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题目内容

(

单选题

)

439.设置开关到打开位。

A、　Set the switch to on.

B、　Move the switch to on.

C、　Put the switch to on.

答案：A

噜啦啦噜啦噜啦啦啦啦啦啦1

576.IF THE WHEEL TEMPERATURE INCREASES TO MORETHAN 177 DEG., THE CORE
OF THE FUSIBLE PLUG MELTS AND THE TIRE DEFLATES.

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756.This Specification is designed to provide guidance for the
preparation of Handbooks for all types of general aviation airplanes
originally certificated at maximum takeoff weights of 12,500 pounds or
less (or 5,700 kg).

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234.调节罗盘系统 1 直到和罗盘系统 2 一致。

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571.Wherever the CAP is directed to a specific part or component, It is
implied that the Inspection will include observation and evaluation of
the surrounding area of parts and equipment.

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437.当使用该组件前,需先进行特定的测试程序。

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86.WHILE THE ENGINE CONTINUES TO TURN, ( ) FOR UNUSUAL NOISES.

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329.IF THE SYMPTOMS ( ) AGAIN, DO A SYSTEM TEST.

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659.Removal/Installation、 The removal/installation portion shall state
clearly the sequence of steps required to remove and reinstall a component
or unit, along with precautions to be observed.

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636.It is expected that the manufacturers of major components will
provide maintenance, troubleshooting, inspection and repair data in the
format of this specification.

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287.The CAP will address primary and secondary airframe components, and
primary and secondary systems to accomplish the stated objective of
continued airworthiness.

题目内容

(

单选题

)

手机预览

噜啦啦噜啦噜啦啦啦啦啦啦1

439.设置开关到打开位。

A、　Set the switch to on.

B、　Move the switch to on.

C、　Put the switch to on.

答案：A

相关题目

576.IF THE WHEEL TEMPERATURE INCREASES TO MORETHAN 177 DEG., THE CORE
OF THE FUSIBLE PLUG MELTS AND THE TIRE DEFLATES.

A. 　如果轮胎温度升高超过 177 度,插头熔化且轮胎放气。

B. 　如果轮胎温度升高超过 177 度,易熔塞和轮胎融化。

C. 　如果轮胎温度升高超过 177 度,易熔塞熔化且轮胎放气。

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A. 　本规范旨在为最初以 12500 磅或以下(或 5700 千克)最大起飞重量认证的所
有类型通用航空飞机提供手册编制指南。

B. 　本规范的制定是为手册编写提供规范性制导,用于 12500 磅(或 5700 千克)
或以下最大起飞重量的所有类型飞机。

C. 　本规范规定了以起始为 12500 磅或以下(或 5700 千克)最大起飞重量认证的
所有类型通用航空飞机提供手指编制指导。

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234.调节罗盘系统 1 直到和罗盘系统 2 一致。

A. 　Adjust compass system 1 until it agrees with compass system 2.

B. 　Synchronize compass system 1 with compass system 2.

C. 　Regulation compass system 1 until it agrees with compass system 2.

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571.Wherever the CAP is directed to a specific part or component, It is
implied that the Inspection will include observation and evaluation of
the surrounding area of parts and equipment.

A. 　因 CAP 是针对特定的零件或部件,可得知检查将包括对零件和设备周围区域
的观察和评估。

B. 　由于 CAP 是针对特定的零件或部件,可推测出检查将包括对零件和设备周围
区域的观察和评估。

C. 　只要 CAP 是针对特定的零件或部件,就意味着检查将包括对零件和设备周围
区域的观察和评估。

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437.当使用该组件前,需先进行特定的测试程序。

A. 　Before you accept the unit, do the functional test procedure.

B. 　Before you accept the unit, do the operational test procedure.

C. 　Before you accept the unit, do the specified test procedure.

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86.WHILE THE ENGINE CONTINUES TO TURN, ( ) FOR UNUSUAL NOISES.

A. 　LISTEN

B. 　FIND

C. 　LOOK

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329.IF THE SYMPTOMS ( ) AGAIN, DO A SYSTEM TEST.

A. 　OCCUR

B. 　FOUND

C. 　ARISE

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659.Removal/Installation、 The removal/installation portion shall state
clearly the sequence of steps required to remove and reinstall a component
or unit, along with precautions to be observed.

A. 　拆/装、拆卸/安装部分应清楚说明拆卸和安装部件或组件所需的步骤顺序,以
及遵循的预防事项。

B. 　拆装、拆卸/安装部分应清楚说明拆卸和重新安装部件或组件所需的步骤顺序,
以及要遵守的预防措施。

C. 　拆/装、拆卸/安装部分应清楚说明拆卸和重新安装部件或组件以及遵循的预防
事项所需的步骤顺序。

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636.It is expected that the manufacturers of major components will
provide maintenance, troubleshooting, inspection and repair data in the
format of this specification.

A. 　The manufacturers of major components must provide maintenance,
troubleshooting, inspection and repair data in the same layout of this
specification.

B. 　The manufacturers of major components is looking forward to gain
maintenance, troubleshooting, inspection and repair data with the same
form of this specification.

C. 　The manufacturers of major components should provide maintenance,
troubleshooting, inspection and repair data with same form of this
specification.

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287.The CAP will address primary and secondary airframe components, and
primary and secondary systems to accomplish the stated objective of
continued airworthiness.

A. 　The CAP will come up with main and subordinate airframe components,
and main and subordinate systems to achieve the stated objective of
continued airworthiness.

B. 　Primary and secondary airframe components, and Primary and secondary
systems are contained in CAP to complete the stated objective of continued
airworthiness.

C. 　To continue the stated objective of sustain airworthiness, major and
minor airframe components, and major and minor system are covered in CAP.

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