A、 不变
B、 由右侧风变为左侧风
C、 由左侧风变为右侧风
答案:C
A、 不变
B、 由右侧风变为左侧风
C、 由左侧风变为右侧风
答案:C
A. 灰白色
B. 灰色
C. 浓白色
A. 1000
B. 1200
C. 1500
D. 2000
A. 自动点火开
B. 点火A
C. 连续点火
D. 点火B
A. 失去所有的正常交流电源 loss of all normal AC generating sources
B. 失去APU发电机和失去发电机1或2 Loss of APU GEN and loss of either GEN 1 or GEN2
C. 失去交流通用汇流条1和2 Loss of AC UTIL BUS 1 and AC UTIL BUS 2
D. 交流发电机1和2不可用 AC GEN 1and AC GEN 2 not available
A. FQGC的一个通道处于激活状态 one channel of the FQGC is active.
B. FQGC持续地进行通电自测 the FQGC continuously preforms a built-in test
C. FQGC的一号通道计算燃油重量和密度,二号通道计算燃油温度 channel one of the FQGC calculates fuel weight and density and channel two calculates fuel temperature.
D. FQGC使燃油转移实现自动化the FQGC enables fuel transfer to be automatic
A. 推力手柄 Thrust levers
B. 燃油增压泵 Fuel booster pump
C. 紧急释压电门 Emer depress switch
D. 防冰电门 Anti-ice switch
A. 跑道长度; 着陆距离runway length;landing distance
B. 着陆距离; 跑道长度 landing distance;runway length
C. 刹车压力 着陆距离brake pressure; landing distance
A. 1600 米 MSL
B. 1200 米 MSL
C. 1000 米 MSL
A. 油门杆必须设置在起飞推力,机轮承重thrust levers must be set at takeoff power with weight-on-wheel
B. 扰流板控制电门在自动位置和左或右油门杆在TOGA卡位或之上位置Spoiler control switch is in AUTO and left or right thrust lever is at or above TOGA detent position
C. 扰流板控制电门在人工预位的位置和N1前推至起飞推力Spoiler control switch is in MAN ARM and N1 is advanced towards takeoff power
D. N1必须设置在起飞推力和扰流板控制电门设置在人工预位N1 must be set at takeoff power and spoiler control switch is set at MAN ARM
A. 38329
B. 38555.0
C. 34065.0
D. 32092