A、 低于96%。below 96%
B、 在45%-85%之间。within 45% and 85%
C、 液压油箱1和2至少45%,油箱3至少85%。at least 45% for reservoirs 1 and 2 and 85% for reservoir 3
D、 超过45%。more than 45%
答案:B
A、 低于96%。below 96%
B、 在45%-85%之间。within 45% and 85%
C、 液压油箱1和2至少45%,油箱3至少85%。at least 45% for reservoirs 1 and 2 and 85% for reservoir 3
D、 超过45%。more than 45%
答案:B
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A. 机翼油箱之间的交输 crossflow to either wing tank
B. 从加油/排油活门里排油 defueling from the refuel/defuel valve
C. 人工压力加油 manual pressure refueling
D. 燃油计算机连续通电自测continuous built-in test of the fuel computer
E. 加油前的系统测试 system testing prior to refueling
F. 自动压力加油 automatic pressure refueling
G. 燃油从中央油箱中转移到任意机翼油箱 fuel transfer from the center tank to either wing tank
A. 越大;
B. 越小;
C. 越冷
A. 可能存在强降水
B. 可能存在风切变
C. 可能存在严重结冰
A. 航空器、发动机、螺旋桨和航空器上的设备
B. 航空器、发动机、螺旋桨
C. 航空器、发动机
A. 中断起飞过程中推力手柄收至慢车且反推放出。The thrust levers are retarded to idle during a rejected takeoff and thrust reverser are deployed
B. 中断起飞过程中推力手柄收至慢车且反推在过渡中。The thrust levers are retarded to idle during a rejected takeoff and thrust reverser are in transit
C. 中断起飞过程中推力手柄收至慢车。The thrust levers are retarded to idle during a rejected takeoff
D. 中断起飞过程中推力手柄收至慢车,反推放出且使用刹车。The thrust levers are retarded to idle during a rejected takeoff and thrust reverser are deployed and brakes applied
A. 可用时长约10分钟的独立可充电式电瓶independent rechargeable batteries for approximately 10 minutes duration
B. 可用一定时长的主直流汇流条 main DC bus for an unlimited duration
C. 可用时长约30分钟的APU电瓶 APU battery for approximately 30 minutes duration
D. 可用时长约30分钟的飞机主电瓶 main aircraft battery for approximately 30 minutes duration
A. 30
B. 40.0
C. 50.0
D. 55
A. 一条跑道的复飞航迹与相邻跑道的复飞航迹扩散角不小于90度
B. 一条跑道的复飞航迹与相邻跑道的复飞航迹扩散角不小于60度
C. 一条跑道的复飞航迹与相邻跑道的复飞航迹扩散角不小于30度