506 Steering Collar Wear Limits
Aug 01/94 Figure 601 (Sheet 1) 32-51-61
Page 601
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Steering Collar Wear Limits 513
32-51-61 Figure 601 (Sheet 2) Oct 20/93
Page 602
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
NOSE GEAR STEERING DEPRESSURIZATION VALVE - R/I
EFFECTIVITY
Airplanes with steering depressurization valve
1. Equipment and Material
A. Ground Lock Assemblies (Ref 32-00-01)
B. Steering Lockout Pin
2. Remove Depressurization Valve (Fig. 401)
A. Check ground lock assembly is installed in nose gear.
B. Depressurize hydraulic system (A (Ref Chapter 29).
C. Disconnect hydraulic lines and cap both lines and valve fittings.
D. Remove three mounting bolts and remove valve.
3. Install Depressurization Valve (Fig. 401)
A. Position valve on mounting bracket and install three mounting bolts.
B. Remove caps from hydraulic lines and fittings. Connect hydraulic lines to valve.
C. Pressurize hydraulic system A and check valve installation for hydraulic leaks.
D. Remove hydraulic power if no longer required.
Feb 20/85 32-51-71 Page 401
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Steering Depressurization Valve 532
32-51-71 Figure 401 Oct 20/83
Page 402
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
LANDING GEAR POSITION INDICATING AND WARNING SYSTEM -DESCRIPTION AND OPERATION
1. General
A. The landing gear position indicating and warning system provides warning and indication for landing gear down and locked, landing gear not locked, and landing gear position not in accordance with control lever position. In addition, the down and locked position of each landing gear can be observed through inspection viewers. Green indicator lights come on when the landing gear are down and locked and the airplane is safe to land. Red warning lights come on and a warning horn sounds when the landing gears are not down and locked (Chapter 31). The landing gear position indicating and warning system consists of the following:
(1)
Three green indicator lights, one for each main gear, and one for the nose gear indicate gear down and locked. The indicator lights are controlled by the landing gear lock and position sensors, in conjunction with solid-state circuits, to come on when the respective landing gear is down and locked. The indicator lights are mounted on the pilots' landing gear panel above the landing gear control lever (Fig. 1). A dimmer switch on the center panel is provided to reduce the indicator light intensity during night operations.
(2)
A test switch testing the landing gear indicator and warning lights is mounted near the dimmer switch on the center panel.
(3)
Three red warning lights, one for each main gear, and one for the nose gear indicate an unsafe-to-land condition (Fig. 1). The warning lights come on when the landing gear and control lever positions do not coincide, when any landing gear is unlocked, or when the engine thrust levers are in idle range and the landing gear are not down and locked. The lights are controlled by the landing gear control lever position switch. Additional control of the lights is provided by the landing gear lock and position sensors on the landing gear and the solid-state circuits in the landing gear electrical module. The lights will remain on and cannot be turned off if the landing gear and control lever positions do not coincide or any landing gear is unlocked. A dimmer switch on the center panel is provided to reduce the indicator light intensity during night operations.
(4)
A warning horn sounds when the landing gear position is incorrect for the current operating conditions. For more information on the warning horn, refer to Chapter 31, Aural Warning and Call Devices.
503
Aug 15/77 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 32-61-0 Page 1
Indicator and Warning Lights 508
32-61-0 Figure 1 Aug 1/74
Page 2
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
2. Landing Gear Mechanical Downlock Indication
A. Mechanical downlock indication of the landing gear is provided by observing the alignment of red paint stripes or arrows located on locking components of the landing gear (Fig. 2 and 3). The down and locked position of the landing gear can be observed from inside the airplane through landing gear downlock viewers. For more information on the viewers, refer to Viewers and Observation Windows, Chapter 56.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 起落架 LANDING GEAR(182)
