A、 液压泵1A,2B,和3A；hydraulic pumps 1A,2B, and 3A;
B、 液压泵2A,2B,和3A；hydraulic pumps 2A,2B, and 3A;
C、 液压泵1B,2B,和3B；hydraulic pumps 1A,2B, and 3B;
D、 液压泵1B,2B,和3A；hydraulic pumps 1A,2B, and 3A;
答案：D
A、 液压泵1A,2B,和3A；hydraulic pumps 1A,2B, and 3A;
B、 液压泵2A,2B,和3A；hydraulic pumps 2A,2B, and 3A;
C、 液压泵1B,2B,和3B；hydraulic pumps 1A,2B, and 3B;
D、 液压泵1B,2B,和3A；hydraulic pumps 1A,2B, and 3A;
答案：D
A. 大气数据基准面板air data reference panel
B. 飞行控制面板Flight control panel
C. 显示转换面板Reversionary display panel
D. 显示控制面板Display control panel
A. 首先
B. 最后
A. 根据实际地速计算一个下降率
B. 根据下降率表中的地速使用插值法计算出所需要的下降率
C. 根据飞机地速在下降率表中所处的范围，向上选取下降率
A. 14.0
B. 18.0
C. 23.0
D. 27.0
A. 飞机全重小于或等于最大着陆重量（MLW）时，垂直下降率大于600 英尺每分钟或10 英尺每秒的着陆 A landing at a vertical descent rate greater than 600 feet per minute or 10 feet per second when the airplane gross weight is less than or equal to the maximum landing weight (MLW);
B. 飞机全重大于最大着陆重量（MLW）但小于或等于最大 起飞重量（MTOW），垂直下降率大于360 英尺每分钟 或6 英尺每秒的着陆；A landing at a vertical descent rate greater than 360 feet per minute or 6 feet per second when the airplane gross weight is greater than the maximum landing weight (MLW), but less than or equal to the maximum take-off weight (MTOW);
C. 飞机在一条可用的跑道表面侧滑，或着陆时发生不能控 制的侧滑并且从可用的跑道表面移动到不可用的跑道 的着陆； A landing where the airplane lands with an uncontrolled sideways skid or continues to move from the applicable runway surface to a runway surface that is not applicable;
D. 以上全部above all
A. 确认在NAV源旋钮上选择的有效NAV源。 identify valid NAV sources selected at the NAV source knob
B. 计算从大气数据及姿态/航向计算机上获取的输入从而去测试转换控制的可用性。Calculate inputs from air data and attitude/heading computer to test the availability of reversionary control
C. 确保AHRS（使用IRS作为航道）校准完成。Ensure AHRS (use IRS for metric course）alignment is complete
D. 确保同样的数据同时显示给两位飞行员。Ensure that the same data is shown to both pilots
A. 积状云和阵雨；
B. 雾和毛毛雨；
C. 层状云和连续性降水
A. 30, 30
B. 20, 30
C. 25, 30
D. 20, 20
A. 运输航空严重征候
B. 运输航空一般征候
C. 通用航空征候
D. 运输航空地面征候
