相关题目
机翼防冰控制器是由直流汇流条1和直流重要汇流条供电The wing anti icing controller are powered by DC bus 1 and DC ESS BUS.
引气面板ISOL活门正常在什么位置? what is the normal position of ISOL on Bleed panel?
BLEED SOURCE(引气源)正常在什么位置？what is the normal position of BLEED SOURCE valve？
BLEED VALVES(引气活门)正常在什么位置？what is the normal position of BLEED VALVES？
正常引气构型状态下，机翼防冰交输引气活门在( )位置under normal bleed configuration，WING A/I BLEED valve is in ( ) position.
机轮刹车组件上使用除冰/防冰液将严重 降低刹车性能。The use of de icing / anti icing fluid on the wheel brake assembly will seriously reduce the brake performance.
在任何情况下，只要已经对飞机进行了防冰，决不能在现存的防冰覆盖层上再涂II类/III类/IV类除/防冰液Under no circumstances shall class II/III/IV deicing/antiicing fluids be re-applied to the existing anti-icing covers as long as the aircraft has been deiced.
以下选项当中不属于全静压系统的部件是The following options are not part of the total hydrostatic system.
飞机安装有( )个结冰探测系统，用来向飞行机组报警即将出现的结冰状态。结冰探测系统包括( )个独立的结冰探测器探头。The aircraft is equipped with （） ice-detection system to alert the flight crew of imminent ice-forming conditions. The ice detection system includes （） independent ice detector probe.
判断正误，如果起飞时需要接通防冰系统，起飞数据不需要修改。If the anti-ice system needs to be open before takeoff, the take-off data will not need to be modified.
