A、 当达到预设阈值时,烟雾探测器通过客舱内部通信数据系统触发警告。
B、 当预设的温度达到时,烟雾探测器会发出警告,通过客舱内部通信数据系统。
C、 当预设的数值达到时,客舱内部通信数据系统里的烟雾探测器会发出警告。
答案：A
A、 当达到预设阈值时,烟雾探测器通过客舱内部通信数据系统触发警告。
B、 当预设的温度达到时,烟雾探测器会发出警告,通过客舱内部通信数据系统。
C、 当预设的数值达到时,客舱内部通信数据系统里的烟雾探测器会发出警告。
答案：A
A. If you find metal particles in the pump,find their source and repair the defective part.
B. If magnetic particles are found in thepump,locate their location and repair the affected part.
C. Locate their source and disassemble the defective part if you find metal objects.
A. The flight deck is located between the pressure dome and the front passenger door,and it is above the floor.
B. Cockpit is on the floor panel and between the pressure dome and the rear passenger partition.
C. Flight compartment is above the floor and between the forward passenger partition and the forward pressure dome.
A. 表格遵循以下显示的数据。
B. 以下表格显示该数据。
C. 后面的桌子上放着数据。
A. 本程序中要求不止一个人。
B. 对于本程序来说,更多的人员要求是必要的。
C. 执行本程序需要超过一个人。
A. The brackets should be connected to the nearest components.
B. Align the brackets with the adjacent components.
C. Keep the brackets engaged with the nearby components.
A. Failure of the air turbine starter can trigger the engine overheat and fire indications.
B. The air turbine starter fails to trigger the engine overheat and fire indications.
C. Failure of the air turbine starter can cause the engine overheat and fire indications.
A. 在初始蒙皮的初始紧固件位置,安装埋头铆钉。
B. 在初始蒙皮的初始紧固件位置,制作埋头垫圈。
C. 使埋头垫圈适用于初始蒙皮上的初始紧固件。
A. Remove the test cap between the Precooler Control Valve and the 3908 sensor on the control pressure sense line and ensure that there is air flowing out of the port.
B. From precooler control valve to 3908 sensor,remove the sense line test cap,make certain thatthe air flows from the test hub.
C. The purpose of the test cap removal from the Precooler Control Valve to the 3908 sensor is to guarantee that there is airflow at the test port.
D. C.The purpose of the test cap removal from the Precooler Control Valve to the 3908 sensor is to guarantee that there is airflow at the test port.
A. The toxic conditions are given in Paragraph 2.0.
B. All the test result are given in Paragraph 2.0.
C. All the test conditions are given in Paragraph 2.0.
A. Spoilers are used to increase the drag of the aircraft in flight,or to interrupt lift during landing and during rejected take-off.
B. Spoilers are used to enhance aircraft resistance in flight or to disrupt boost during landing and when take-off is canceled.
C. Spoilers are used to increase the aircraft drag in flight,or destroy the lift during landing and in case of aborted take-off.
