相关题目
EICAS上显示＇PARK BRAKE SOV＇警戒信息表明：The＇PARK BRAKE SOV＇ caution message displayed on EICAS indicates:
判断正误True or False: 当飞机防滞功能受限或没有防滞功能时，将会严重影响飞机的刹车性能，但在这种情况下，飞机的着陆距离并不会受影响。Aircraft braking performance is severely affected when operating the aircraft with limited or no anti-skid protection， which will not affect the landing distance。
EICAS上显示＇IB BRAKE PRESS＇警戒信息表明：The ＇IB BRAKE PRESS＇ caution message displayed on EICAS indicates:
判断正误True or False: 在空中，没有机轮承重信号时，防滞控制活门释压以防止机轮在接地时锁死。In the air, with no weight-on-wheels signal, the anti-skid control valves dump pressure to prevent wheel lock-up on touchdown.
防滞系统是由（ ）来提供动力的。The anti-skid system is powered by ( ).
判断正误True or False: 在每个刹车组件上装有两个刹车磨损指示器，用于提供目视的刹车磨损指示。Two brake wear indicator pins, installed on each brake assembly, are used to provide a visual indication of brake wear.
EICAS上显示＇A/SKID INBD＇警戒信息表明：The ＇A/SKID INBD＇ caution message displayed on EICAS indicates:
判断正误True or False: 如果失去一个液压系统，飞机将保持50％的对称刹车能力并且工作的刹车仍有50%防滞控制功能。With the loss of one hydraulic system, the aircraft has 50% symmetric braking capability with 50% anti-skid control to the working brakes.
判断正误True or False: 如果刹车管路出现泄漏，相应的液压保险装置将关闭液压管路，防止整个系统的液压油漏失。If a leak occurs in a brake line, the associated hydraulic fuse will close off the hydraulic line, preventing loss of the entire system fluid.
刹车控制活门通过（ ）个独立的防滞控制活门和（ ）个液压保险装置，计量与脚蹬压力成比例的液压压力，传递到四个主机轮刹车组件。The brake control valves meter hydraulic pressure, proportional to the pedal pressure, to the four main wheel brake units, through（ ） independent anti-skid control valves and（ ） hydraulic fuses.
