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A 737-300/400/500MAINTENANCE MANUAL …..................................1 R = REVISED, A = ADDED OR D = DELETED CHAPTER 55 F = FOLDOUT PAGE EFFECTIVE PAGES 17 B PAGE 1 JUL 12/02 LAST PAGE D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 55 - STABILIZERS TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ STABILIZERS 55-00-00 ___________ Description and Operation 1 ALL RUDDER, ELEVATOR AND HORIZONTAL 55-00-01 STABILIZERS Inspection/Check 601 ALL HORIZONTAL STABILIZER 55-10-00 _____________________ Description and Operation 1 ALL General 1 Stabilizer structure 1 THRUST BRACE LINKS 55-10-10
Removal/Installation 401 ALL ELEVATOR 55-20-00 ________ Description and Operation 1 ALL General 1 Elevators Elevator Control Tabs 1
VERTICAL STABILIZER (FIN) 55-30-00 _________________________ Description and Operation 1 ALL General 1 Vertical Fin Structure 1
Removal/Installation 401 ALL Inspection/Check 601 ALL DORSAL FIN 55-32-11 Removal/Installation 401 ALL VERTICAL STABILIZER (FIN) 55-33-11 LEADING EDGE Removal/Installation 401 ALL VERTICAL STABILIZER (FIN) TIP 55-33-21 Removal/Installation 401 ALL
RUDDER 55-40-00 ______ Description and Operation 1 ALL General 1 Rudder Structure 1
BBEJ Page 1 Mar 15/96 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL CHAPTER 55 - STABILIZERS TABLE OF CONTENTS_________________ Subject_______ Chapter SectionSubject_______ Page____ Effectivity___________ ATTACH FITTINGS_______________ Description and Operation General Horizontal Stabilizer Outboard Section Attach Fitting Horizontal Center Section Truss Attach Fitting Elevator Attach Fitting Rudder Attach Fitting 55-50-00 1 11 ALL
BBEJ Page 2 Mar 15/96 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL STABILIZERS - DESCRIPTION AND OPERATION _______________________________________ 1. General_______ A. The stabilizers comprise the empennage of the airplane and consist of a vertical stabilizer (fin), and a horizontal stabilizer (Fig. 1). The vertical fin, a structure composed of front and rear spars with interconnecting ribs and skin, is attached to the fuselage. The left and right horizontal stabilizer outboard sections are attached to an adjustable center section truss located within the fuselage. The movable center section pivots on two hinge joints attached to a bulkhead in the fuselage and is operated by a jackscrew mounted at the front spar. Each horizontal outboard section consists of two spars with interconnecting ribs and skin forming a torsion and bending structure. A rudder is hinged from the vertical fin and elevators are hinged from the horizontal stabilizer. A dorsal fin fairs in the fuselage and the vertical fin. Empennage Figure 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 55-00-00 ALL ú ú B01 Page 1 ú Oct 20/83 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL RUDDER, ELEVATOR AND HORIZONTAL STABILIZERS - INSPECTION/CHECK ______________________________________________________________ 1. General _______ A. This procedure has one task. The task gives instructions to do a visual inspection of the elevator spars and ribs, rudder spars and ribs, rudder mast fittings and internal backup fittings, mass balance weights including tip weight, and adjustable weights and weight support structure within the internal area of the rudder, elevator, and the horizontal stabilizers. TASK 55-00-01-206-001-B00 2. Examine the Composite Flight Controls _____________________________________ A. References (1) AMM 27-21-00/201 Remove the Pressure - Rudder Hydraulic Systems A & B
(2) 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 安定面 STABILIZERS
