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1960.This reporting system does not supersede the normal channels of communication for items not covered by the CAP.

A、这一报告系统并非用于取代《持续适航维修大纲(CAP)》未涵盖项目的常规沟通渠道。

B、这个系统并不取代正常的沟通渠道,进而处理《持续适航维修大纲(CAP)》不涉及的项目。

C、该报告系统不会阻碍《持续适航维修大纲(CAP)》未涵盖项目的正常交流。

D、 C.该报告系统不会阻碍《持续适航维修大纲(CAP)》未涵盖项目的正常交流。

答案：A

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1816.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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2802.Airplane certification conditions include one engine becoming inoperative and windmilling (or,in airplanes with autofeathering devices,feathered),not more than a 5° bank toward the operative engine,takeoff power on the operative engine,landing gear up,flaps in the takeoff position,and the most critical C.G.

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1751.Procedures shall be prepared in reference number sequence within each chapter with proper major and minor subject heads,without the necessity of each procedure starting at the top of a new page.

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2148.如果杆端轴承的径向磨损大于 0.010 英寸,在接下来的 10 个飞行循环或 25 个飞行小时内(先到为准)将其报废。

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385.The flight crew can use the flight director commands to control the attitude of the airplane.

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1373.The title shall be Airplane Maintenance Manual if all technical data is included.

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101.Use the manual procedure if it is not possible to use the automatic control.

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2957.制造商可以省略对该产品不适用的系统/章节,或者在可行的情况下合并系统/章节。

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1841.针对飞机类别适合的机动飞行,应提供以下信息:(a)获准的机动飞行以及合适的进入速度的相关信息;(b)未获授权的机动飞行的相关信息;(c)已获准或未获准或不适合进行螺旋训练的相关信息。

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581.Hydraulic fluid can cause corrosion.

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1960.This reporting system does not supersede the normal channels of communication for items not covered by the CAP.

A、这一报告系统并非用于取代《持续适航维修大纲(CAP)》未涵盖项目的常规沟通渠道。

B、这个系统并不取代正常的沟通渠道,进而处理《持续适航维修大纲(CAP)》不涉及的项目。

C、该报告系统不会阻碍《持续适航维修大纲(CAP)》未涵盖项目的正常交流。

D、 C.该报告系统不会阻碍《持续适航维修大纲(CAP)》未涵盖项目的正常交流。

答案：A

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1816.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.

A. 本规范准备过程中所遵循的(语法)结构规则与 FAA 在其规章准备过程中所使用的专用规则相同。

B. 在编写本规范时遵循的(语法)结构规则与 FAA 在编写其规章时通常使用的规则相同。

C. (语法)结构规则遵循该规范的编写,该规范和 FAA 在编写其规章时通常使用的规则相同。

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A. 飞机审定条件包括:一台发动机不工作并处于风车状态(或对于安装自动顺桨装置的飞机,已顺桨),朝向工作发动机一侧倾斜不超过 5 度,工作发动机处于起飞功率,起落架收上,襟翼在起飞位置,以及最临界重心位置。

B. 飞机的审定条件包括:一个发动机停车,有风动(或在有自动羽化装置的飞机上,已羽化)朝向工作发动机的倾斜度小于 5 度,起落架升起,襟翼处于起飞状态,以及最不利的重量。

C. 飞机的审定条件包括:一个发动机停止工作,有风动(已在飞机上调为自动顺桨模式)朝向工作发动机的倾斜度大于 5 度,起落架升起,襟翼处于起飞状态,以及重心处于临界位置。

D. C.飞机的审定条件包括:一个发动机停止工作,有风动(已在飞机上调为自动顺桨模式)朝向工作发动机的倾斜度大于 5 度,起落架升起,襟翼处于起飞状态,以及重心处于临界

E. C.飞机的审定条件包括:一个发动机停止工作,有风动(已在飞机上调为自动顺桨模式)朝向工作发动机的倾斜度大于 5 度,起落架升起,襟翼处于起飞状态,以及重心处于临界位置。

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1751.Procedures shall be prepared in reference number sequence within each chapter with proper major and minor subject heads,without the necessity of each procedure starting at the top of a new page.

