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.

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?

低速中断和高速中断的分界值速度是多少？What is the boundary speed for determining low speed and high speed rejected takeoff?

V1后防滞失效是否可以中断起飞？Can the takeoff be rejected after V1 due to anti-skid failure?

中断起飞的简令由谁来完成？Who shall complete the briefing for rejected takeoff?

中断起飞后应该遵守多久的刹车冷却时间？How much time shall be followed for cooling brakes after rejecting takeoff?

高原机场80节以后什么情况不能中断起飞？Due to which condition can the rejected takeoff not be performed after 80 knots at plateau airport?

单发复飞时，推力手柄应设置在( ) For the single engine go-around, the thrust lever should be set at( )

进近时发动机失效，在能完成单发进近程序且有把握的情况下，主飞飞行员应( ) For ENGINE FAILURE DURING APPROACH, If stable approach can be accomplished，PF shall( )

单发进近时，N1 推力设定值比正常进近时( ) For SINGLE ENGINE APPROACH, N1 is ( ) than normal thrust setting

单发进近，襟翼为（ ）For SINGLE ENGINE APPROACH, the flap should be set to （ ）.