A、 The failure of the test causes that the message under MORE DETAlLS on the display is false.
B、 lf the test fails, a fault message is displayed after ‘MORE DETAILS is selected.
C、 lf the test fails, fault message can be displayed below MORE DETAILS.
答案:C
A、 The failure of the test causes that the message under MORE DETAlLS on the display is false.
B、 lf the test fails, a fault message is displayed after ‘MORE DETAILS is selected.
C、 lf the test fails, fault message can be displayed below MORE DETAILS.
答案:C
A. 如果由于腐蚀你不能拆卸螺栓,则涂渗透油
A. 更换磨损超过最大限度的部件。
B. 更换部件,磨损已超过最小限度。
C. 拆卸元件,磨擦已超过最大限度。
A. 写作规则包括语法和文体观点。字典给出了撰写人可以使用的一般词汇。
B. 写作规则包括语法和文体方面。字典给出了撰写人可以使用的一般词汇。
C. 写作规则包括语法和文体细则。字典给出了撰写人可以使用的全体词汇。
A. 确保皮托管温度增加至 500 摄氏度以上。
B. 确保机外环境温度增加 500 摄氏度。
C. 确保探头温度增加至、500 摄氏度以上
A. The emergency exit doors are known as, backup exit and they should not be used in special condition
B. The emergency exit doors are used for the escape and are not used as the normal exits.
C. The emergency exit doors are applied to board that are not usually used for exit.
A. However, manufacturers may omit System/Chapters that are not applicable to the product or combine
Systems/Chapters where it is feasible.
B. However, manufacturers may adopt Systems/Chapters that are not applicable to the product or constitute
systems/Chapters when necessary
C. However, operators may omit Systems/Chapters applicable to the product or constitute Systems/Chapters
where practical.
A. 在执行此程序过程中请使用 12 英寸的套筒扳手。
B. 在此过程中使用 12 英尺套筒手柄。
c、在此过程中使用 12 号扳手手柄。
A. 重心是飞机悬浮时保持平衡的点。它与参考基准的距离是通过总力矩除以飞机的总重量得出的。
B. 飞机的重心是使飞机保持平衡的点。它与参考基准的距离可以通过总弯矩除以飞机总重量找到。
C. 重心是如果飞机悬着使飞机保持平衡的点。它到参照基准的距离可以通过总长度除以总重量找到。
A. A small child should sit in an unlimited seat.
B. A small child needs to sit in a seat with safety device.
C. A small child could sit in an adult seat.
A. The Federal Aviation Regulations 'require "maximum continuous power.to be used during airframe and
engine combination certification to show obedience with certain criteria.
B. Federal aviation regulations require "maximum continuing power" to be used during the certifying of the
airframe and engine to meet certain criteria.
C. Federal aviation regulations,
"maximum continuous power", are used to show compliance with certain standards.