露点的定义是

A. 意味着N1或者N2转速超过了红区4秒以上Indicates that N1 or N2 has exceeded redline for more than four seconds.

B. 意味着相对应的发动机失效，FADEC系统无法成功重新起动对应的发动机，并且油门杆没有在关断位Indicates flameout of respective engine, FADEC was not successful with re−light and thrust lever not at shut−off.

C. 意味着对应的油门杆失效，FADEC将会继续保持最后一次的推力设定直到进近Indicates failure of respective thrust lever. FADEC will maintain last power level setting until approach.

D. 意味着相对应的操作引气活门无法关闭Indicates that respective operability bleed valve has failed closed.

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. 机身后机腹；the backward belly of the fuselage

A. L BLEED DUCT

B. ANTI-ICE DUCT

C. L BLEED LOOP

D. R BLEED DUCT

A. 3 米／秒；

B. 12 米／秒；

C. 10 米／秒

A. 大气和地面的摩擦

B. 同一平面上的不同气压

C. 锋面的移动

A. 主起落架和前起落架的排序sequencing of the main and nose landing gear

B. 前轮转弯Nosewheel steering

C. 主起落架舱门Main landing gear doors

D. 防滞刹车系统Anti-skid braking system

A. 10

B. 8.0

C. 12.0

D. 6

A. 小于90 less than 90

B. 小于120度 less than 120

C. 小于 100度 less than 100

A. 失速Stall

B. 风切变Windshear

C. 低于下滑道Below glideslope

D. 过大接近率Excessive closure rate

A. 遮光板上主警告灯亮 Master warning switch light illuminates on glare-shield;

B. 遮光板上的 APU 火警灯亮 APU FIRE PUSH button illuminates on glare-shield;

C. ED1 显示 APU FIRE 红色警告信息并伴有语音 APU FIRE red warning message displayed on ED1 accompanied with a voice;

D. 如果 APU 正在运转，APU 自动关车，APU 电源自动断开 If APU is working, APU will shut down automatically, APU power will be off automatically.