水平安定面配平系统的2个通道被断开是通过按压：The two channels of the horizontal stabilizer trim system are disengaged by pressing the:
A. 水平安定面配平控制面板上的马赫配平电门mach trim switchlight on the horizontal stabilizer trim control panel
B. 任一操纵盘上的STAB TRIM DISC电门 Stab trim disc switch on either control wheel
C. 水平安定面配平控制面板上的通道1和2 电门 Channel 1 and 2 switchlight on the horizontal stabilizer trim control panel
D. 任一操纵盘上的AP/SP DISC电门 AP/SP DISC switch on either control wheel
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判断正误True or False: 飞机的方向（偏航）控制是由方向舵并辅以偏航阻尼器来实现的。Directional (yaw) control of the aircraft is provided by the rudder, assisted by yaw damping.
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如果某地的QFE 为980hPa（标高200 米），则QNH 大致为
A. 1000hPa
B. 1005hPa
C. 1010hPa
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副翼系统卡阻的信息与现象Briefly introduce the informations and phenomens of AILERON system jammed.
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导航源，FMS,VOR,LOC都是使用什么选择？Nav source, FMS,VOR and LOC are selected using the
A. 显示控制面板display control panel
B. 大气数据基准面板Air data reference panel
C. 调谐选择面板Tuning select panel
D. 飞行控制面板Flight control panel
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发动机限制值EICAS系统上由各种符号，图形或颜色来显示最大值或最小值以及警示范围，那么N1%RPM在0-99.4%显示的颜色是什么？The engine limit display markings on EICAS must be used to determine compliance with the maximum/minimum limits and precautionary ranges. The color of N1% RPM 0 to 99.4% in EICAS
A. 红色Red
B. 黄色Amber
C. 绿色Green
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如果在 400 米 MSL 高度上空气的温度为 8℃，气温直减率等于标准大气的直减率，那么结冰层的
高度大约是多少
A. 1600 米 MSL
B. 1200 米 MSL
C. 1000 米 MSL
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(案例分析) 飞机在7200米的巡航高度，双人制飞行，机长负责操纵飞机，忽然机长侧出现火情，机长直接解开安全带使用驾驶舱的灭火瓶进行灭火。请问，这种处理方式对吗，如果不对请简述驾驶舱处置方法？
(Case analysis) An aircraft is cruising at 7200m, two pilots in the cockpit, and captain is the PF. Suddenly fire comes out near to the side of captain, the captain releases the seat belt and use the extinguisher in the cockpit to extinguish fire. is the handling method correct? please brief the correct handling methods?
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着陆技术（收油门的技术）会受到以下哪些因素影响? The landing technique (power reduction) is influenced by a number of variables including（）。
A. 空气密度和气温
air density and temperature
B. 侧风crosswind
C. 机场标高和跑道表面情况
airport elevation and runway surface condition
D. 以上全部above all
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判断正误True or False: 如果全部电源发生故障时，主飞行操纵将由 ACMP 3B(交流马达泵 3B)提供液压动力，该交流马达泵在应急情况下由空气驱动发电机 (ADG)提供电力。In the event of a total electrical power failure, the primary flight controls will remain hydraulically-powered by ACMP 3B, which will be powered by the air-driven generator (ADG) in an emergency.
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