在卫星云图上，锋面常表现为

从下列中选出四个与气源系统相关的EICAS页面From the list below, select the four EICAS pages associated with the pneumatic system.

只在环控简图页上显示的是：only the ECS synoptic page displays the:

判断正误True or False：引气管理是全自动的，但是在非正常运行状态下，可以人工控制该系统。Bleed air management is fully automated; however, manual control of the system is provided for non-normal operations.

＇ISOL FAIL＇警戒信息指示：＇ISOL FAIL＇ caution message indicates:

＇BLEED MISCONFIG＇警戒信息指示：＇BLEED MISCONFIG＇ caution message indicates:

刹车温度监控系统在红区，说明刹车温度读数（ ）。If Brake temperature monitoring system (BTMS) is in the red range，which indicates that the readout is（ ）.

判断正误True or False: 起落架和刹车温度监控系统操作的指示显示在主页上。The EICAS primary pages present indications of landing gear and BTMS operation.

如果在无线电高度小于 ( ) AGL 并且指示空速小于 ( )KIAS时，任何一个起落架没有放下并锁定，那么系统将发出＇TOO LOW GEAR＇的语音警告。The ＇TOO LOW GEAR＇ aural warning sounds if any landing gear is not down and locked with the radio altitude less than ( ) ft AGL and the indicated airspeed at less than ( ) KIAS.

判断正误True or False:当一个推力杆在慢车位，且起落架没有放下并锁定时，起落架警告喇叭可以被静音。The landing gear warning horn may be MUTED with one thrust lever at IDLE and the landing gear not in the down and locked position.

EICAS上显示＇PARK BRAKE SOV＇警戒信息表明：The＇PARK BRAKE SOV＇ caution message displayed on EICAS indicates: