80Kts以后V1前出现以下哪种情况要中断起飞？Which condition(s) come(s) out, the takeoff shall be rejected after 80kts and before V1?

判断正误True or False: 1号系统和2号系统主泵是发动机驱动泵(EDPs), 1号系统EDP(1A)是由左发驱动而2号系统EDP(2A)是由右发驱动。No. 1 and No. 2 main pumps are Engine Driven Pumps (EDPs). System No. 1 EDP (referred to as 1A) is driven by the left engine and system No. 2 EDP (referred to as 2A) is driven by the right engine.

判断正误True or False: 1号、2号和 3号系统备用泵(1B、2B和3B)是交流马达泵(ACMPs)。 System No. 1, 2 and 3 backup pumps (referred to as 1B, 2B and 3B) are Alternating Current Motor Pumps (ACMPs).

液压系统为 ( ) 操作提供动力。The hydraulic systems supply power to operate the（）

下列哪些由1号液压系统提供动力： Which of the following are powered by hydraulic system 1：

下列哪些由2号液压系统提供动力： Which of the following are powered by hydraulic system 2：

下列哪些由3号液压系统提供动力： Which of the following are powered by hydraulic system 3：

判断正误True or False: 2号液压系统控制方向舵、右侧副翼、右反推。 Hydraulic system 2 controls rudder, right aileron and right thrust reverser.

液压系统1和2的主要部件有： The main components of Hydraulic system 1&2 includes:

在双发故障的情况下(液压发动机驱动泵和整体驱动发电机不工作)，ADG自动放出，主飞行控制系统将从（）液压泵上获得液压动力。In the event of a double engine failure (the hydraulic EDP and IDG inoperative), ADG will automatically deploy, the primary flight controls will remain hydraulically powered from ACMP（ ）

左副翼由液压系统( )提供动力。The left aileron is powered by hydraulic system ( ).