相关题目
左右探头开关，在正常飞行中是自动控制的，与开关位置无关The left and right probe switches are automatically controlled in normal flight and independent of switch position.
在地面，在自动模式下，当 其中一个发动机发电机打开且左右探头开关(在防冰控制面板上)选择 关闭,左右皮托管及备用皮托管以一半的动力来加热(自动模式在APU 发电机或外接电源下无此功能)。on ground. In automatic mode, when either engine generator is on and the LH and RH PROBES switches (on the ANTI-ICE control panel) are OFF, the LH and RH pitot probes and the standby pitot probe are heated at half power (automatic mode is not functional when the airplane is being powered by the APU generator or external power).
整流罩防冰和机翼防冰都是利用发动机热引气Both the bleed of cowl and the wing anti-ice are powered by the engine.
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.
