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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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以下首字母缩略词在本节中可互换使用,它们分别代表同一系统和设备。

A、 The following synonyms are used interchangeably throughout this section and they are the sample of one system and device respectively.

B、 The following antonyms are used interchangeably throughout this section and they present the same system and device partly.

C、 The following acronyms are used interchangeably throughout this section and they represent the same system and device respectively.

答案:C

民用航空器维修人员执照英语参考试题(个人)
如果这一步不足以阻止泄漏,更换作动器。
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副翼位于每侧机翼后缘外侧。
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Two sensors are on the top of the aft lock link.
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确保指示不超过400节。
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The bottom mark on the board is red.
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Measure the depth of the dent with a straightedge and feeler gauges.
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The alphanumeric display shows only voltage and frequency when you select one of these pushbutton.
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INSPECTION PROCEDURE sets forth the inspection procedure(s) to be utilized, such as magnetic particle, visual, etc, and may reference another document for the actual procedure, such as a nondestructive testing manual.
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Overhaul of any or all components in this chapter must be accomplished in a qualified shop in accordance with data supplied by the component manufacturer.
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In the description of the airplane's Engine, the engine controls shall be described including: 1.Throttle or power control 2.Propeller control 3.Mixture control 4.Cooling controls 5.Turbocharger controls 6.Friction lock
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民用航空器维修人员执照英语参考试题(个人)

以下首字母缩略词在本节中可互换使用,它们分别代表同一系统和设备。

A、 The following synonyms are used interchangeably throughout this section and they are the sample of one system and device respectively.

B、 The following antonyms are used interchangeably throughout this section and they present the same system and device partly.

C、 The following acronyms are used interchangeably throughout this section and they represent the same system and device respectively.

答案:C

民用航空器维修人员执照英语参考试题(个人)
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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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副翼位于每侧机翼后缘外侧。

A. The ailerons are located to the outside rare edge of each wing.

B. The spoilers are located on the outside rare edge of each wing.

C. The ailerons are located on the outboard trailing edge of each wing.

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Two sensors are on the top of the aft lock link.

A. 两个电感器在后锁连杆上方工作。

B. 两个传感器位于后锁连杆的顶部。

C. 两个探测器在杆锁定位的后上方。

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确保指示不超过400节。

A. Make sure that the scale is not more than 400 knots.

B. Make sure that the indication is not more than 400 knots.

C. Make sure that the indication is not more than 400 miles.

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The bottom mark on the board is red.

A. The color of the bottom mark on the plate is amber.

B. You can see the red bottom mark on the board.

C. There is no color of the bottom mark on the board.

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Measure the depth of the dent with a straightedge and feeler gauges.

A. 用专用尺子确定凹坑的长度。

B. 用直尺和塞尺测量凹坑的深度。

C. 用角尺和直尺测量裂纹的深度。

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The alphanumeric display shows only voltage and frequency when you select one of these pushbutton.

A. 当你选择这些按钮中的其一时,数字字母显示只出现电压和频率。

B. 当你选择这些按钮中的其一时,模拟数字显示只出现电压和频率。

C. 当你选择这些开关中的其一时,模拟数字显示只出现电压和频率。

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INSPECTION PROCEDURE sets forth the inspection procedure(s) to be utilized, such as magnetic particle, visual, etc, and may reference another document for the actual procedure, such as a nondestructive testing manual.

A. “检查程序”用于列出要使用的检查程序,如磁性粒子、目视检查等,也可参考其他文件(如《无损检测手册》)中包含的程序。

B. “检查程序”用于规定要使用的检查程序,如磁粉检查、目视检查等,也可指向其他文件(如《无损检测手册》)中包含的程序。

C. “检查程序”用于规定要使用的检查程序,如磁粉检查、目视检查等,并可寻找另一个文件的实际程序,如无损检测手册。

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Overhaul of any or all components in this chapter must be accomplished in a qualified shop in accordance with data supplied by the component manufacturer.

A. With the aid of the component manufacturer, all components in this chapter can be overhauled in any workshops with different qualifications.

B. Without the data supplied by the component manufacturer, it is possible for the most qualified shop to overhaul any components included in this chapter.

C. You must overhaul any or all components in this chapter in an eligible shop on the basis of data provided by the component manufacturer.

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In the description of the airplane's Engine, the engine controls shall be described including: 1.Throttle or power control 2.Propeller control 3.Mixture control 4.Cooling controls 5.Turbocharger controls 6.Friction lock

A. 描述飞机发动机时,应描述的发动机控制包括: 1.油门或功率控制 2.螺旋桨控制 3.混合控制 4.冷冻控制 5.涡轮增压器控制 6.摩擦止动装置

B. 描述飞机发动机时,应描述的发动机控制器包括: 1.油门杆或功率控制杆 2.螺旋桨控制 3.油气混合比控制 4.冷却控制器 5.涡轮增压器控制器 6.摩擦止动装置

C. 描述飞机发动机时,应描述的发动机控制包括: 1.油门或电源控制 2.螺旋桨控制 3.油气混合比控制 4.冷却控制 5.涡轮增压器控制 6.摩擦止动装置

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