Control
Panel - Autobrake Control 1
Switches - Hydraulic Pressure 7
Valves - Autobrake Shuttle 7
Operation 9
Trouble Shooting 101 ALL Adjustment/Test 501 ALL MODULE - AUTOBRAKE PRESSURE 32-43-46
CONTROL
Maintenance Practices 201 ALL Filter Removal/Installation 201 Pressure Switch 209
Removal/Installation
Servo Valve 205
Removal/Installation
Solenoid Shutoff Valve 203
Removal/Installation
Removal/Installation 401 ALL
VALVE - AUTOBRAKE SHUTTLE 32-43-26
Removal/Installation 401 ALL
PARKING BRAKE SYSTEM 32-44-00
Description and Operation 1 ALL General 1 Light - Parking Brake 1 Linkage - Parking Brake 1 Valve - Parking Brake Shutoff 1 Operation 6
Trouble Shooting 101 ALL Adjustment/Test 501 ALL LINKAGE - PARKING BRAKE 32-44-11
Removal/Installation 401 ALL VALVE - PARKING BRAKE SHUTOFF 32-44-21 Removal/Installation 401 ALL
32-CONTENTS
BEJ Page 10 Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CHAPTER 32 - LANDING GEAR
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
TIRES AND WHEELS 32-45-00
Description and Operation 1 ALL General 1 Snubber - Nose Wheel 3 Wheel and Tire - Main Gear 1 Wheel and Tire - Nose Gear 1
Maintenance Practices 201 ALL Inspection/Check 601 ALL SNUBBER - NOSE GEAR WHEEL 32-45-31
Maintenance Practices 201 ALL Inspection/Check 202 Removal/Installation 201
WHEEL - NOSE GEAR 32-45-21 Removal/Installation 401 ALL WHEEL AND TIRE - MAIN GEAR 32-45-11 Removal/Installation 401 ALL
STEERING 32-50-00
________ NOSE WHEEL STEERING SYSTEM 32-51-00 Description and Operation 1 ALL General 1 Cables - Steering 6 Collar - Steering 2 Mechanism - Rudder Pedal 6 Steering Valve - Steering Metering 1 Operation 11 Trouble Shooting 101 ALL Adjustment/Test 501 ALL ACTUATOR - RUDDER PEDAL STEERING 32-51-81 ROTARY Removal/Installation 401 ALL CABLES - STEERING 32-51-31 Removal/Installation 401 ALL Inspection/Check 601 ALL COLLAR - STEERING 32-51-61 Removal/Installation 401 ALL Inspection/Check 601 ALL CYLINDER - STEERING 32-51-51 Removal/Installation 401 ALL MECHANISM - RUDDER PEDAL 32-51-21 STEERING Removal/Installation 401 ALL
32-CONTENTS
BEJ Page 11 Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CHAPTER 32 - LANDING GEAR
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
NOSE LANDING GEAR 32-51-71 DEPRESSURIZATION VALVE Removal/Installation 401 ALL STEERING WHEEL AND CABLE DRUM 32-51-41 Removal/Installation 401 ALL VALVE - STEERING METERING 32-51-11 Removal/Installation 401 ALL
POSITION AND WARNING 32-60-00
____________________ LANDING GEAR POSITION INDICATING 32-61-00 AND WARNING SYSTEM Description and Operation 1 ALL General 1 Indication - Landing Gear 3 Mechanical Downlock Sensors - Landing Gear Uplock 3 and Downlock Switch - Control Lever 3 Position Operation 8 Trouble Shooting 101 ALL Adjustment/Test 501 ALL Cleaning/Painting 701 ALL SENSOR - MAIN GEAR DOWNLOCK 32-61-31 Removal/Installation 401 ALL SENSOR - MAIN GEAR UPLOCK 32-61-21 Removal/Installation 401 ALL Adjustment/Test 501 ALL SENSOR - NOSE GEAR DOWN 32-61-51 Removal/Installation 401 ALL SENSOR ACTUATOR - NOSE GEAR LOCK 32-61-41 Removal/Installation 401 ALL SWITCH - CONTROL LEVER POSITION 32-61-11 Removal/Installation 401 ALL
32-CONTENTS
BEJ Page 12 Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
LANDING GEAR - DESCRIPTION AND OPERATION
________________________________________
1. General_______
A. The landing gear consists of two main gear and one nose gear (Fig. 1). Each main gear is located aft of the rear wing spar inboard of the engine nacelles. The nose gear is located below the aft bulkhead of the control cabin.
B. The main and nose gear use air-oil type shock struts to absorb impact on landing and vibrations and shock from movement of the airplane on the ground. Each nose and main gear is equipped with two tire and wheel assemblies. Each main gear wheel is fitted with disc-type hydraulic brakes modulated by an antiskid system.
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 起落架 LANDING GEAR 1(4)
