF PLATE 53-13-01
Removal/Installation 401 ALL WHEEL WELL 53-14-00 Description and Operation 1 ALL
AUXILIARY STRUCTURE 53-20-00 ___________________ PASSENGER CABIN FLOORS 53-21-00 Description and Operation 1 ALL Removal/Installation 401 ALL Approved Repairs 801 ALL BARRIER - WATER 53-21-11
Approved Repairs 801 ALL FIXED PARTITIONS 53-22-00 Description and Operation 1 ALL
PLATES AND SKINS 53-30-00 ________________ SKIN 53-31-00 Description and Operation 1 ALL STABILIZER TO BODY FRONT SPAR 53-31-31
SLIDING SEAL Removal/Installation 401 ALL ATTACH FITTINGS 53-40-00 _______________ STRUCTURE ATTACHMENT FITTINGS 53-41-00 Description and Operation 1 ALL Door Attachment Fittings 1 Landing Gear Attachment 1 Fittings 53-CONTENTS
BBEJ Page 1 Mar 15/96 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL CHAPTER 53 - FUSELAGE TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ EQUIPMENT ATTACHMENT FITTINGS 53-42-00 Description and Operation 1 ALL Miscellaneous Equipment 1 Attachment Fittings Seat Attachment Fittings 1 PASSENGER CABIN AND CARGO 53-42-11 COMPARTMENT TRACKS Cleaning/Painting 701 ALL
AERODYNAMIC FAIRING 53-50-00 ___________________ FILLET FAIRINGS 53-51-00 Description and Operation 1 ALL AFT WING-TO-BODY FAIRING 53-51-21
Removal/Installation 401 ALL FORWARD FAIRINGS - WING-TO-BODY 53-51-19 Removal/Installation 401 ALL MID FAIRINGS - WING-TO-BODY 53-51-20 Removal/Installation 401 ALL WING-TO-BODY FAIRING BLOWOUT 53-51-11 PANEL Removal/Installation 401 ALL NOSE RADOME 53-52-00 Description and Operation 1 ALL Removal/Installation 401 ALL Inspection/Check 601 ALL Cleaning/Painting 701 ALL DIRECTOR BAR - GLIDE SLOPE 53-52-31
ANTENNA Removal/Installation 401 ALL LIGHTNING DIVERTER STRIPS 53-52-03 Maintenance Practices 201 ALL TAIL CONE 53-53-00 Removal/Installation 401 ALL
BBEJ Page 2 Jul 15/97 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL FUSELAGE - DESCRIPTION AND OPERATION ____________________________________ 1. General_______ A. The fuselage is a semimonocoque structure consisting of skin reinforced by circumferential frames and longitudinal stringers. Major fuselage components are illustrated in Fig. 1. B. A typical section through the fuselage consists of an upper oval lobe and a lower oval lobe which intersect approximately at the floor level. At the intersection the fuselage is reinforced by transverse floor beams. Above this floor structure, which extends from the front pressure bulkhead at body station 178 to the rear pressure bulkhead at body station 1016, the upper lobe of the fuselage encloses the cabin and is basically a continuous shell, with cutouts in the skin for doors and windows. Below the floor the continuity of the lower lobe, which encloses the cargo compartments, is interrupted by several major structural features: the nose landing gear wheel well, the cavity for the center wing box and the main landing gear wheel well. Aft of the rear pressure bulkhead the floor is discontinued and this section of the fuselage, which tapers towards its aft end, supports the vertical fin, the horizontal stabilizer, a tail skid and contains a compartment with fireproof walls for the APU. 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 机身 FUSELAGE
