A、 自动推杆器失效或故障或失速保护计算机的一个通道故障或 AOA 传感器故障。Pusher deactivated or failed or one channel of the stall protection computer failed or AOA sensor failed.
B、 俯仰感力系统故障。Failure of the pitch feel system.
C、 方向舵行程限制器(RTL)功能缺失。Loss of rudder travel limiter (RTL) function.
D、 两个偏航阻尼器都关断或故障。Both yaw dampers are off or failed.
答案:A
A、 自动推杆器失效或故障或失速保护计算机的一个通道故障或 AOA 传感器故障。Pusher deactivated or failed or one channel of the stall protection computer failed or AOA sensor failed.
B、 俯仰感力系统故障。Failure of the pitch feel system.
C、 方向舵行程限制器(RTL)功能缺失。Loss of rudder travel limiter (RTL) function.
D、 两个偏航阻尼器都关断或故障。Both yaw dampers are off or failed.
答案:A
A. 停止滑行、听从地面指挥
B. 靠右方滑行
C. 靠左方滑行
A. 只有左右机翼前缘Left and right wing leading edges only
B. 左机翼,右机翼和升降舵前缘 Left wing, right wing,and elevator leading edges
C. 发动机整流罩,左机翼和右机翼Engine cowls, left wing and right wing
D. 机翼和探头 wings and probes
A. 500
B. 1000
C. 1500
D. 2000
A. 变化不大
B. 将要增大
C. 将要减小
A. 20
B. 30
C. 40
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. 飞行扰流板没有收起,飞机为起飞构型。Flight spoilers are not retracted with the aircraft configured for takeoff.
C. 水平安定面配平不在起飞范围之内。Horizontal stab trim is outside of the takeoff range.
D. 停留刹车设置, 飞机为起飞构型且两台发动机>70% N1。Parking brake is set with the aircraft configured for takeoff and both engines >70% N1.
A. 1分钟70% N1 70% N1 for 1 minutes
B. 2分钟75% N1 75% N1 for 2minutes
C. 1分钟80% N1 80% N1 for 1 minutes
D. 2分钟85% N1 85% N1 for 2 minutes
A. 环控和防冰简图页 ECS and ANTI-ICE synoptic pages
B. 防冰简图页 ANTI-ICE synoptic page
C. 状态页 status page
D. 环控简图页 ECS synoptic page
A. 沿山谷中间飞;
B. 离开迎风坡而靠近背风坡;
C. 离开背风坡而靠近迎风坡