A、 将飞机放回到通常停放位。
B、 将飞机放回到初始位置。
C、 将飞机恢复到初始构型.
答案:C
A、 将飞机放回到通常停放位。
B、 将飞机放回到初始位置。
C、 将飞机恢复到初始构型.
答案:C
A. 确保在表 1 中给定的范围内进行测量。
B. 确保在表 1 中给定的范围内进行调节。
C. 确保按照表 1 中的数值进行校准。
A. 移动装有隔热毯的喷射管或排气锥时要小心。
B. 当你移动喷气式管道或带有绝缘垫的排气孔时要小心。
C. 小心地移动发射管或排气口的保温垫。
A. Solid the sealant at a peripheral temperature.
B. Cure the sealant at a uniform temperature.
C. Solid the sealant at the same temperature.
A. 通常,在描述飞机或其系统时,应使用第三人称。例如:前轮配备有摆振阻尼器(减摆器),以防止地面滑行时前轮振颤。
B. 通常,在描述飞机或其系统时,应使用第一人称。例如:前轮配备有摆振阻尼器(减摆器),以防止在地面上滑行时前轮振颤。
C. 通常,在描述飞机或其系统时,应使用第三人称。例如:后轮配备有摆振阻尼器(减摆器),以防止在地面上滑行时后轮振颤。
D. C.通常,在描述飞机或其系统时,应使用第三人称。例如:后轮配备有摆振阻尼器(减摆器),以防止在地面上滑行时后轮振颤。
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.
A. 这些单位及组件为阻止或销毁雨雪形成在飞机的各个部分上提供了渠道。
B. 这些单件及组件提供了一种方法,能够阻止或祛除飞机各部分的冰雨形成。
C. 能够防止飞机不同地方形成积冰和积雨或消除相关影响的部件及组件。
A. 如果一种化合物用于紧固件,使用“润滑紧固件”力矩。
B. 如果下列某一种化合物要用在紧固件上,则力矩需参考“润滑紧固件”。
C. 如果下列化合物之一用在紧固件上,则需使用“经润滑的紧固件”扭矩值。
A. Make sure there is no leakage of hydraulic fluid at the router.
B. Make sure there is no leakage of hydraulic fluid at the transducer.
C. Make sure there is no leakage of hydraulic fluid at the transponder.
A. Overhaul of any components covered in this chapter shall be completed in accordance with data other than those provided by the manufacturer.
B. None of the components covered by this chapter shall be overhauled except in accordance with the manufacturer's data.
C. All components covered in this chapter must be overhauled according to the technical dataprovided by the manufacturer.
D. C.All components covered in this chapter must be overhauled according to the technical dataprovided by the manufacturer.
A. Materials used to repair layered structures must keep the rigidity,gravity,aerodynamic or electronic properties of the original assembly.
B. The materials used in the repair of laminate structures must preserve the strength,weight,aerodynamic characteristics,or electrical properties of the original assembly.
C. Materials that are used for fixing the layer structures must maintain the intensity,weight,aerodynamic or electrical properties of the original assembly.