A、 At the location shown in the figure,waterproof corrosion inhibiting compound has been used on certain aircraft construction.To keep the effectiveness of this protection,reapply the compound in these or other locations periodically.
B、 Water displaying corrosion inhibiting compound has applied on certain airplanes structure in the locations in this figure.Periodic reapplication must be applied in these and other locations,so as to maintain effectiveness of this protection.
C、 Water displacing anti-seize compound has been applied on certain airplanes construction in the locations in this figure.Periodic reapplication should be utilized in these and other locations,in order to keep effectiveness of the protection.
答案：A
A、 At the location shown in the figure,waterproof corrosion inhibiting compound has been used on certain aircraft construction.To keep the effectiveness of this protection,reapply the compound in these or other locations periodically.
B、 Water displaying corrosion inhibiting compound has applied on certain airplanes structure in the locations in this figure.Periodic reapplication must be applied in these and other locations,so as to maintain effectiveness of this protection.
C、 Water displacing anti-seize compound has been applied on certain airplanes construction in the locations in this figure.Periodic reapplication should be utilized in these and other locations,in order to keep effectiveness of the protection.
答案：A
A. 沿四周向内对窗户进行抛光。
B. 以圆周运动方式擦拭窗户。
C. 呈垂直方向给窗户镀膜。
A. The valve allows the hydraulic pressure to pass through in this configuration.
B. The hydraulic pressure is blocked by the valve in this setup.
C. In this configuration,the hydraulic pressure bypasses the valve.
A. 所有人员必须充分了解安全预防措施。
B. 所有人员必须充分了解安全规定。
C. 所有人员必须充分了解逃生方法。
A. 发动机燃油系统包括协调器或与其不同作用的装置、发动机泵和滤清器总成、主和推力增强器、燃油控制装置、电子温度基准控制装置、温度基准阀、燃油歧管、燃油喷嘴、燃油浓缩系统、转速传感开关、继动箱总成、电磁滴水阀、燃烧器排水阀等。
B. 飞机燃油系统包括协调器或同等作用的装置、温度基准阀、燃油歧管、燃油喷嘴、燃油浓缩系统、转速传感开关、继动箱总成、电磁滴水阀、燃烧器排水阀等。
C. 发动机燃油系统包括调节器或同等装置、发动机驱动的燃油泵和油滤组件、主燃烧室和加力燃烧室燃油控制装置、电子温度基准控制装置、温度基准阀、燃油总管、燃油喷嘴、富油系统、转速敏感电门、继电器组件、电磁滴油阀、燃烧室排油阀等。
D. B.飞机燃油系统包括协调器或同等作用的装置、温度基准阀、燃油歧管、燃油喷嘴、燃油浓缩系统、转速传感开关、继动箱总成、电磁滴水阀、燃烧器排水阀等。
E. C.发动机燃油系统包括调节器或同等装置、发动机驱动的燃油泵和油滤组件、主燃烧室和加力燃烧室燃油控制装置、电子温度基准控制装置、温度基准阀、燃油总管、燃油喷嘴、富油系统、转速敏感电门、继电器组件、电磁滴油阀、燃烧室排油阀等。
A. For all fuel loadings,the initial airplane weight should be the maximum allowable.
B. The initial airplane weight should contain the maximum allowable for all fuel loads.
C. For all kinds of fuels,the initial aircraft weight should be the maximum allowable.
A. Apply a layer of sealant on the top access panel.
B. Apply a layer of solvent on the top access panel.
C. Apply a layer of sealant on the bottom access panel.
A. 2 毫米的价值是允许的。
B. 允许使用 2 毫米的价值。
C. 允许使用 2 毫米的值。
A. In order to locate lower margins of safety components and areas,current records were reviewed.
B. To find components and areas where have showed lower margins of safety,existing results were examined.
C. Existing analyses were reviewed to identify components and areas that may have exhibited lower margins of safety.
A. 就防冰或除冰系统对飞机在已知结冰条件下的运行批准的影响,应在“补充程序”中的限制部分里予以明确。
B. “补充程序”的极限章节应明确规定,在已知结冰条件下运行必须确保防冰或除冰系统正常工作。
C. 防霜或除霜系统对在已知结冰条件下操作飞机的批准的影响应在“补充程序”的限制章节中明确规定。
D. C.防霜或除霜系统对在已知结冰条件下操作飞机的批准的影响应在“补充程序”的限制章节中明确规定。
A. Contamination of the grease can cause damage to the bearing.
B. Contamination of the oil can cause damage to the shaft.
C. Pollution of the grease can cause damage to the axle.
