判断正误True or False: 如果入侵飞机无运行的方式 S 应答机，TCAS 系统不提供交通冲突的指示。The TCAS system provides no indication of traffic conflicts if the intruder airplane is without an operative Mode ＇S＇ transponder.

A. 任一ACP上的扬声器音量旋钮。With the speaker volume knob on either ACP

B. 其它测试面板上的HI/LO电门。With the HI/LO switch on the miscellaneous test panel

C. 自动地，双发运转。Automatically, with the engines running

D. 无法被调整。It cannot be adjusted

A. ECS简图页ECS synoptic page

B. 状态页 Status page

C. 交流电源简图页 AC ELECTRICAL synoptic page

D. 主页 Primary page

E. 飞行操纵简图页 FLIGHT CONTROLS synoptic page

F. 液压简图页 HYDRAULIC synoptic page

G. 直流电源简图页 DC ELECTRICAL synoptic page

A. 180 kts

B. 250kts

C. 0.45 Mach

D. 0.40 Mach

A. 有雷暴活动的锋面附近

B. 海陆交界地区

C. 空中冷平流较强的地区

A. 活跃的冷锋

B. 成熟的气旋

C. 高空槽

A. 打开航行灯和滑行灯,用慢速滑行；

B. 在引导车的引导下滑行；

C. 用慢车速度滑行

A. 所有简令和检查单已完成 All briefings and checklists have been completed.

B. 飞机处于正确的飞行航径 The plane is on the correct flight path.

C. 推力调定与飞机的形态相适应 Thrust setting is compatible with the aircraft configuration.

D. 飞机未建立正确的着陆形态 The aircraft did not establish the correct landing configuration.

A. 防冰和漏气探测器（AILC）探测到左侧引气管道引气泄露。 A bleed air leak detected by AILC in the left bleed ducting.

B. 防冰和漏气探测器（AILC）探测到右侧引气管道引气泄露。 A bleed air leak detected by AILC in the right bleed ducting.

C. 引气泄露后引气关闭且系统未选择关闭。Bleed shutdown after bleed leak and system not selected off.

D. 在通电自检测试中（PBIT），左引气管路的漏气双探测环路失效。 Loss of both leak detection loops in left bleed ducting during PBIT.

A. CBFA

B. CDFA

C. CFP

D. EFB