A、 This section includes limitations adapted by the airworthiness authority.
B、 The limitations included in this Section are approved by the airworthinessauthority.
C、 The limitations included in this Section are adopted by the airworthiness authority.
答案:B
A、 This section includes limitations adapted by the airworthiness authority.
B、 The limitations included in this Section are approved by the airworthinessauthority.
C、 The limitations included in this Section are adopted by the airworthiness authority.
答案:B
A. 三台计算机收集数据,与系统参数一起放在连接到显示器组件的数据链路上。
B. 三台计算机从系统中更正数据和参数,将它们放在连接到显示器组件的数据链路上。
C. 三台计算机收集系统数据和参数,并通过数据链接将它们一起传送给显示组件。
A. If the passed or failed indication that shows on the MAT does not agree with the indication on the maintenance page,ignore the indication on the MAT.
B. If the pass or fail prompt displayed on MAT is inconsistency with the prompt on the maintenance page,please ignore the prompt on MAT.
C. Neglect the instruction on MAT,whether the passing or failure sign shown on the MAT or not.
A. When the indicator is visible,stop the pump.
B. When the indicator comes on ,stop the pump.
C. Stop the pump unless the indicator comes into view.
A. 探头的颜色变为绿色。
B. 指示器的颜色变为绿色。
C. 显示器的颜色变为绿色。
A. 如果有一个或多个叶片损毁,请在发动机日志中记录。
B. 如果有一个或多个叶片缺失,请查看发动机日志中的记录。
C. 若缺少一个或多个叶片,在发动机记录本中予以记录。
A. Do not exceed this dimension or Mach in any operation.
B. Do not exceed the regulated flight speed or Mach Number in any operation.
C. Do not exceed this speed or Mach Number in any operation.
A. 后缘襟翼有 25 个以上的组件。
B. 后缘襟翼超过 25 个单位。
C. 前缘襟翼超过 25 个单位。
A. 有两种可用的编号方法。对于拥有一系列复杂系统的飞机,建议使用完整的“系统/章节”索引方法。对于小飞机或相对不复杂的飞机,可用简化的索引方法。
B. 有两种可用的编号方法。对于拥有一系列复杂系统的飞机,建议使用完整的“系统/章节”索引方法。对于小飞机或相对不复杂的飞机,可在编写索引号时用缩写的方式。
C. 有两种可用的编号方法。对于拥有复杂系统矩阵的飞机,建议使用完整的“系统/章节”索引方法。对于小飞机或相对不复杂的飞机,可在编写索引号时用缩写的方式。
D. C.有两种可用的编号方法。对于拥有复杂系统矩阵的飞机,建议使用完整的“系统/章节”索
E. C.有两种可用的编号方法。对于拥有复杂系统矩阵的飞机,建议使用完整的“系统/章节”索引方法。对于小飞机或相对不复杂的飞机,可在编写索引号时用缩写的方式。
A. If the pressure decreases quickly,the shear pins in the latch will break.
B. If the pressure reduces gradually,the shear pins in the lock will break.
C. If the pressure drops radically,the alignment pin in the lock will damages.
A. The pitot tube is on the external forward part of the airplane.
B. You may find the pitot probe on the front internal side of the fuselage.
C. The pitot probes are located on the forward external part of the airplane.