1415.To obtain exact performance values from tables,it is necessary to interpolate between the incremental values.

153.Principal dimensions shall be shown upon the drawing.

A. 特殊尺寸应显示在图形中。

B. 详细尺寸应显示在图纸上。

C. 主要尺寸应显示在图纸上。

3007.在更正栏中,列出部件故障纠正措施涉及的所有注意事项或要点。

A. In the correction column,list any notes or key points involved in correcting the trouble in the unit.

B. List any notes or key points involved in corrective actions for units faults during correction.

C. List all corrective actions,any notes or key points related to a unit failure when you do the Correction.

1912.The usual control for the left pack makes sure that it supplies air at a temperature that gives the necessary cooling for the flight compartment.

A. The usual control for the left pack ensures that it supplies air at a temperature.The temperature gives the occasional cooling for the flight compartment.

B. The normal control for the left pack makes sure that it supplies air.The cooling provides the necessary temperature for the flight compartment.

C. The usual control for the left pack assures that the temperature of the supplied air will provide the control cabin with the needed cooling.

3079.应急照明是指单独的、独立的子系统,在主电源故障的情况下提供照明。

A. Emergency illumination refers to an individual and dependent subsystem which is used to provide lighting when the main electrical power fails.

B. Emergency lighting can provide illumination for an individual and independent subsystem in case of main electrical power failure.

C. Emergency lighting is the separate and independentsubsystem used to provide illumination in case of primary electrical power failure.

965.描述机身、机翼和尾翼的结构。

A. State structure of airframe,wings and tail.

B. Present structure of airframe,wings and empennage.

C. Describe structure of fuselage,wings,and empennage.

261.Additional information provided by the manufacturer should be appropriately integrated into the order shown in paragraphs 5.37 or 5.41.

A. 制造商提供的附加信息应适当地纳入第 5.37 或 5.41 段所示的指令中。

B. 制造商应该提供适当的附加信息,这些信息在第 5.3 或 5.41 段的指令中显示出。

C. 制造商提供的附加信息应该是适当的,并便如第 5.37 或 5.41 段相关指令中。

1921.When there is an ""emergency"" situation,it is usually a failure that requires an immediate and quick response,such as an entire engine failure,fire or smoke,or perhaps a rapid drop in cabin pressure."

A. For "emergency",the related failure should be responded immediately,for example,the total engine failure,fire or smoke,sudden cabin pressure lost.

B. An "Emergency" almost including a serious failure that requires later response,such as a total engines failure,flame out or smoke,or rapid cabin pressurization.

C. For "emergency",the related failure should be treated immediately,for example,the total engine is not malfunctioning,fire or smoke,sudden cabin pressure lost.

823.逆时针旋转盖子。

A. Turn the cap counterclockwise.

B. Turn the cap clockwise.

C. Rotate the cap clockwise.

232.The sealant burns at 109 deg.F.

A. 这种防腐剂在华氏 109 度时融化。

B. 这种密封胶在华氏 109 度时燃烧。

C. 这种混合物在华氏 109 度时气化。

2792.Deactivation/Reactivation procedures for circuits,systems,units,etc.,shall be included.This is important because during maintenance,certain components may need to be deactivated for safety reasons or to prevent damage to the aircraft or equipment.It is also important to have instructions for reactivating these components once maintenance is complete to ensure that theyare functioning properly and do not pose a risk to the safety of the aircraft or its occupants.

A. 停用/重新启用电路、系统、组件等的程序应包括在内。这是因为在维护过程中,由于安全原因或为防止对飞机或设备造成损坏,某些部件可能需要停用。同样重要的是,一旦维护完成,需要有重新启用这些部件的说明,以确保它们正常运行,不会对飞机或机上设备的安全构成风险。

B. 停用/重新启用电路、系统、组件等的程序应包括在内。这是因为在维护过程中,由于安全原因或为防止对飞机或设备造成损坏,某些部件可能需要停用。同样重要的是,一旦维护完成,需要有重新启用这些部件的说明,以确保它们工作正常,不会对飞机或机上人员的安全构成风险

C. 停用/重新启用管路、系统、组件等的程序应包括在内。这是因为在维护过程中,由于安全原因或为防止对飞机或设备造成损坏,某些部件可能需要停用。同样重要的是,一旦维护完成,需要有重新启用这些部件的说明,以确保它们工作正常,不会对飞机或机上人员的安全构成风险