185.Apply two layers of protective compound to prevent hydraulic fluid
damage to the sealant.

A. 　使用具有良好硬度特性和足够重量和质量的白纸,以消除双面打印时透视显
示。

B. 　使用具有良好力量特性和足够重量和质量的白纸,以消除双面打印时透视显
示。

C. 　使用具有良好强度特性和足够重量和质量的白纸,以消除双面打印时透视显
示。

A. 　在发动机记录卡上填写记录

B. 　在室温下填写发动机记录卡

C. 　把温度写在发动机记录卡上。

A. 　 当你安装天线,排列符号必须指向前方。

B. 　 当你安装天线,校准箭头必须指向前方。

C. 　 当你安装天线,校准点必须向前方。

A. 　SUPPLYS

B. 　RECEIVES

C. 　ACCEPTS

A. 　定义的措词应尽可能简单,并且必须与手册中定义的术语相符。

B. 　定义的措词必须与手册中使用的定义术语一致,还应该用简单的方式来表达。

C. 　定义的措词应简单并符合手册中的术语。

A. 　Let the temperature increase until it is the same as the ambient
temperature.

B. 　Wait for a few minutes until the temperature of the component exceeds
the ambient temperature.

C. 　Let the component cool down until its temperature is the same as the
ambient temperature.

A. 　You can use electric motors to drive fuel and hydraulic pumps or to
drive a valve to the commanded position in the fuel,hydraulic or air
conditioning system or to move doors and cargo containers.

B. 　Electric motor can drive fuel and hydraulic pumps or drive a valve to
the commanded position in the fuel,hydraulic or air conditioning system
or move mechanical parts like doors and cargo containers to produce
mechanical power.

C. 　Electric motor produce mechanical power and their main functions are
to drive fuel and hydraulic pumps,to drive a valve to the commanded
position and to move mechanical parts like doors and cargo containers.

A. 　虽然建议使用诸如阴暗面、交叉区域、分隔符或类似的方法,但颜色的使用
是符合规定的。

B. 　虽然建议使用诸如斜线、交叉线、分栏符或类似的方法,但颜色的使用是允
许的。

C. 　虽然建议使用诸如阴影、交叉阴影、隔挡或类似的方法,但颜色的使用是允
许的。

A. 　It is standard to do the procedure in this service bulletin.

B. 　It is necessary to do the procedure in this service bulletin.

C. 　It is mandatory to do the procedure in this service bulletin.

A. 　Maneuvering Speed is the maximum speed what required of full uncommitted
aerodynamic control will not exceed the airplane.

B. 　Maneuvering Speed is the largest speed that the aerodynamic application
by the full available control will not cause the aircraft overexert.

C. 　Maneuvering Speed is the maximum speed at which application of full
available aerodynamic control will not overstress the airplane.