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1145. The surface contour of a repair in a 3 inches radius from the centerline of a static port does not have an error of more than 0007 inch

A、 距离皮托管中心线半径3英寸的修复表面轮廓外形,误差不应大于0.007英寸。

B、 距离静压盘中心线3英寸半径上的修复表面等高线,误差不应大于0.007英寸。

C、 静压孔中心线3英寸半径内的修复表面轮廓,误差不应大于0.007英寸。

答案:C

设备系统操作理论翻译
2774. 第一步应该始终是工作准备,最后一步应该是收尾或清理。
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1877. The section of the engine through which the air enters the compressor section Includes items such as guide vanes, shrouds, cases, etc
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2703. To prevent damage to the engine, immediately install protective covers on all openings
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457. 用03-002滑油润滑新的封严组件。
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828. However, the title and applicable airplane or airplane series designation will be prominently shown on the cover or spine of the handbook
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1696. Where diagrams are complex by virtue of their automatic features or interrelated controls, such characteristics shall be covered by means of explanatory text in the diagram or accompanying text instead of by schematic representation
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1788. The normal pitch control law is basically the closed loop control of the load factor, and includes flight envelope protections
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1221. 接近1号液压系统的储压器。
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2368. 要指出的是,在对飞机进行任何改装之前,都应该先与联邦航空局联系,以确保飞机的适航性不受影响。
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470. 根据制造商的选择,静压系统的描述和讨论可以结合第749段的皮托管压力系统。
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设备系统操作理论翻译
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设备系统操作理论翻译

1145. The surface contour of a repair in a 3 inches radius from the centerline of a static port does not have an error of more than 0007 inch

A、 距离皮托管中心线半径3英寸的修复表面轮廓外形,误差不应大于0.007英寸。

B、 距离静压盘中心线3英寸半径上的修复表面等高线,误差不应大于0.007英寸。

C、 静压孔中心线3英寸半径内的修复表面轮廓,误差不应大于0.007英寸。

答案:C

设备系统操作理论翻译
相关题目
2774. 第一步应该始终是工作准备,最后一步应该是收尾或清理。

A. The first step should always be Job Set-Up, and the last should be finish or Cleaning.

B. The first step is always Job prepare, and the last should be end or Clean-Up.

C. The first step should always be Job Set-Up, and the last should be Close-Up or Clean-Up.

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1877. The section of the engine through which the air enters the compressor section Includes items such as guide vanes, shrouds, cases, etc

A. 空气通过发动机的导流叶片、支撑罩、外壳等部件进入压气机。

B. 空气通过发动机进入压气机的部分。包括导流叶片、支撑罩、外壳等。

C. 空气通过导流叶片、支撑罩、外壳等部件进入压气机。

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2703. To prevent damage to the engine, immediately install protective covers on all openings

A. 为防止损坏发动机,立即打开所有安装的防护罩。

B. 为防止损坏发动机,稍候装上所有开口的防护罩。

C. 为防止损坏发动机,立即在所有开口上安装防护罩。

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457. 用03-002滑油润滑新的封严组件。

A. Seal the new sealing assemblies with 03-002 oil.

B. Lubricate the new components with 03-002 lube.

C. Lubricate the new sealing assemblies with 03-002 oil.

https://www.shititong.cn/cha-kan/shiti/0009ffa1-9bf9-320e-c0b8-ef8d402da900.html
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828. However, the title and applicable airplane or airplane series designation will be prominently shown on the cover or spine of the handbook

A. 但是,标题和适用的飞机或飞机系列名称要在手册的封面或书背上加粗显示

B. 但是,标题和适用的飞机或飞机系列名称要在手册的封面或书背上突出显示

C. 但是,标题和适用的飞机或飞机系列名称要在手册的封面或书脊上突出显示

https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b42-0e0c-c0b8-ef8d402da900.html
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1696. Where diagrams are complex by virtue of their automatic features or interrelated controls, such characteristics shall be covered by means of explanatory text in the diagram or accompanying text instead of by schematic representation

A. 当图表由于其自动功能或不同类别的控件而变得复杂时,这些特征应通过图表中的解释性文字或随附文字来代替,而不是通过示意图表示。

B. 当图表由于其自动功能或相关控件而变得复杂时,这些特征应通过图表中的解释性文字或随附文字来代替,而不是通过符号来表示。

C. 当图表由于其自动功能或相关控件而变得复杂时,这些特征应通过图表中的解释性文字或随附文字来代替,而不是通过示意图表示。

https://www.shititong.cn/cha-kan/shiti/0009ffad-f67e-1e4f-c0b8-ef8d402da900.html
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1788. The normal pitch control law is basically the closed loop control of the load factor, and includes flight envelope protections

A. 正常俯仰控制法则基本上是负载系数的闭环控制,包括飞行发展保护。

B. 正常俯仰控制法基本上是负载厂家的闭环控制,包括飞行包线保护。

C. 正常俯仰控制法则基本上是负载系数的闭环控制,包括飞行包线保护。

https://www.shititong.cn/cha-kan/shiti/0009ffad-f67f-491d-c0b8-ef8d402da900.html
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1221. 接近1号液压系统的储压器。

A. Get access to the accumulator for the no.1 hydraulic system.

B. Get access to the reservoir for the no.1 hydraulic system.

C. Get access to the accumulator for the no.1 fluid system.

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2368. 要指出的是,在对飞机进行任何改装之前,都应该先与联邦航空局联系,以确保飞机的适航性不受影响。

A. Point out that the FAA should be informed after any modifications on airplane to ensure that the airworthiness of the airplane is not effected.

B. Point out that any modifications on airplane may be informed to FAA to confirm the airworthiness of the airplane.

C. Point out that the FAA should be contacted prior to any alterations on airplane to ensure that the airworthiness of the airplane is not violated.

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470. 根据制造商的选择,静压系统的描述和讨论可以结合第749段的皮托管压力系统。

A. At the manufacturer's option, static pressure systems description and discussion may be combined with Paragraph 7.49, Pitot Pressure Systems.

B. The manufacturer could combine the description and discussion of the dynamic pressure systems in Paragraph 7.49, Pitot Pressure Systems.

C. The manufacturer decides to insert static pressure systems description and discussion into Paragraph 7.49, Pitot Pressure Systems.

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