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1087、此系统用于伸出或收回起落架

A、  This system is used to expand and return the landing gear

B、  This system is used to extend and retract the landing gear.

C、  This system is used to extract and retract the landing gear.

答案:B

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1161、To remove the cover assembly (9. first remove the four screws (10)
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1055 、 CAP supplements the airplane’s maintenance manual ( )
which is the primary document containing the procedures for the continuing airworthiness of the airplane
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305、 单词列表只突出显示主要更改。
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275、Fill the space between the patch and the adjacent structure with sealant.
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497 、 Utilizing an airplane as intended by the manufacturer, combined with sound inspection and
maintenance practices/ , forms the/ basis for assuring the airplane remains airworthy and safe to operate.
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378、Make sure that the doors are closed during the pressurization test.
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1186、Do not use solvents that contain chlorine to clean parts with a Rilsan coating.
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340 易碎接头是常闭活门。
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487、The difference between the two dimensions must not be more than 0.10mm. 两个尺寸的差值不得超过 0.10mm。
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461、The normal pitch control law is basically the closed loop control of the load factor, and includes flight
envelope protections.
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1087、此系统用于伸出或收回起落架

A、  This system is used to expand and return the landing gear

B、  This system is used to extend and retract the landing gear.

C、  This system is used to extract and retract the landing gear.

答案:B

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相关题目
1161、To remove the cover assembly (9. first remove the four screws (10)

A.  要先安装螺钉(10),才能安装盖组件(9

B.  要拆下盖组件(9),首先要拆下这四个螺钉(10)

C.  要拆下螺母(9),首先要拆下这四个螺栓(10

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1055 、 CAP supplements the airplane’s maintenance manual ( )
which is the primary document containing the procedures for the continuing airworthiness of the airplane

A.  irworthiness). The CAP is the primary document containing the aircraft's continuous airworthiness procedures.

B.  、 The airplane's maintenance manual (or Instructions for

C.  、 CAP supplements the airplane's maintenance manual (or Instructions for Continuing Airworthiness). The supplements are Ethe major document and involve in the procedures for the continuing airworthiness of the airplane

E.  the major document and involve in the procedures for the continuing airworthiness of the airplane

I.  nstructions for Continuing Airworthiness). The supplements are Ethe major document and involve in the procedures for the continuing airworthiness of the airplane

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305、 单词列表只突出显示主要更改。

A.   The word list only shows major changes.

B.   The word list only shows minor changes.

C.   Only major changes are highlighted in the word list.

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275、Fill the space between the patch and the adjacent structure with sealant.

A.  用密封剂填充补片及相邻结构之间的缝隙。

B.  用密封剂填充补片的缝隙,并粘接相邻结构。

C.  在附近的密封结构和补片之间留出空隙。

https://www.shititong.cn/cha-kan/shiti/0005f400-4315-9ae0-c0f5-18fb755e8802.html
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497 、 Utilizing an airplane as intended by the manufacturer, combined with sound inspection and
maintenance practices/ , forms the/ basis for assuring the airplane remains airworthy and safe to operate.

A.  按照制造商的计划要求使用飞机,结合例行检查和维护实践,从而构成飞机保持适航和安全运行的基础。

B.  按照制造商的要求使用飞机,结合合理的检查和维修实践,形成了确保飞机保持适航和安全运行的基础。

C.  由制造商决定飞机的使用,结合良好的检查和维修实践,以构成飞机保持适航性和安全运行的基础。

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378、Make sure that the doors are closed during the pressurization test.

A.  在释压测试期间,不得开启舱门。

B.  在增压测式期间,确保舱门关闭。

C.  进行水压测试时,确保舱门关闭。

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1186、Do not use solvents that contain chlorine to clean parts with a Rilsan coating.

A.  不要让清洁剂接触带有瑞尔森(Rilsan)涂层的零件

B.  不要使用含氯的溶剂清洁带有瑞尔森(Rilsan)涂层的零件。

C.  不可以使用含氯的瑞尔森(Rilsan)溶液清洁带有涂层的零件。

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340 易碎接头是常闭活门。

A.   The fragile connector is usually closed. 易碎连接器通常是闭合的

B.   The quick-break switch is normally in the off position.

C.   The frangible fitting is a normally closed valve.

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487、The difference between the two dimensions must not be more than 0.10mm. 两个尺寸的差值不得超过 0.10mm。

A.   The difference between the two sizes must be 0.10mm or less.

B.   The difference between ‘the two dimensions must exceed 0.10mm.

C.   The error between the two sizes must be less than 0.10mm.

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461、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。

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