A、 GET INTO
B、 GO INTO
C、 ENTER
答案:B
A、 GET INTO
B、 GO INTO
C、 ENTER
答案:B
A. Copy density should be the same throught the page.
B. Copy density must be different throught the page.
C. Density of copy must be different throught the page.
A. 封面上包含的信息将由制造商自行决定
B. 封面左侧上包含的信息将由制造商自行选择的
C. 封面左侧上包含的信息将由制造商自行设计的
A. You can use electric motors to drive fuel and hydraulic pumps or to
drive a valve to the commanded position in the fuel,hydraulic or air
conditioning system or to move doors and cargo containers.
B. Electric motor can drive fuel and hydraulic pumps or drive a valve to
the commanded position in the fuel,hydraulic or air conditioning system
or move mechanical parts like doors and cargo containers to produce
mechanical power.
C. Electric motor produce mechanical power and their main functions are
to drive fuel and hydraulic pumps,to drive a valve to the commanded
position and to move mechanical parts like doors and cargo containers.
A. The bolts are on the opposite side of the flange.
B. The bolts are on the rear side of the flange.
C. The bolts are on the across side of the flange.
A. If the airplanes mentioned in the document are no more manufactured,
B. 、Unless the airplanes shown in this document are not produced any more,
C. 、Even if the airplanes covered in this document are no longer produced,
E. ven if the airplanes covered in this document are no longer produced,
A. Maneuvering Speed is the maximum speed what required of full uncommitted
aerodynamic control will not exceed the airplane.
B. Maneuvering Speed is the largest speed that the aerodynamic application
by the full available control will not cause the aircraft overexert.
C. Maneuvering Speed is the maximum speed at which application of full
available aerodynamic control will not overstress the airplane.
A. REACH
B. STRETCH
C. EXTEND
A. does not permitted to
B. not permitted to do
C. permit to do
A. 液位计带有一个 80 立方厘米的透明腔体。
B. 液位计带有一个 80 立方厘米的转换腔体。
C. 液位计带有一个 80 立方厘米的次级腔体。
A. 真实空速是飞机相对于未受扰动的空气的空速,是根据高度、温度和压缩性
修正的 CAS。
B. 真实空速是飞机相对于稳定的空气的空速,是根据姿态、温度和膨胀性修正
的 CAS。
C. 真实空速是飞机相对于未受扰动的空气的空速,是根据高度、温度和调节性
修正的 CAS。