A、 先拉出控制手柄和旋转舱门向下到锁定位。First pull the control handle and swing the door downward into the locked position.
B、 通过按压辅助手柄触发面板弹出控制面板，拉出控制手柄且旋转舱门向下到锁定位。Eject the control handle by pressing the secondary handle trigger plate, pull the control handle and swing the door downward into the open locked position.
C、 人工打开压力释放舱门，拉出手柄且舱门自动打开。Manually open pressure relief door, pull handle and door will open automatically.
D、 从水平位置拉出旋转手柄，顺时针选择并按压舱门朝内。Pull rotating handle from its flush position, rotate clockwise and push door inward.
答案：B
A、 先拉出控制手柄和旋转舱门向下到锁定位。First pull the control handle and swing the door downward into the locked position.
B、 通过按压辅助手柄触发面板弹出控制面板，拉出控制手柄且旋转舱门向下到锁定位。Eject the control handle by pressing the secondary handle trigger plate, pull the control handle and swing the door downward into the open locked position.
C、 人工打开压力释放舱门，拉出手柄且舱门自动打开。Manually open pressure relief door, pull handle and door will open automatically.
D、 从水平位置拉出旋转手柄，顺时针选择并按压舱门朝内。Pull rotating handle from its flush position, rotate clockwise and push door inward.
答案：B
A. 应当上升到上一层高度飞向备降机场
B. 应当下降到下一层高度飞向备降机场因飞行安全高度所限不能下降到下一层高度的，应当上升至上一层高度飞向备降机场
C. 因与地面联络中断，可以保持原高度飞向备降机场，由地面管制指挥其他飞机避让
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.
A. 提供人工增压控制 provide manual pressurization control
B. 提供一个可控温度的环境 produce a temperature controlled environment
C. 控制地面活门的开和关 control the opening and closing of the ground valve
D. 控制从机身排出的空调气流流量 control the rate of conditioned air outflow from the fuselage
A. 4160 米高度上，气温-4℃，风向240°，风速15 米/秒；
B. 4800 米高度上，气温4℃，风向65°，风速24 公里/小时；
C. 4800 米高度上，气温-4℃，风向240°，风速65 公里/小时
A. 一旦出现35节机轮转动信号或机轮承重信号在5秒延迟后显示。Once a 35 knot wheel spin-up signal is present or a WOW signal after a 5 second delay.
B. 接地时。 At touchdown.
C. 一旦机轮承重信号在15秒延迟后显示。 Once a WOW signal is present after a 15 second delay.
D. 一旦出现25节机轮转动信号。Once a 25 knot wheel spin-up signal is present.
A. 气温垂直递减率
B. 大气压力
C. 标准气温和地面气温之差
