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民用航空器维修人员执照英语参考试题(个人)

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民用航空器维修人员执照英语参考试题(个人)

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校装包括设置钢索张力，调节飞控舵面的行程限位和设置行程止动点。

A、 Setting cable tension, flight control surfaces travel limits and stops are the main tasks of rigging.

B、 Cable tension set, flight controls travel limits adjustment and travel stops set are the rigging procedures.

C、 Rigging involves setting cable tension, adjusting travel limits of flight controls, and setting travel stops.

答案：C

民用航空器维修人员执照英语参考试题(个人)

Do the calibration of the resistance of the runway light connection.

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Recommendations for ATC holding operation in icing conditions for up to 45 minutes shall provided.

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In the description of the airplane＇s Heating, Ventilating, Defrosting and Air-Conditioning Systems, how to get maximum benefit using the controls provided shall be explained.

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不锈钢接触镁、铝或镉金属时会导致它们腐蚀。

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Examine the removed parts for damage.

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确保溶剂没在发动机尾喷管附近。

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将所有装有不同金属螺套或有较深盲孔的金属零件在烤箱中干燥至少一小时，烤箱温度为225到275华氏度(107 to 135°C)。

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These ALIs are mandatory and cannot be changed or deleted without the approval of the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency.

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Floor beam at body station 360 has moderate corrosion 2 inches in length and 1 inch in diameter.

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The thickness of the strap should be between 1 and 1.2 times the thickness of the initial stringer pad.

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民用航空器维修人员执照英语参考试题(个人)

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民用航空器维修人员执照英语参考试题(个人)

校装包括设置钢索张力，调节飞控舵面的行程限位和设置行程止动点。

A、 Setting cable tension, flight control surfaces travel limits and stops are the main tasks of rigging.

B、 Cable tension set, flight controls travel limits adjustment and travel stops set are the rigging procedures.

C、 Rigging involves setting cable tension, adjusting travel limits of flight controls, and setting travel stops.

答案：C

相关题目

Do the calibration of the resistance of the runway light connection.

A. 测量跑道灯连接的电阻。

B. 校准跑道灯连接的电阻。

C. 复核跑道灯连接的电阻。

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Recommendations for ATC holding operation in icing conditions for up to 45 minutes shall provided.

A. 应提供结冰条件下最多保持空中等待程序运行45分钟的建议。

B. 建议在结冰条件下保持空中交通管制运行45分钟。

C. 应提供在结冰条件下ATC保持运行长达45分钟的建议。

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In the description of the airplane＇s Heating, Ventilating, Defrosting and Air-Conditioning Systems, how to get maximum benefit using the controls provided shall be explained.

A. 描述飞机加热、通风、除霜和空调系统时，应说明如何使用所提供的操纵系统获得最大效益。

B. 描述飞机加热、通风、除霜和空调系统时，应说明如何使用所提供的控制装置使这些系统能够获得最大效益。

C. 描述飞机加热、通风、除霜和空调系统时，应说明如何获得最大收益以便使用所提供的控制装置。

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不锈钢接触镁、铝或镉金属时会导致它们腐蚀。

A. CRES causes magnesium, aluminum, or cadmium to corrode when it touches these metals.

B. Stainless steel corrodes once touching magnesium, aluminum, or chromium metals.

C. Magnesium, aluminum, or chromium metals shall be protected from the corrosion caused by CRES.

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Examine the removed parts for damage.

A. 检查并拆下损坏的零件。

B. 检查拆下的零件是否损坏。

C. 检查损坏的零件，判断是否要拆下。

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确保溶剂没在发动机尾喷管附近。

A. Make sure that chemical compound are not near the engine nozzle.

B. Make sure that solvents are not near the engine exhaust.

C. Make sure that there＇s no isopropyl alcohol near the engine exhaust port.

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将所有装有不同金属螺套或有较深盲孔的金属零件在烤箱中干燥至少一小时，烤箱温度为225到275华氏度(107 to 135°C)。

A. Dry all metal parts that have different metal inserts or deep blind holes in an oven at 225 to 275°F (107 to 135°C) for a minimum of one hour.

B. Put all different metal inserts or deep blind holes metal parts in an oven at 225 to 275°F (107 to 135°C) for a maximum of one hour.

C. All metal parts that have different metal inserts or deep blind holes are dry in an oven of 225 to 275°F (107 to 135°C) for a minimum of one hour.

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These ALIs are mandatory and cannot be changed or deleted without the approval of the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency.

A. 这些ALIs 是强制性的，未经负责飞机型号证书的FAA 办公室或适用的监管机构的批准，不能更改或删除。

B. 这些ALIs 是指令性的，未经FAA办公室批准不得更改或删除。FAA办公室负责飞机型号证书，或发布适用的管理规章。

C. 这些ALIs 是非常必要的，任何更改或删除必须获得FAA办公室批准，或者其他可以颁发飞机型号证书的监管机构的批准。

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Floor beam at body station 360 has moderate corrosion 2 inches in length and 1 inch in diameter.

A. 机身站位360处的地板梁有低度腐蚀（长2英寸，直径1英寸）。

B. 机身站位360处的地板梁有重度腐蚀（长2英寸，半径1英寸）。

C. 机身站位360处的地板梁有中度腐蚀（长2英寸，直径1英寸）。

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The thickness of the strap should be between 1 and 1.2 times the thickness of the initial stringer pad.

A. 衬板的厚度应该是初始翼梁衬垫的厚度的1-1.2倍。

B. 加强条的厚度乘以1-1.2就得到初始长桁衬垫的厚度。