ADG放出后将给下列哪个服务组件供电？After deployment, which service component of the following will be supplied power from ADG?

所需目视参考(required visual reference): 飞行员应该看到 目视助航设施的一部分或进近区的一部分，并有充分时间让飞行员评 估航空器相对于预定飞行航径的位置和位置变化率。在盘旋进近中， 所需的目视参考是跑道周围的物体。Required visual reference: The pilot should see part of the visual navigation aids or part of the approach area, and have sufficient time for the pilot to evaluate the position and position change rate of the aircraft relative to the predetermined flight path. In circling approach, the required visual references are the objects around the runway.

判断正误： L 或 R IGN A or B FAULT 状态信息（白色）表明一套点火系统故障。True or False:L or R IGN A or B FAULT status (white) Indicates a fault in the respective ignition driver.

判断正误True or False：如果任一空调组件失效，剩余的组件将向驾驶舱和客舱供气，但供气量减少。Should a single pack fail, the remaining pack can supply conditioned air to both compartments but at a reduced volume.

起飞时，PF按压TOGA电门，报出：“（ ）”。For takeoff, the PF presses TOGA switch, calls out：“( )”.

A. TO/TO 两个，起飞; Two TO/TO， takeoff;

B. TO/TO 两个，形态OK; Two TO/TO， CONFIG OK;

C. 起飞; Takeoff;

D. TO/TO 两个，形态OK，起飞. Two TO/TO， CONFIG OK, takeoff.

如果选择N1风扇同步，则右发N1值的差异必须在什么范围？For N1 synchronization to be enabled, the right engine N1 must be within ___%

A. a)         相对于左发N1差异在1.1% 1.1% of the left engine N1.

B. b)        相对于左发N1差异在1.3% 1.3% of the left engine N1.

C. c)         相对于左发N1差异在1.5% 1.5% of the left engine N1.

执行低能见起飞程序和模拟低能见起飞时（ ）。When carrying out low visibility takeoff procedure or simulating low visibility takeoff, ( ).

A. 可以使用一般起飞方式 Common takeoff methode can be used

B. 只能滑跑起飞 Only rolling take off

C. 无起飞方式要求 No requirement to takeoff methode

D. 只能静止起飞 only static takeoff is allowed

具有卫星功能的应急定位发射机（ELT）发射标准扫频音在：The satellite capable emergency locator transmitter (ELT) transmits a standard swept tone on:

A. 121.5 MHz

B. 243.0 MHz

C. 406.0 MHz

D. 以上全部All of the above

某飞行员在低空飞行时发现前方的云十分高大，云底阴暗混乱，起伏明显并呈滚轴状，他可以断
定，前方的云是＿＿

A. 碎积云

B. 积雨云

C. 浓积云

通电时，APU燃油泵的燃油来源于：when energized, the APU fuel pump source of fuel is from the:

A. 从中央油箱到APU center tank to the APU

B. 左和右燃油箱 right and left fuel tanks

C. 左和中央燃油箱 left and center fuel tanks

D. 左集油箱 left collector tank

飞行状态下满足以下哪些条件时，刹车温度信息将会从状态页移除：1.BTMS指示正常2.襟翼收上3.起落架收上并锁定。During flight, the brake temperature information is removed from the status page if conditions of the following is met: 1. BTMS indications are normal. 2. The flaps are up. 3. Landing gear is up and locked.

A. 1，2

B. 2，3

C. 1，2，3

D. 1，3