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861.底漆层厚度必须介于 0.05 毫米到 0.06 毫米之间。

A、 The coating thickness must be more than 0.05mm and less than 0.06mm.

B、 The thickness of the second coating layer must be 0.05mm and 0.06mm.

C、 The thickness of primer layer must be between 0.05 mm and 0.06 mm.

答案:C

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1568.The turbine clearance control sensor supplies the EEC with temperature data from the high pressure turbine shroud.
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1972.In the description of the airplane's Flight Controls,trimming arrangements shall be explained.
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1279.Scratches can prevent the free movement of the piston in the sleeve.
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1539.When the entire storage area is full,new fault data,i.e.data for the current flight leg,will replace/overwrite the data for the oldest flight leg in the fault history.
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3003.升降舵的行程受升降舵动力控制组件的行程限制。
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2736.关于一般信息,参见发动机工作限制、指南和专用程序。
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2896.如果这一步不足以阻止泄漏,更换作动器。
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987.检查封严是否存在缺陷。
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3002.如果飞机停在斜坡上,请确保放好轮挡处。
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1876.Utilizing an airplane as intended by the manufacturer,combined with sound inspection and maintenance practices,forms the basis for assuring the airplane remains airworthy and safe to operate.
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861.底漆层厚度必须介于 0.05 毫米到 0.06 毫米之间。

A、 The coating thickness must be more than 0.05mm and less than 0.06mm.

B、 The thickness of the second coating layer must be 0.05mm and 0.06mm.

C、 The thickness of primer layer must be between 0.05 mm and 0.06 mm.

答案:C

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1568.The turbine clearance control sensor supplies the EEC with temperature data from the high pressure turbine shroud.

A. 涡轮间隙控制传感器提供高压涡轮的温度数据给 EEC。

B. 涡轮间隙控制传感器提供来自高压涡轮保护罩的 EEC 温度数据。

C. 涡轮间隙控制传感器提供高压涡轮保护罩的温度数据给 EEC。

https://www.shititong.cn/cha-kan/shiti/00059993-c61b-90ec-c057-47291d003a00.html
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1972.In the description of the airplane's Flight Controls,trimming arrangements shall be explained.

A. 描述飞机飞行控制系统时,应说明平衡设置。

B. 描述飞机飞行控制系统时,应对相应的配平装置进行描述。

C. 描述飞机飞行控制系统时,应解释配平安排。

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1279.Scratches can prevent the free movement of the piston in the sleeve.

A. 能防止自由运动的活塞在套筒中有划伤。

B. 刻痕能阻止活塞在套筒中的自由运动。

C. 刻痕能防止自由运动的活塞在套筒中。

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1539.When the entire storage area is full,new fault data,i.e.data for the current flight leg,will replace/overwrite the data for the oldest flight leg in the fault history.

A. 当整个存储区域已满时,新的故障数据和当前航班的数据,将替换/覆盖故障历史中最老的航班的数据。

B. 当整体存储区域已满时,新的故障数据,例如当前飞行段的数据,将替换/覆盖具有最早故障历史航班的数据。

C. 当整个存储区域已满时,新的故障数据,即当前飞行段的数据,将替换/覆盖故障历史中最早的飞行段的数据。

D. B.当整体存储区域已满时,新的故障数据,例如当前飞行段的数据,将替换/覆盖具有最早故障历史航班的数据。

E. C.当整个存储区域已满时,新的故障数据,即当前飞行段的数据,将替换/覆盖故障历史中最早的飞行段的数据。

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3003.升降舵的行程受升降舵动力控制组件的行程限制。

A. Elevator move is limited by the move of the elevator power control units.

B. Elevator trip is limited by the move of the elevator power control units.

C. Elevator travel is limited by the stroke of the elevator power control units.

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2736.关于一般信息,参见发动机工作限制、指南和专用程序。

A. Refer to the general information in addition to engine operation limits,guidelines and special procedures.

B. For general information,refer to engine operation limits,guidelines and special procedures.

C. Refer to engine operation limits,guidelines and special procedures besides general information.

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2896.如果这一步不足以阻止泄漏,更换作动器。

A. If this step can not stop the leakage,remove the actuator.

B. If this step is not enough to stop the leakage,change the motor.

C. If this step is not sufficient to stop the leakage,replace the actuator.

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987.检查封严是否存在缺陷。

A. Examine the seal for defects.

B. Check the abnormality of the sealant.

C. Inspect whether there are the defaults in the solvent.

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3002.如果飞机停在斜坡上,请确保放好轮挡处。

A. If the aircraft is parked on the ground,make sure that wheel chocks are placed.

B. If the aircraft is parked on the ground,make sure that wheel chocks are in position.

C. If the aircraft is parked on a slope,make sure that wheel chocks are in position.

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1876.Utilizing an airplane as intended by the manufacturer,combined with sound inspection and maintenance practices,forms the basis for assuring the airplane remains airworthy and safe to operate.

A. The basis for assuring an airplane remains airworthy and safe to operate is to combine the manufacturer's requirements with sound inspection and maintenance practices.

B. To ensure airworthiness and safe operation of an airplane,it is essential to follow themanufacturer's instructions in the utilization of airplane,and perform sound inspection and maintenance practices as well.

C. Airworthiness and safe operation are fundamental to aircraft utilization as required bythe manufacturer,so sound inspection and maintenance practices are carried out.

D. C.Airworthiness and safe operation are fundamental to aircraft utilization as required bythe manufacturer,so sound inspection and maintenance practices are carried out.

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