A、 The test will stop when the pressure is larger than 7000 kpa.
B、 Stop the test if the pressure reaches 7000 pa.
C、 Stop the test when the pressure is more than 7000 kpa.
答案：C
A、 The test will stop when the pressure is larger than 7000 kpa.
B、 Stop the test if the pressure reaches 7000 pa.
C、 Stop the test when the pressure is more than 7000 kpa.
答案：C
A. 为了使句子简短不要增加太多名词。
B. 为了使句子简短不要忽略名词。
C. 不要为了使句子简短而省略名词。
A. If the airspeed values are necessary to more than one configuration,the more restrictive IAS shall be used.
B. Where the airspeed values may be applicable to more than one configuration,the more conservative IAS value shall be used.
C. The more accurate IAS value should be used where the airspeed values are mandatory to less than one configuration.
A. 每一个系统有一个接收器,这个接收器位于电子舱。电子舱内可以对 FMS 自动调谐,或是对相应的 NAV 控制面板手动调谐。
B. 每一个系统有一个接收器,这个接收器位于电子舱。接收器可以通过 FMS 自动调谐,或是通过相应的 NAV 控制面板手动调谐。
C. 每一个系统有一个电子舱接收器,接收器可以被 FMS 远程调谐,或是通过相应的 NAV控制面板手动调谐。
D. C.每一个系统有一个电子舱接收器,接收器可以被 FMS 远程调谐,或是通过相应的 NAV控制面板手动调谐。
A. Move it lightly and make it through the hole
B. Move it slightly to make it aim at the hole
C. Move it gently to make it enter the hole
A. Navigation and full/static pressure systems refer to those units and components that provide aircraft navigation information,covering OOMB,pitot,static,ILS,flight guides,binnacles,indicators,etc.
B. Navigation and pitot/static systems refer to those units and components which provide aircraft navigational information,including VOR,pitot,static,ILS,flight director,compasses,indicators,etc.
C. Navigation and pitot/static systems refer to those units and components that provide aircraft navigation information,including VOR,pitot,still tubes,instrumental system,flight manual,compasses,indicator,etc.
A. Refer to the general information in addition to engine operation limits,guidelines and special procedures.
B. For general information,refer to engine operation limits,guidelines and special procedures.
C. Refer to engine operation limits,guidelines and special procedures besides general information.
A. 现代飞机都安装单元体结构的发动机。
B. 一个铸造结构的发动机安装在现代飞机上。
C. 一个整体发动机安装在所有现代飞机上。
A. The pump is installed behind the hydraulic motor.
B. The gearbox is installed behind the pneumatic motor.
C. Thehydraulic motor is installed behind the pump.
A. 引擎多的飞机改出螺旋程序可由代理商分别编写。
B. 多发飞机的改出螺旋程序可由制造商选择。
C. 多台发动机的改出螺旋程序可以包含在飞机制造商的操作手册中。
A. Get the approval of the design authority,whatever it is necessary to change the repair scheme.
B. Change the repair scheme,until getting the approval of the design authority.
C. If it is necessary to change the repair scheme,get the approval of the design authority.
