Electrical Power system is about units and components which generate, control and supply AC and/or DC electrical power for other systems, including generators and relays, inverters, batteries, etc.
A. 电源系统讲的是发电、控制和向其他系统提供交流或直流电的组件和部件，包括发电机、继电器、变流器、电瓶等。
B. 电源系统讲的是发电、控制和向其他系统提供交流或直流电的组件和部件，包括发电机、继电器、整流器、电瓶等。
C. 电源系统讲的是发电、控制和向其他系统提供交流或直流电的组件和部件，包括发电机、继电器、静变流器、电瓶等。
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Equivalent substitutes can be used.
A. Substitutes with different quality can be used.
B. You can not use substitutes with same quantity.
C. Equivalent substitutes are permitted to use.
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If the components fall, permanent damage can occur.
A. 如果部件跌落，有可能会造成轻微的损坏。
B. 如果部件掉落，可能会造成永久性的损坏。
C. 部件永久性的损坏可能是由掉落造成的
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In the description of the airplane＇s Landing Gear, wheel brakes shall be described.
A. 描述飞机起落架时，应描述前轮制动。
B. 描述飞机起落架时，应描述机轮刹车。
C. 描述飞机起落架时，应描述机轮停车。
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Inspection and observation are the windows used for examining compartments and equipment in and about the airplane, including items such as transparent material, its frame, etc.
A. 检查和观察是用于检查飞机内部和周围的舱室和设备的窗口，包括透明材料、框架等。
B. 检查窗和观察窗是用于检查飞机内部和飞机上的舱室和设备的窗口，包括透明材料、框架等。
C. 检查和观察是用于检查飞机内部和周围的舱室和设备的窗口，包括透明材料、其框架等项目。
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Make sure the sealant is continuously squeezed out along the edges of the contact surfaces.
A. 确保密封剂被完全挤出接触面边缘。
B. 确保沿接触面边缘持续涂抹封严胶。
C. 确保封严胶沿接触面边缘不断挤出。
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Data shall be presented as Calibrated Airspeed versus Indicated Airspeed assuming zero instrument error.
A. 数据应该被显示为仪表空速和指示空速来保证零误差。
B. 数据应作为标定空速呈现，而不是零机械误差的仪表空速。
C. 假定仪表误差为零，数据应以校正空速和指示空速显示。
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本章应提供制造商认为必要的信息，以便在飞机使用寿命内可能需要的各种维修、大修或重要修理中对飞机进行适当的校平。
A. Necessary information by manufacturer should be provided in this chapter to maintain, overhaul or major repair the aircraft so as to properly level it during the life of the aircraft.
B. In order to properly level the aircraft when performing repair, overhaul or major repairs during the life of the aircraft, this chapter should provide all considered information by manufacturer.
C. This chapter shall provide that information considered necessary by the manufacturer to properly level the aircraft for any of the various maintenance, overhaul or major repairs which might become necessary during the life of the aircraft.
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The system interface circuits adapt to the physical properties of the connected systems.
A. 系统接口电路适配已连接系统的物理特征。
B. 系统的电路跳开关符合连接系统的物理特性。
C. 系统电路的物理特点与所连接系统相匹配。
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The resulting data were used to determine if the component should be considered for incorporation into the CAP.
A. 如果这个部件应该纳入CAP，那么使用最终数据做出判断。
B. 公司应利用现有数据判断该部件是否与CAP相关联。
C. 已用所得数据来确定是否应将该部件纳入CAP。
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