当可操纵副翼一侧的飞行员选择亮着的ROLL SEL 电门时，会发生什么？What happens when the pilot with the operable aileron selects the illuminated ROLL SEL switchlight?
A. 控制钢索分离，任一飞行员控制一个副翼和一个扰流副翼The control cable is split and each pilot controls an aileron and a spoileron.
B. 横滚操纵由一个副翼和2个扰流副翼提供。Roll control is provided by one aileron and both spoilerons.
C. 飞行员控制本侧副翼和对侧扰流副翼。The pilot controls the onside aileron and the cross-side spoileron.
D. SSCU 自动给飞行员提供两侧副翼和扰流副翼。The SSCU automatically provides the pilot with both ailerons and spoilerons.
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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：
A. 外侧多功能扰流板、起落架、外侧刹车 Outboard multifunction spoiler panels、landing gear、Outboard brakes
B. 外侧刹车、升降舵、内侧地面扰流板Outboard brakes、elevators、Inboard ground spoilers
C. 左发反推、外侧多功能扰流板、外侧地面扰流板 Left thrust reverser、Outboard multifunction spoiler panels、Outboard ground spoilers
D. 方向舵、前轮转弯、起落架 Rudder、nosewheel steering、landing gear
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单发操作过程中，当油门杆在什么位置时，自动性能储备（APR）系统被激活：During single engine operation, the automatic performance reserve(APR)system is activated when the thrust lever for the:
A. 工作发动机一侧油门杆放到爬升卡位 operating engine is placed in the CLIMB detent
B. 不工作的发动机一侧油门杆放到TOGA卡位 shut down engine is placed in the TOGA detent
C. 工作发动机一侧油门杆放到TOGA卡位 operating engine is placed in the TOGA detent
D. 不工作的发动机一侧油门杆放到最大推力卡位 shut down engine is placed in the MAX POWER detent
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发动机的最大额定功率为在海平面的 ISA+15°C(86°F)情况下The engine performance is flat rated at 59°F (15°C) at sea level as follows:
A. 正常起飞推力额定功率Normal take-off thrust – 13360 lb (59.43 kN)
B. 最大起飞推力（APR）额定功率Max take-off thrust (with APR) – 13360 lb (59.43 kN)
C. 最大连续推力额定功率Max continuous thrust – 13360 lb (59.43 kN)
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当在低高度难以控制飞行航迹，或在出现“WINDSHEAR、WINDSHEAR、WINDSHEAR”音响警告，并伴随着飞行指引仪显示风切变引导时，飞行员应执行哪些动作？When flight path is difficult to be controlled at low altitude, or "WINDSHEAR" "WINDSHEAR" "WINDSHEAR" aural warning comes on, and with windshear guidance on FD, pilot shall:
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在卫星云图上，纤维状纹理是哪种云的特征＿＿
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电子飞行仪表系统（ EFIS）包含以下哪些部件？Which of the following are components of EFIS system?
A. 电子飞行显示器 Electronic Flight Displays
B. 显示转换面板和显示控制面板 Display Reversionary Panel and Display Control Panel
C. 源选择面板 Source Selector Panel
D. 以上全部 All above
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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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如果在加油时发生燃油溢出，应该立即采取的措施是：
A. "立刻停止加油,操作人员必须离开加油区
B. 关闭加油区域内的地面电源车、其它发动或电动机，避免打开其他任何电源
C. 通知机场消防队,通知机场管理部门
D. 立即警告机上的每个人
E. 以上全部"
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起飞后3000尺，应增速（ ）After takeoff, at 3000 feet, the plane shall be accelerated to ( ).
A. 250KIAS
B. 限制速度. Restricted speed
C. 230KIAS
D. 250KIAS或者限制速度. 250KIAS or restricted speed
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