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题目内容
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单选题
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144.若觉得发动机过热,将电门设置在“关”位。

A、 if the engine appears to be heating, turn it off.

B、 if the engine appears to be overheating, turn it off.

C、 if you think the engine is too hot, turn the switch to “off”.

答案:C

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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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512.An important occurrence that can cause damage or have dangerous
results.
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133.If it is necessary( )the cable tension more, use the turnbuckle.
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299.BEFORE YOU ( )THE UNIT, DO THE SPECIFIED TEST PROCEDURE.
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592.On schematic diagrams such as electrical, where a large number of
items are listed, the items shall be presented in a logical order such
as the sequence of the arrangement of the items in the airplane or in
the schematic diagram.
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426.标准化将通过统一解释根据本规范编制的持续适航方案中包含的检查要求
来提高安全性。
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674.Motor the engine without ignition.
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181.本规范编写时遵循的构成规则与 FAA 编写规则时用到的大体相同。
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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.
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63.Flight Idle Power is the power required to run an engine,in flight,
at the lowest speed that will ensure satisfactory engine operation and
airplane handing characteristics.
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144.若觉得发动机过热,将电门设置在“关”位。

A、 if the engine appears to be heating, turn it off.

B、 if the engine appears to be overheating, turn it off.

C、 if you think the engine is too hot, turn the switch to “off”.

答案:C

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相关题目
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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512.An important occurrence that can cause damage or have dangerous
results.

A.  INCIDENT

B.  THING

C.  IN FACT

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133.If it is necessary( )the cable tension more, use the turnbuckle.

A.  to decrease

B.  decreased

C.  decreasing

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299.BEFORE YOU ( )THE UNIT, DO THE SPECIFIED TEST PROCEDURE.

A.  ACCEPTABLE

B.  ACCEPTANCE

C.  ACCEPT

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592.On schematic diagrams such as electrical, where a large number of
items are listed, the items shall be presented in a logical order such
as the sequence of the arrangement of the items in the airplane or in
the schematic diagram.

A.  如果列出了大量项目在电气示意图上,则项目应按逻辑顺序呈现,如飞机上
或示意图中项目的排列顺序。

B.  在电气示意图上,如果列出了大量项目,则项目应按逻辑顺序呈现,如飞机
上或示意图中项目的排列顺序。

C.  如果列出了大量项目,例如电气示意图上的项目应按逻辑顺序呈现,如飞机
上或示意图中项目的排列顺序。

https://www.shititong.cn/cha-kan/shiti/0005f3d5-4f16-9950-c0f5-18fb755e8802.html
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426.标准化将通过统一解释根据本规范编制的持续适航方案中包含的检查要求
来提高安全性。

A.  irworthiness Programs prepared to enhance safety.

B.  、Standardization will enhance safety though uniform interpretation of
inspection requirements contained in

C.  、Standardization will in accord with this Specification through uniform
interpretation of inspection requirements contained in Continuing

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674.Motor the engine without ignition.

A.  发动机的驱动马达没有点火。

B.  启动发动机但不点火。

C.  带转发动机但不点火。

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181.本规范编写时遵循的构成规则与 FAA 编写规则时用到的大体相同。

A.  When making this specification,the rules are generally refer to the
rules that used by FAA in making its rules .

B.  When making this specification,we use the exact identical construction
rules with FAA in making its specifications.

C.  The rules of construction followed in the preparation of this
specification are the same as generally used by the FAA in the preparation
of its rules.

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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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63.Flight Idle Power is the power required to run an engine,in flight,
at the lowest speed that will ensure satisfactory engine operation and
airplane handing characteristics.

A.   In flight,Flight Idle Power required for the engine to operate at slowly
speed is an important condition to ensure good engine operation and
airplane handing characteristics.

B.   Flight Idle Power is the power required for an engine to operate at
a minimum speed during flight to ensure satisfactory engine operation and
aircraft handing characteristics.

C.   In flight,good engine operation and aircraft handing characteristics
are guaranteed to provide the engine with Flight Idle Power needed to
operate at the lowest speed .

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