1155. It includes those maintenance practices necessary to prepare the aircraft for weighing
A. 它包括了准备飞机称重时的有用的维护信息;
B. 它包括了准备飞机顶起时的必要维护工作的信息;
C. 它包括了准备飞机称重时的必要维护工作的信息;
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404. The approved words were selected because they were simple and easy to recognize
A. The approved words were chosen because they are as simple as to be recognized.
B. If the words are difficult and hard to identify, they may not be selected as the approved words.
C. Simplicity and legibility are the main features of the approved words.
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2980. The airplane has been maintained in accordance with manufacturer recommendations or equivalent
A. 飞机已按照制造商要求或同等标准进行检查
B. 飞机已按照运营人要求或同等标准进行维护
C. 飞机已按照制造商建议或同等标准进行维护
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1000. Schematic diagrams may be used to indicate flow and to illustrate the operation of systems such as air control, electrical, fluid power, fuel and turbo systems
A. 原理图可以用来表示流程,并说明系统的工作过程,如空气控制、电力、流体动力、燃油和压气机系统。
B. 原理图可以用来表示流程,并说明系统的工作原理,如空气分庄、电力、流体动力、燃油和涡轮系统。
C. 原理图可以用来表示流程,并说明系统的操作,如空气控制、电力、流体动力、燃油和涡轮系统。
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3301. The pump( ) operate because the shaft( )broken 轴的损坏导致泵不能正常运行。
A. was not; was
B. does not; are
C. did not; was
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2927. Make sure that the flaps are retracted and the aileron trim handwheel is in the zero position
A. 确保襟翼收回或者副翼配平手轮在零位。
B. 确保襟翼伸出,并且副翼调节手轮在零位。
C. 确保襟翼收回,并且副翼配平手轮在零位。
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3062. That portion of the system which is used to dissipate static electricity
A. 系统中用于消散静电的部分。
B. 系统中用于排放静电的部分。
C. 系统中用于清除静电的部分。
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2882. 按如下方式计算垫片的厚度:t=x-y。
A. Accumulate the thickness of the shim as follows: t=x-y.
B. Calculate the thickness of the shim as follows: t=x-y.
C. Calculate the width of the shim as follows: t=x-y.
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1006. When you do work in a fuel tank a person must be near the tank at all times
A. When someone is working in a fuel tank you must stay next to the tank at all times.
B. When you do work in a fuel tank you must stay close to the tank at all times.
C. When one person does work in a fuel tank another person must be outside the tank at all times.
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372. 失速恢复期间最大高度损失约800英尺
A. Maximum altitude loss during stall recovery is approximately 800 feet.
B. Maximum altimeter loss during spin recovery is about 800 feet.
C. Maximum weight loss during stall recovery is nearly 800 feet.
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