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.
答案：D
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.
答案：D
A. 10,000ft
B. 8,500ft
C. 14,000ft
D. 15,000ft
A. 左引气管道
B. 右引气管道
C. 右防冰管道
D. 右防冰管道
A. 经度longitude
B. 纬度latitude,
C. 高度altitude
D. 时刻time
A. 惯性离心力的作用
B. 地转偏向力的作用
C. 摩擦力的作用
A. 在平均海平面温度为15 度，修正气压1013.25 Hpa
B. 在平均海平面温度为15 度，高度每增加1KM 温度减小6 度
C. 修正气压1013.25 Hpa，高度每增加1KM 温度减小6 度
A. 机身前顶部；the forward top of the fuselage
B. 机身前机腹；the forward belly of the fuselage
C. 机身后顶部；the backward top of the fuselage
D. 垂直安定面两侧；bothside of the vertical stabilizer
A. 稳定的大气和上升气流
B. 暖湿气流和热力乱流
C. 上升气流和不稳定的大气
A. 内侧防滞系统发现故障。 Fault found in the anti-skid INBD system.
B. 外侧防滞系统发现故障。 Fault found in the anti-skid OUTBD system.
C. 转弯控制组件探测到故障。 Steering control unit has detected a fault.
D. 防滞-BTMS控制组件失去裕度，可能失去接地保护。 Loss of redundancy in anti-skid - BTMS control unit with a possible loss of touch-down protection.
