A、 Make sure that the latch is fully engaged.
B、 Make sure that the knob is fully engaged.
C、 Make sure that the latch in full engaged position.
答案:A
A、 Make sure that the latch is fully engaged.
B、 Make sure that the knob is fully engaged.
C、 Make sure that the latch in full engaged position.
答案:A
A. 油箱释压活门在 85-90psi 之间打开以保护油箱不会超压。
B. 为保护管路不会超压,释压活门在 85-90psi 之间打开。
C. 选择活门在 85-90psi 之间打开以保护油箱正常工作。
A. Set the "ATT" knob to the local attitude.
B. Set the "ALT" knob to the local altitude.
C. Set the "LAT" knob to the local latitude.
A. 对于着陆距离,应包括地面滑跑和超过 50 英尺障碍物的总距离。
B. 对于着陆距离,应包括地面滑跑距离和从高于着陆表面 50 英尺到着陆完全停止飞越的地面距离。
C. 对于着陆距离,应包括地面滚转和超过 50 英尺障碍物的总距离。
A. 测量压力下降所需时间。
B. 必须测量压力下降时间。
C. 压力下降所需时间是可以测量的。
A. 本段描述了不同飞行阶段重量和力矩的计算程序,以及确保重心处于经批准范围内的程序。
B. 本段描述了为计划飞行的各个阶段计算重量和力矩的程序,以此确保重心处于经批准的范围内。
C. 本段描述了为计划飞行的各个阶段计算重量和配平的程序以及确保重力的中心点在批准范围内的程序。
D. B.本段描述了为计划飞行的各个阶段计算重量和力矩的程序,以此确保重心处于经批准的范围内。
E. C.本段描述了为计划飞行的各个阶段计算重量和配平的程序以及确保重力的中心点在批
F. C.本段描述了为计划飞行的各个阶段计算重量和配平的程序以及确保重力的中心点在批准范围内的程序。
A. 适航指令是从事飞机进行维修时必须使用的程序。
B. 在航空器上执行适航指令时,必须阅读本程序。
C. 适航指令必须是对飞机维修有用的程序。
A. 风干过滤器。
B. 在大气中干燥排油口。
C. 在空中排干加油口。
A. That portion of the system is used to perform the cranking portion of the starting operation.
B. That portion of the system is used to perform the igniting portion of the starting operation.
C. That portion of the system is used to perform the cranking portion of the igniting operation.
A. Oil comes from the supply system to lubricate and cool internal components in the engine.
B. Oil coming from the scavenge system will supply lubrication and cooling for the internal components of the engine.
C. The oil supply system will give lubrication and cooling for the internal components of the engine.
A. When showing a low flow or not sufficient cooling condition,the low flow sensor produces an alarm signal of the flight compartment for warning.
B. When a low flow or under cooling condition occurs,the low flow sensor provides an alarm signal to the cabin compartment for alert.
C. When a low flow or not sufficient cooling condition occurs,the low flow sensor supplies an alarm signal to the flight compartment for annunciation.