航空器对头相遇,应当各自靠右滑行,并且保持必要的安全间隔;航空器交叉相遇,飞行员从座舱______侧看到另一架航空器时,应当停止滑行,主动避让。
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急救飞行在无法取得目的地天气实况时,如何掌握放飞条件
A. 根据天气预报放行航空器;
B. 根据起飞站天气实况放行航空器;
C. 根据任务需要放行航空器
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缝翼和襟翼由______个缝翼/襟翼电子控制组件(SFECUs)进行控制。The slats and flaps are controlled by ______ slat/flap electronic control units (SFECUs).
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为什么摩擦层以上的大范围空气运动具有平行于等压线流动的趋势
A. 因为地转偏向力垂直作用在高低压中心的连线上
B. 因为地转偏向力有与水平气压梯度力相平衡的趋势
C. 因为空气与地表的摩擦力使得空气的运动向垂直于水平气压梯度力的方向偏转
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当N2达到%( ) rpm时,起动机马达脱开。Starter motor cut-out occurs at percent N2 rpm.
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单发飘降时应使用()方式下降。In case of SINGLE ENGINE DRIFT DOWN, use ( )mode for descent
A. DES
B. PITCH
C. VS
D. IAS
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在重要天气预告图上,符号“ LOC */? ”表示
A. 零星小雨夹雪
B. 零星小雪或霰
C. 局部地区有小雪或小雨
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判断正误True or False: 在五边进近航段,若失去完成进近所需导航精度,则PFD上将显示琥珀色的NO APPR信息。During the final approach segment, if the required navigation accuracy to complete the approach is lost, an amber NO APPR message is displayed on the PFD.
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ENG SYNC OFF 状态信息(白色)表明ENG SYNC OFF status (white)
A. 表明2台发动机处于高功率计划中Indicates that both engines are at a high power schedule.
B. 表明发动机 SYNC(同步)人工取消选择。Indicates that engine synchronization manually selected off by flight crew.
C. 指示一个 FADEC 通道不工作或可能会影响发动机传感器裕度的故障组合。Indicates that one FADEC channel is inoperative or a combination of faults that may affect engine sensor redundancy.
D. 指示 L FADECFAULT 1 包含的状态信息之外不严重的故障组合。Indicates a combination of faults that are less serious than the faults covered by a FAULT 1 status message.
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飞机压力加油的最大可加油量负载是:The maximum usable fuel load for a pressure refueled aircraft is:
A. 两侧油箱3398kg和中央油箱2267kg。3,398 kg. in both wings and 2,267 kg. in the center tank
B. 两侧油箱3,659 kg 和中央油箱2,267 kg 。3,659 kg. in both wings and 2,267 kg. in the center tank
C. 两侧油箱3,659 kg 和中央油箱2,091 kg 。3,659 kg. in both wings and 2,091 kg. in the center tank
D. 两侧油箱3,398 kg 和中央油箱2,091 Kg 。3,398 kg. in both wings and 2,091 Kg. in the center tank.
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