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题目内容

(

单选题

)

81.若要改变这个修理程序,则要得到设计主管部门的批准。

A、　If you change this repair procedure,get approval of the Design Authority .

B、　Any alteration to this repair procedure must have approval of the Design Authority.

C、　To change this repair procedure, get agree of the Design Authority .

答案：A

噜啦啦噜啦噜啦啦啦啦啦啦1

153.The data, power, or energy put into equipment or a system.

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527.Hook the towing arm up to the nose gear.

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398.The listed model or components and listed serials/units are to be
cumulative for all inspections in the Continuing Airworthiness Program

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530.NOTE、 This system does not supersede the normal channels of
communication for items not covered by the CAP.

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620.If the airplane has a built-in auxiliary power unit, describe it and
explain how it fits in with the electrical system.

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479.The exhaust gas temperature indicator, on piston engine powered
airplanes, is the instrument used to identify the lean fuel flow mixtures
for various power settings.

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166.If the manual is loose-leaf,each page should contain the data and
effective revision data when revised,or otherwise be identified as to
revision status.

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328.The servicing required on units as the result of the accomplishment
of any other maintenance practice.

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189.MOVE THE ENGINE THROTTLE BACK TO 60%RPM.

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89.The pump( ) operate because the shaft( )broken. 轴的损坏导致泵不能
正常运行。

题目内容

(

单选题

)

手机预览

噜啦啦噜啦噜啦啦啦啦啦啦1

81.若要改变这个修理程序,则要得到设计主管部门的批准。

A、　If you change this repair procedure,get approval of the Design Authority .

B、　Any alteration to this repair procedure must have approval of the Design Authority.

C、　To change this repair procedure, get agree of the Design Authority .

答案：A

相关题目

153.The data, power, or energy put into equipment or a system.

A. 　INNER

B. 　OUTPUT

C. 　INPUT

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527.Hook the towing arm up to the nose gear.

A. 　Hinge the towing arm up to the nose gear.

B. 　Connect the towing arm to the nose gear.

C. 　Fix the towing arm up to the nose gear.

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398.The listed model or components and listed serials/units are to be
cumulative for all inspections in the Continuing Airworthiness Program

A. 　在持续适航方案检查文件中,列出的型号或部件和列出的系列号/组件的所有
检查应采取累计方式。这将允许用户通过查看一个清单来识别受影响的飞机,而
不是必须去查看每个单独持续适航方案检查的合理性。

B. 　在持续适航方案检查文件中,列出的型号或部件和列出的系列号/组件的所有
检查应采取累计方式。这将允许用户通过查看一个清单来识别受影响的飞机,而
不是必须去查看每个单独持续适航方案检查的适用性。

C. 　在持续适航方案检查文件中,列出的型号或部件和列出的系列号/组件的所有
检查应采取累计方式。这将允许用户通过查看一个清单来识别受影响的飞机,而
不是必须去查看每个单独持续适航方案检查的有效性。

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530.NOTE、 This system does not supersede the normal channels of
communication for items not covered by the CAP.

A. 　注意、本系统不能超出 CAP 未涵盖项目的正常通信渠道。

B. 　注意、本系统不取代 CAP 未涵盖项目的正常通信渠道。

C. 　注意、本系统不能紧随 CAP 未涵盖项目的正常通信渠道。

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620.If the airplane has a built-in auxiliary power unit, describe it and
explain how it fits in with the electrical system.

A. 　如果飞机有机载的辅助动力装置,请对其进行描述并说明其如何与电气系统
配合使用。

B. 　如果飞机有一个附加的辅助电源组件,描述该装置并解释它是如何对接电气
系统的。

C. 　如果飞机有一个内置的辅助动力装置,描述该装置并解释它是如何装配到电
气系统的。

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479.The exhaust gas temperature indicator, on piston engine powered
airplanes, is the instrument used to identify the lean fuel flow mixtures
for various power settings.

A. 　在活塞发动机驱动的飞机上,排气温度指示器用于识别各种功率设置下的油
气比。

B. 　在活塞发动机驱动的飞机上,排气温度指示器用于设置各种功率设置下的油
和空气的混合比。

C. 　在动力活塞驱动的飞机发动机上,排气温度指针用于识别最大功率设置下的
油气比。

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166.If the manual is loose-leaf,each page should contain the data and
effective revision data when revised,or otherwise be identified as to
revision status.

A. 　若为松散页,则每一页应注明修改日期和生效日期,或以其他方式表明修订
方式

B. 　若为活页,则每一页应注明修改日期和生效日期,或以其他方式表明修订方
式

C. 　若为固定页,则每一页应注明修改日期和生效日期,或以其他方式表明修订
方式

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328.The servicing required on units as the result of the accomplishment
of any other maintenance practice.

A. 　由于其他维护工作需要对设备进行维修。

B. 　由于对设备进行维修需要先完成其他维护工作。

C. 　由于完成其他维护工作而需要对设备进行的维修。

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189.MOVE THE ENGINE THROTTLE BACK TO 60%RPM.

A. 　将发动机油门杆前推至 60%RPM。

B. 　将发动机油门杆稳定在 60%RPM。