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题目内容

(

单选题

)

301.Individual wire identification codes are established to assist in
tracing circuitry (Figure 5).

A、　建立单独的导线标识码,以组建追踪电路(如图 5)

B、　建立单独的导线标识码,以协助追踪电路(如图 5)

C、　建立单独的导线标识码,以装配追踪电路(如图 5)

答案：B

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388.Do an inspection for damage caused by corrosion.

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554.Remove all sealant that is around the hole.

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29.Basic control and operation information describing how the airplane
components are controlled and how they operate,including any special
procedures, and limitations that apply.

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425.THE TEMPERATURE BULB ( ) THE OUTSIDE AIR TEMPERATURE.

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739.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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333.若要改变这个修理程序,则要得到设计主管部门的批准。

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136.Let the pressure become stable after each turn of the adjustment
screw.

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480.( ) THAT THE DUCT IS CORRECTLY ATTACHED TO THE FILTER.

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616.The diagram shall be arranged so that the flow of the system can be
traced with a minimum of effort.

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104.This Aviation Manufacturers Association as guidance for airplane, engine and component
manufacturers in preparing Continuing Airworthiness Program Inspection

题目内容

(

单选题

)

手机预览

噜啦啦噜啦噜啦啦啦啦啦啦1

301.Individual wire identification codes are established to assist in
tracing circuitry (Figure 5).

A、　建立单独的导线标识码,以组建追踪电路(如图 5)

B、　建立单独的导线标识码,以协助追踪电路(如图 5)

C、　建立单独的导线标识码,以装配追踪电路(如图 5)

答案：B

相关题目

388.Do an inspection for damage caused by corrosion.

A. 　做腐蚀检查。

B. 　做损害检查。

C. 　检查由腐蚀造成的损伤。

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554.Remove all sealant that is around the hole.

A. 　移动所有孔周围的密封胶。

B. 　清除孔周围的所有密封胶。

C. 　检查所有密封胶圈绕着孔。

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29.Basic control and operation information describing how the airplane
components are controlled and how they operate,including any special
procedures, and limitations that apply.

A. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到一些特殊程序
和飞行控制信息适用的限制。

B. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到许多特殊程序
和飞机部件适用的限制。

C. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到所有特殊程序
和飞机部件适用的限制。

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425.THE TEMPERATURE BULB ( ) THE OUTSIDE AIR TEMPERATURE.

A. 　GETS

B. 　SENSES

C. 　OBTAINS

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739.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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333.若要改变这个修理程序,则要得到设计主管部门的批准。

A. 　uthority.

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

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

D. 　esign Authority .

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136.Let the pressure become stable after each turn of the adjustment
screw.

A. 　调节螺钉转动后,使压力平稳。

B. 　每次转动调节螺钉后,使压力稳定。

C. 　只要转动调整螺钉后,使压力稳定。

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480.( ) THAT THE DUCT IS CORRECTLY ATTACHED TO THE FILTER.

A. 　ASSURE

B. 　MAKE SURE

C. 　ASCERTAIN

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616.The diagram shall be arranged so that the flow of the system can be
traced with a minimum of effort.

A. 　图表的布置应使系统的流程能够最便于进行追踪。

B. 　图表的设置应使系统的流程能以最省事的流程进行查找。

C. 　图文的设计应使系统的流程能够最便于更改。

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104.This Aviation Manufacturers Association as guidance for airplane, engine and component
manufacturers in preparing Continuing Airworthiness Program Inspection

A. 　viation Regulations may prepare CAPs

B. 　General Aviation Manufacturers Association Built up this Specification
to guide the airplane, engine and component manufacturers to prepare

C. 　APs

D. 　ocuments(which may also be
called Continuing Airworthiness Programs or CAPs). All types of general
aviation airplanes and components certified under the applicable Federal

F. 　ederal

I. 　nspection Documents(which may also be
called Continuing Airworthiness Programs or CAPs). All types of general
aviation airplanes and components certified under the applicable Federal

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301.Individual wire identification codes are established to assist intracing circuitry (Figure 5).

301.Individual wire identification codes are established to assist in
tracing circuitry (Figure 5).