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民用航空器维修人员执照英语参考试题(个人)
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Braking system is used to decrease run-down time or stop propeller rotation during engine power-off conditions.

A、 制动系统用于降低滑行速度,以及发动机停车状态下的停止螺旋桨旋转。

B、 制动系统是用来减少停车时间或在发动机关车的情况下使螺旋桨停止转动。

C、 在发动机低速运转或螺旋桨低速旋转时,制动系统能快速刹住。

答案:B

民用航空器维修人员执照英语参考试题(个人)
If the aircraft is parked on a slope, make sure that the wheel chocks are in position.
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从滑油箱上拆下磁性排放堵头。
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指示是系统中用来显示空气系统的温度、压力、控制位置等的部分。包括发射机、指示器等项目。
https://www.shititong.cn/cha-kan/shiti/000045bc-608d-6211-c0f0-9b9ce9a83100.html
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发动机可以把功率传给螺旋桨轴。
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The charts, diagrams, and text show the area, dimensions, stations, access doors and physical locations, of the structural members of the aircraft.
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For turbine engines, exhaust includes units external to the basic engine.
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Turbine blade tip clearances decrease when the turbine case is cooled.
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A red mark on the pin identifies the lubrication point.
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All persons who are in this area must use a respirator.
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Measure the resistance between the antenna baseplate and the airplane skin.
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民用航空器维修人员执照英语参考试题(个人)

Braking system is used to decrease run-down time or stop propeller rotation during engine power-off conditions.

A、 制动系统用于降低滑行速度,以及发动机停车状态下的停止螺旋桨旋转。

B、 制动系统是用来减少停车时间或在发动机关车的情况下使螺旋桨停止转动。

C、 在发动机低速运转或螺旋桨低速旋转时,制动系统能快速刹住。

答案:B

民用航空器维修人员执照英语参考试题(个人)
相关题目
If the aircraft is parked on a slope, make sure that the wheel chocks are in position.

A. 如果飞机停在机坪上,确保轮子刹车在位。

B. 如果飞机停靠在廊桥,一定确保轮档在位。

C. 如果飞机停在斜坡上,确保轮挡在位。

https://www.shititong.cn/cha-kan/shiti/000045bc-607f-f35f-c0f0-9b9ce9a83100.html
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从滑油箱上拆下磁性排放堵头。

A. Remove the magnesium drain plug from the hydraulic reservoir.

B. Replace the magnetic drain plug of the oil tank.

C. Remove the magnetic drain plug from the oil tank.

https://www.shititong.cn/cha-kan/shiti/000045bc-607b-785e-c0f0-9b9ce9a83100.html
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指示是系统中用来显示空气系统的温度、压力、控制位置等的部分。包括发射机、指示器等项目。

A. Indicating is that portion of the system which is used to indicate temperature, pressure, control positions, etc. of the air systems. Includes items such as transmitters, indicators, etc.

B. Indicators are systems used to display air temperature, pressure, control position, etc. It includes switches, thermometers and other components.

C. Indication system is used to indicate atmospheric temperature, pressure, control position, etc. It includes crossfeeding system, thermometer and other components.

https://www.shititong.cn/cha-kan/shiti/000045bc-608d-6211-c0f0-9b9ce9a83100.html
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发动机可以把功率传给螺旋桨轴。

A. The power is transmitted from the propeller to the engine.

B. The engine is used to transmit power to the propeller shaft.

C. The power is transmitted to the shaft by the engine cable.

https://www.shititong.cn/cha-kan/shiti/000045bc-6088-0181-c0f0-9b9ce9a83100.html
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The charts, diagrams, and text show the area, dimensions, stations, access doors and physical locations, of the structural members of the aircraft.

A. 飞机结构件的面积、尺寸、站位、接近门以及物理位置由表、图和文本表示。

B. 飞机结构件的面积、尺寸、纵剖面、接近门以及物理位置由表、图和文本表示。

C. 飞机结构件的面积、尺寸、水位线、接近门以及物理位置由表、图和文本表示。

https://www.shititong.cn/cha-kan/shiti/000045bc-6083-dd44-c0f0-9b9ce9a83100.html
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For turbine engines, exhaust includes units external to the basic engine.

A. 对涡轮发动机来说,排气系统包括发动机本体以外的部件。

B. 对涡轮发动机来说,排气系统包括发动机主系统内的装置。

C. 对涡轮发动机来说,排气系统不包括发动机主系统以外的装置。

https://www.shititong.cn/cha-kan/shiti/000045bc-6086-dc02-c0f0-9b9ce9a83100.html
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Turbine blade tip clearances decrease when the turbine case is cooled.

A. 当压气机机匣被冷却后,压气机叶片间距变小。

B. 当涡轮机匣被冷却后,涡轮叶尖距变小。

C. 当涡轮机匣被冷却后,涡轮叶片间距变小。

https://www.shititong.cn/cha-kan/shiti/000045bc-607e-bb23-c0f0-9b9ce9a83100.html
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A red mark on the pin identifies the lubrication point.

A. The location where a red mark is on the pin needs to be lubricated.

B. You should identify the red mark on the lubricant point.

C. The lubrication point shows that you can find marks on the pin.

https://www.shititong.cn/cha-kan/shiti/000045bc-607c-d58d-c0f0-9b9ce9a83100.html
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All persons who are in this area must use a respirator.

A. 此区域所有人员必须佩戴防毒面具。

B. 该区域所有人员必须佩戴口罩。

C. 必须给该区域的所有人员配置防烟面罩。

https://www.shititong.cn/cha-kan/shiti/000045bc-6078-787f-c0f0-9b9ce9a83100.html
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Measure the resistance between the antenna baseplate and the airplane skin.

A. Evaluate the impedance between the antenna baseplate and the airplane skin.

B. Record the measured resistance between the antenna baseplate and the airplane skin.

C. Perform the measurement of the resistance between the antenna baseplate and the airplane skin.

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