A、 The cover title shall be "Pilot＇s Operating Handbook" or "Pilot＇s Operating Handbook and FAA Approved Airplane Flight Manual".
B、 The topic cover shall be "Pilot＇s Controlling Manual" or "Pilot＇s Controlling Manual and FAA Accepted Airplane Flight Manual".
C、 The page topic shall be "Pilot＇s Managing Handbook" or "Pilot＇s Managing Handbook and FAA Authorized Airplane Flight Manual".
答案：A
A、 The cover title shall be "Pilot＇s Operating Handbook" or "Pilot＇s Operating Handbook and FAA Approved Airplane Flight Manual".
B、 The topic cover shall be "Pilot＇s Controlling Manual" or "Pilot＇s Controlling Manual and FAA Accepted Airplane Flight Manual".
C、 The page topic shall be "Pilot＇s Managing Handbook" or "Pilot＇s Managing Handbook and FAA Authorized Airplane Flight Manual".
答案：A
A. 数据库更新正在等待中。
B. 数据库同步正在进行中。
C. 数据库升级正在按顺序进行。
A. 描述飞机电源系统时，应提供相关限制、警告和操作提示。
B. 描述飞机电源系统时，应解释相关束缚、警示和操作提示。
C. 描述飞机电源系统时，应提供相关限制、警告和操作警示。
A. The EEC processes the simulated signal from the fuel filter differential pressure bulb.
B. The fuel filter differential pressure sensor sends an modulated signal to the EEC.
C. The EEC receives the analog signal from the fuel filter differential pressure switch.
A. 将要测试的这个系统在上个航段运转不正常。
B. 该系统要测试上一航段的不正常运行。
C. 在上一航段里该系统被测试为运行不正常。
A. The localizer beam is aligned with the centerline of the runway.
B. The localizer way is misaligned with the centerline of the runway.
C. The localizer course is aligned with the centerline of the runway.
A. Each of the two life vests located at L2 entry door flight crew station is damaged.
B. Each of the two life vests located at L2 entry door flight crew station is out of time limit.
C. Each of the two life vests located at L2 entry door flight crew station is out of service.
A. 残留在零件上的溶剂会导致腐蚀。
B. 残留在零件上的油液会导致腐蚀。
C. 残留在零件上的溶剂会导致穿孔。
A. “力臂”是物体重心到基准面的水平距离。
B. “力臂”是物体重心到参考面的垂直距离。
C. “力矩”是物体中心到参考基准面的距离。
A. 提高温度以缩短固化时间。
B. 提高温度以缩短治疗时间。
C. 降低温度以增加固化时间。
A. AIRBORNE AUXILIARY POWER UNITS are those power plants (engines) built-in on the aircraft for creating and supplying power in a single type or combination of auxiliary electric, hydraulic, pneumatic or other power.
B. AIRBORNE AUXILIARY POWER UNITS are those units (engines) that are suspended on the aircraft for bringing and providing power in a single manner or combination of auxiliary electrical, hydraulic, pneumatic, or other power.
C. AIRBORNE AUXILIARY POWER UNITS are those airborne power plants (engines) which are installed on the aircraft for the purpose of generating and supplying a single type or combination of auxiliary electric, hydraulic, pneumatic or other power.
