A、 "EMERGENCY EXIT" placard at exit hatch over Left wing is illegal.
B、 "EMERGENCY EXIT" placard at exit hatch over Left wing is not legible.
C、 "EMERGENCY EXIT" placard at exit hatch over Left wing is missing.
答案:B
A、 "EMERGENCY EXIT" placard at exit hatch over Left wing is illegal.
B、 "EMERGENCY EXIT" placard at exit hatch over Left wing is not legible.
C、 "EMERGENCY EXIT" placard at exit hatch over Left wing is missing.
答案:B
A. If fault message continues,push the audio cancel pushbutton on the aviation electric test panel.
B. If fault message persists,press audio cancel pushbutton on the avionics test panel.
C. If fault message goes on,press audio cancel pushbutton on the airborne test panel.
A. 使用良好的设备去做这项检查以及目视检查。
B. 使用正确的设备去做这项检查而不是目视检查。
C. 使用正常的设备去做这项检查而不是目视检查。
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.
A. Examine and remove the parts that are damaged.
B. Examine the removed parts with damage.
C. Examine the removed parts for damage.
A. 提供液压动力的说明在显示液压动力警告的屏幕底部,你必须向下滚动屏幕才能看到
B. 液压动力供给说明在屏幕底部显示液压动力警告,你必须向下滚动屏幕才能看到说明。
C. 你必须向下滚动屏幕才能看到液压动力供给指令,因为指令在显示警告的屏幕底部。
A. 这表明您可以安装一个替代的继电器。
B. 这表明您可以安装一个新的继电器。
C. 这表明您可以更换一个新的继电器。
A. 如果没有液压动力放下前起落架,起落架的重量和气流会将其推至放下位。
B. 如果液压动力未将前起落架放下,起落架的重量和重力会将其放下。
C. 液压动力可以放下前起落架,起落架的重量和气流也可以将其推至放下位。
A. 描述飞机电源系统时,应说明线束保护功能。
B. 描述飞机电源系统时,应提供线路保护的描述。
C. 描述飞机电源系统时,应说明回路保护。
A. 警告和注意事项中的文字将标为粗体,而注释可以在适用的文本之后,取决于要重点突出的材料。
B. 为了突出材料的重点,警告和注意事项应在其适用的文本之前,但注释可以在适用文本之前或之后。
C. 警告和注意事项应在其适用的文本之前,但注释可以在适用文本之前或之后,具体取决于要突出显示的材料。
D. B.为了突出材料的重点,警告和注意事项应在其适用的文本之前,但注释可以在适用文本之前或之后。
E. C.警告和注意事项应在其适用的文本之前,但注释可以在适用文本之前或之后,具体取决于要突出显示的材料。
A. The turboprop engine controls include linkages and controls to the coordinator or equivalent and from the coordinator or equivalent to the propeller governor,fuel control unit,or other units being controlled.
B. The control device of a turbojet engine includes a linkage mechanism and control device to a coordinator or equivalent device,as well as a linkage mechanism from a coordinator or equivalent device to a propeller governor,fuel control component,or other controlled components.
C. The turboprop engine controls include a coordinator or equivalent device,a linkage mechanism,a control device,a propeller governor,a fuel control component,or other controlled components.