判断正误True or False: 每个ACMP被一个在驾驶舱顶头面板上的液压控制面板上的单独旋钮开关控制。Each ACMP is controlled by a separate toggle switch on the hydraulic control panel on the overhead panel in the flight compartment.

出现TCAS RA的信息和现象是( )。The information and phenomena of TCAS RA is that（）

出现TCAS TA的信息和现象是( )。The information and phenomena of TCAS TA is that（）

飞机失速的速度不是恒定的，但其根据飞机重量和机动载荷系数的变化而变化。对于特定的AOA,随着重量和载荷系数的( )，失速速度将( )增加。The speed at which an aircraft stalls is not constant, but is a function of the aircraft weight and the maneuvering load factor. ( ) weight and load factors will ( ) stall speeds for a given stall AOA.

当缝翼和襟翼放出时，失速AOA （ ）。The stall AOA （ ） when slats and flaps are extended.

对于特定的形态，失速AOA 通常是固定的。然而，对于后掠翼涡轮喷气飞机，由于马赫效应失速角通常随着高度的增加而（ ）。The stall AOA is normally constant for a given configuration. However, for swept wing turbojet aircrafts the stall angle generally （ ） as altitude increases due to the Mach effect.

高度低于（）英尺离地高度时，EGPWS能探测到“WINDSHEAR”（风切变）情况并发出警告；For altitude below () feet AGL, EGPWS can detect "Windshear" and generate warning.

如果接近正常抬前轮速度时遇到风切变，并且空速突然减小，则剩余跑道可能不足以使飞机加速到正常起飞速度。如果剩余跑道不足以使飞机停住在跑道上，则应在离跑道头之前至少（）英尺处起始正常抬前轮。确保调定到发动机最大推力。If windshear is encountered when close to normal rotation speed and airspeed suddenly decreases, remaining runway distance may not enough for airplane accelerating to normal take-off speed. If sufficient runway is NOT available to reject the take−off, Rotation should commence no later than () feet before the end of the runway. Ensure advance thrust levers forward to MAX thrust.

当探测到地形警戒或警告的情况时，在两个多功能显示器上将自动“跳出”地形显示，且范围默认为（）海里。When a terrain caution or warning is detected, the terrain display will automatically appear on the two MFDs with a default range of () nautical miles.

风切变警告，地形警告，失速警告，这3种警告的改出优先顺序依次为： the sequence
of recovery on the warnings of wind shear, terrain and stall is ( ).

地形警戒等级的安全避让裕度时间为（）秒，地形警告等级的安全避让裕度时间为（）秒。Safe avoidance margin for the alert level is ()seconds, and the safe avoidance margin for the warning level is ( ) seconds.