A、 襟翼收上到位; Flaps retracted up and in position;
B、 起落架收上到位; Landing gear retracted up and in position;
C、 IAS≥VT或200KIAS（以较大者为准）; IAS≥VT or 200KIAS （which is higher ）;
D、 到达高度3000ft. Reaching altitude of 3000ft.
答案：ABC
A、 襟翼收上到位; Flaps retracted up and in position;
B、 起落架收上到位; Landing gear retracted up and in position;
C、 IAS≥VT或200KIAS（以较大者为准）; IAS≥VT or 200KIAS （which is higher ）;
D、 到达高度3000ft. Reaching altitude of 3000ft.
答案：ABC
A. 着陆时下沉率过大。An excessive sink rate is encountered on landing
B. 飞机低于下滑道2个点。The aircraft is 2 dots below the glideslope
C. 在刚起飞后或复飞过程中，飞机掉高度。Aircraft altitude decreases immediately after takeoff or during a missed approach
D. 进近时起落架放下和襟翼收上。On approach with the gear down and flaps up
A. 左和右推力手柄≤IDLE (慢车)位。L and R thrust lever≤IDLE.
B. 左侧和右侧主起落架承重（4秒）。L and R MLG WOW (4 sec).
C. 下列2个条件中任意1个: 机轮速度＞16节或无线电高度＜10英尺（3秒）。Any 1of the following 2 conditions: wheel speed＞16kt (3 sec), or radio altitude＜10ft (3 sec).
D. 左或右推力手柄≤IDLE (慢车)位。L or R thrust lever≤IDLE.
A. 增长
B. 缩短
C. 保持不变
A. 后设备舱的引气管路 bleed air ducting in the aft equipment bay
B. 中央机身的防冰管路 anti-ice ducting in the center fuselage
C. 发动机吊架的整流罩防冰管路 cowl anti-ice ducting in the engine pylons
D. 空调引气管路air conditioning bleed air ducting
A. 1
B. 3
C. 4
D. 5
A. 查阅MEL，并与机务人员沟通确认符合放行标准。Refer to MEL and communicate with maintenance personnel to confirm that they meet the release standards;
B. 查阅MEL，可以不与机务人员沟通确认符合放行标准。Refer to MEL and may not communicate with maintenance personnel to confirm whether meet the release standards;
C. 不用确认机务人员按照MEL执行维护程序（M）（如有）；Don＇t need to verify the maintenance personnel conducting the maintenance procedures (M) as per MEL (if any);
D. 不用与机组成员预习MEL的操作程序（O）（如有）；Don＇t need to preview MEL operation procedures (O) (if any) together with the flight crew members;
A. 30 800
B. 120 800
C. 30 1600
D. 120 1600
A. 在飞行的所有高度和所有阶段。At all altitudes and phases of flight
B. 仅当起落架放下时Only when the gear is down
C. 仅当起落架和襟翼放下时 Only with the gear and flaps down
D. 在起飞和着陆阶段 During the take-off and landing phases
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.
A. 客舱门或勤务门被打开 passenger door or service door is open
B. 电子设备舱打开 avionics bay door is open
C. 客舱门或勤务门关闭 passenger door or service door is closed
D. 电子舱门关闭 avionics bay door is closed
