A、 相关警戒灯必须在30秒后熄灭。
B、 故障的警告灯必须在30秒后关闭。
C、 相关警告灯会在30秒后熄灭。
答案:A
A、 相关警戒灯必须在30秒后熄灭。
B、 故障的警告灯必须在30秒后关闭。
C、 相关警告灯会在30秒后熄灭。
答案:A
A. 在初始蒙皮的初始紧固件位置,安装埋头铆钉。
B. 在初始蒙皮的初始紧固件位置,制作埋头垫圈。
C. 使埋头垫圈适用于初始蒙皮上的初始紧固件。
A. Supply airspeed instructions and the operational significance of such instructions.
B. Provide airspeed limitations and the operational instruction of such limitations.
C. Provide airspeed limitations and the operational significance of such limitations.
A. Release the hydraulic pressure in the accumulator.
B. Release the power pressure in the accumulator.
C. Release the hydraulic pressure in the actuator.
A. 禁止使用替代器材。
B. 使用消耗器材是允许的。
C. 允许使用替代材料。
A. When preparing dangerous goods, follow the operational instructions.
B. Before you use dangerous materials, obey these precautions.
C. Prior to applying any hazardous material, understand the principles of it.
A. If you find metal particles in the pump, find their source and repair the defective part.
B. If magnetic particles are found in the pump, locate their location and repair the affected part.
C. Locate their source and disassemble the defective part if you find metal objects.
A. The anti-leakage valve prevents oil leakage when you disconnect the oil tube from the anti-leakage valve to the lubrication unit.
B. When you reconnect the oil tube from the anti-leakage valve to the lubrication unit, the anti-leakage valve stops oil leakage.
C. When you discharge the oil tube from the anti-leakage valve to the lubrication unit, the anti-leakage valve protects oil leakage.
A. The arid welding coat may be polished with thin abrasive paper to hold a smoother layer.
B. The waterless painting coat may be worn with precise abrasive paper for a smoother surface.
C. The dried spray coat may be sanded with fine sandpaper to obtain a smoother finish.
A. 对于增压飞机和涡轮增压或涡轮螺旋桨飞机,应规定最大高度限制
B. 增压飞机、涡轮增压飞机或涡轮螺旋桨动力飞机,对于最高飞行高度有陈述。
C. 对于涡轮增压或涡轮螺旋桨飞机,可以提供最大高度限制。
A. After 10 flight cycles or 25 flight hours, which comes first, the rod end bearing shall be discarded if its wear is greater than 0.010 inch of diameter.
B. If the rod end bearing wear is greater than 0.010 inch in radial play, reject it within next 10 flight cycles or 25 flight hours whichever comes first.
C. Destroy the rod end bearing during 10 flight cycles or 25 flight hours when its wear is more than 0.010 inch of its radius, whichever comes first.