A、 副翼配平不在起飞范围之内(配平> ±1 度) 且两台发动机 >70% N1。Aileron trim is outside of the takeoff range (trim > ±1 degree) and both engines >70% N1.
B、 自动驾驶仪接通,飞机为起飞构型且两台发动机>70% N1。Autopilot is engaged with the aircraft configured for takeoff and both engines >70% N1.
C、 襟翼不在起飞位置,飞机为起飞构型。Flaps are not in a takeoff position with the aircraft configured for takeoff.
D、 方向舵配平不在起飞范围之内。Rudder trim is outside of the takeoff range.
答案:D
A、 副翼配平不在起飞范围之内(配平> ±1 度) 且两台发动机 >70% N1。Aileron trim is outside of the takeoff range (trim > ±1 degree) and both engines >70% N1.
B、 自动驾驶仪接通,飞机为起飞构型且两台发动机>70% N1。Autopilot is engaged with the aircraft configured for takeoff and both engines >70% N1.
C、 襟翼不在起飞位置,飞机为起飞构型。Flaps are not in a takeoff position with the aircraft configured for takeoff.
D、 方向舵配平不在起飞范围之内。Rudder trim is outside of the takeoff range.
答案:D
A. 当N2 rpm超过10%的时候When the engine has accelerated to 10% N2 rpm,
B. 当N2 rpm超过20%的时候When the engine has accelerated to 20% N2 rpm,
C. 当N2 rpm超过30%的时候When the engine has accelerated to 30% N2 rpm,
D. 当N2 rpm超过40%的时候When the engine has accelerated to 40% N2 rpm,
A. 直流重要汇流条
B. 交流重要汇流条
C. 直流勤务汇流条
D. 交流汇流条2失效
A. 大气数据基准面板air data reference panel
B. 飞行控制面板Flight control panel
C. 显示转换面板Reversionary display panel
D. 显示控制面板Display control panel
A. 空气的相对湿度
B. 大气的稳定度
C. 空气的温度
A. 200 kts
B. 300kts
C. 0.50 Mach
D. 0.45 Mach
A. 30%;
B. 40%;
C. 50%;
D. 60%;
A. 驱动燃油泵 driven fuel pumps
B. 可变几何作动筒 variable geometry actuators
C. 反推装置 thrust reversers
D. 压缩机导流叶片 compressor stator vanes
A. 显示控制面板display control panel(DCP)
B. 大气数据参考面板Air data reference panel(ARP)
C. 转换面板Reversionary panel
D. 音频控制面板Audio control panel