A、 确保 P36 面板上的“交流已连接”及“未使用”指示灯点亮。
B、 确保交流电已连接,并且 P36 面板上的“未使用”指示灯处于点亮状态。
C、 确保 P36 面板上的“交流已连接”指示灯点亮,但其并未使用。
答案:A
A、 确保 P36 面板上的“交流已连接”及“未使用”指示灯点亮。
B、 确保交流电已连接,并且 P36 面板上的“未使用”指示灯处于点亮状态。
C、 确保 P36 面板上的“交流已连接”指示灯点亮,但其并未使用。
答案:A
A. Report any corrosion found to the manufacturer.
B. Report any cracks found to the manufacturer.
C. Report any damage found to the manufacturer.
A. 电气/电子面板和多用途部件上的图示涵盖了部分重要的通用电气和电子部件。
B. 电气/电子面板和多用途部件涵盖了所有通用电气和电子部件。
C. 电气/电子面板和多用途部件上的文字说明涵盖了所有通用电气和电子部件。
A. 不要使用其他未经批准的动词短语。
B. 不要使用其他未经批准的动词时态。
C. 不要使用其他未经批准的动词词组。
A. This Issue 7 of the specification fully takes place all issues and revisions before.
B. This Issue 7 of the specification fully covers all prior issues and revisions.
C. This Issue 7 of the specification fully replaces all previous issues and revisions.
A. Humidity adjustment is manual.
B. Pressure adjustment is automatic.
C. Temperature adjustment is automatic.
A. 书写名词词组不能超过三个单词。
B. 写出三个单词以上的名词词组。
C. 写出的形容词词组要少于三个词。
A. 确保那些指示的位置是襟翼的位置。
B. 确保指示与襟翼的位置一致。
C. 确保那些迹象同意襟翼的位置
A. Spoilers are used to increase the drag of the aircraft in flight,or to interrupt lift during landing and during rejected take-off.
B. Spoilers are used to enhance aircraft resistance in flight or to disrupt boost during landing and when take-off is canceled.
C. Spoilers are used to increase the aircraft drag in flight,or destroy the lift during landing and in case of aborted take-off.
A. It is very difficult to determine the effects of corrosion but,as the reports from the CAP inspections are received,the inspection times will be adjusted for any severe problems.
B. It is not easy to decide the affection of corrosion,when the reports from the CAP inspections are received,the inspection duration will be changed for any serious problems.
C. It is very hard to make the decision of the corrosion effects but,if the reports from the CAP inspections are obtained,the inspection times will be arranged in accordance with the severest problem.
A. A Weight and Moment Limit diagram shall be used to describe the c.g.limits.
B. The maximum weight moment envelope diagram should be used to describe the c.g.limit of the aircraft.
C. A Weight and Moment Limit diagram shall be used to describe the maximum c.g.limit.