A. 程序应在每章内按编号顺序进行准备,并有适当的主次科目标题,无需从新的页面开始。

B. 程序应在每章内按照主次标题和参考号的形式进行编写,不需要从新的页面的开头开始。

C. 程序应在每章内按参考编号顺序编制,并有适当的主、副标题,而无需从新页的顶部开始。

D. C.程序应在每章内按参考编号顺序编制,并有适当的主、副标题,而无需从新页的顶部开始。

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2148.如果杆端轴承的径向磨损大于 0.010 英寸,在接下来的 10 个飞行循环或 25 个飞行小时内(先到为准)将其报废。

A. After 10 flight cycles or 25 flight hours,which comes first,the rod end bearing shall be discarded if its wear is greater than 0.010 inch of diameter.

B. If the rod end bearing wear is greater than 0.010 inch in radial play,reject it within next 10 flight cycles or 25 flight hours whichever comes first.

C. Destroy the rod end bearing during 10 flight cycles or 25 flight hours when its wear is more than 0.010 inch of its radius,whichever comes first.

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385.The flight crew can use the flight director commands to control the attitude of the airplane.

A. 机组能用飞行指令需求来控制飞机的姿态。

B. 机组能用飞行指引指令来控制飞机的高度。

C. 机组能用飞行指引指令来控制飞机的姿态。

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1373.The title shall be Airplane Maintenance Manual if all technical data is included.

A. 如果包含所有技术数据,则标题应为飞机维修手册。

B. 标题应为飞机维修手册,则所有数据包含在其中。

C. 飞机维修手册的标题应该包含所有技术数据。

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101.Use the manual procedure if it is not possible to use the automatic control.

A. 如果无法使用自动控制,请使用人工控制程序。

B. 用手动程序代替自动控制程序完成操作。

C. 尽可能使用手动程序取代自动控制。

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2957.制造商可以省略对该产品不适用的系统/章节,或者在可行的情况下合并系统/章节。

A. Systems/Chapters that are not applicable to the product by the manufacturers may be omitted or,where possible,omitted.

B. Manufacturers may omit Systems/Chapters that do not apply to the product,or omit such Systems/Chapters where feasible.

C. Manufacturers may omit System/Chapters that are not applicable to the product or combine System/Chapters where it is feasible.

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A. The following information on maneuvers appropriate to the Airplane Category shall be given:(a) A Statement of Authorized Maneuvers and Appropriate Entry Speeds (b) A Statement of Unauthorized Maneuvers (c) A Statement that the airplane is Approved for Spins,Unapproved for Spins,or is characteristically incapable of spinning.

B. The following information should be provided to the maneuver flight as appropriate: (a) A Statement of Entry Speed for Authorized Maneuvers (b) A Statement of Unauthorized Maneuvers(c) A Statement that aircraft is Unapproved or not suitable for Spinning.

C. The following appropriate information should be provided to the aircraft maneuvers: (a) A Statement of Appropriate Entry Speed for maneuvers flight (b) A Statement of Unauthorized maneuvers (c) A Statement that aircraft has been unapproved for Spins,or is characteristically incapable of spinning.

D. B.The following information should be provided to the maneuver flight as appropriate: (a) A Statement of Entry Speed for Authorized Maneuvers (b) A Statement of Unauthorized Maneuvers(c) A Statement that aircraft is Unapproved or not suitable for Spinning.

E. ntry Speed for maneuvers flight (b) A Statement of Unauthorized maneuvers (c) A Statement that aircraft has been unapproved for Spins,or is characteristically incapable of spinning.

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581.Hydraulic fluid can cause corrosion.

A. 液压油会造成起火。

B. 液压油会引起腐蚀。

C. 液压油会导致伤害。

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