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时间:2010-09-30 22:39来源:蓝天飞行翻译 作者:admin
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A.As air density decreases, thrust increases.
B.As temperature increases, thrust increases.
C.As temperature increases, thrust decreases.
C X
21..What effect does an increase in airspeed have on a
coordinated turn while maintaining a constant angle of bank
an altitude?
A.The rate of turn will decrease resulting in a decreased load
factor.
B.The rate of turn will increase resulting in an increased
load factor.
C.-The rate of turn will decrease resulting in no changes in
load factor.
C X
22..What effect does an uphill runway slope have upon takeoff
performance?
A.Increases takeoff distance.
B.Decreases takeoff speed.
C.Decreases takeoff distance.
A X
23..What effect does high relative humidity have upon the
maximum power output of modern aircraft engines?
A.Neither turbojet nor reciprocating engines are affected.
B.Reciprocating engines will experience a significant loss
of BHP.
C.Turbojet engines will experience a significant loss of
thrust.
B X
24..What effect does landing at high elevation airports have
on ground speed with comparable conditions relative to
temperature, wind, and airplane weight?
A.Higher than at low elevation.
B.Lower than at low elevation.
C.The same as at low elevation.
A X
25..What effect does landing at high temperature have on
ground speed with comparable conditions relative to airport
elevation, wind, and airport elevation?
A.Higher than at low temperature.
B.Lower than at low temperature.
C.The same as at low temperature.
A X
26..What effect does landing with increased weight have on
ground speed with comparable conditions relative to
temperature, wind, and airport elevation?
A.Higher than at low weight.
B.Lower than at low weight.
C.The same as at low weight.
A X
27..What does the term of Equivalent shaft horsepower (ESHP)
of a turboprop engine describe?
A.shaft horsepower and jet thrust.
B.jet thrust only.
C.propeller thrust only.
A X
28..What does the throttle opening of a
turbo-charged-reciprocating engine control?
A.Supercharger gear ratio.
B.Exhaust gas discharge.
C.The desired manifold pressure.
C X
29..What effect, if any, does high ambient temperature have
upon the thrust output of a turbine engine?
A.Thrust will be reduced due to the decrease in air density.
B.Thrust will remain the same, but turbine temperature will
be higher.
C.Thrust will be higher because more heat energy is extracted
from the hotter air.
A X
30..What effective runway length is required for a
turbojet-powered airplane at the destination airport if the
runways are forecast to be wet or slippery at the ETA?
A.70 percent of the actual runway available, from a height
of 50 feet over the threshold.
B.115 percent of the runway length required for a dry runway.
C.115 percent of the runway length required for a wet runway.
B X
31..What indicates that a compressor stall has developed and
become steady?
A.Strong vibrations and loud roar.
B.Occasional loud "bang" and flow reversal.
C.Complete loss of power with severe reduction in airspeed.
A X
32..What is an area identified by the term "clearway"?
A.centrally located about the extended centerline and under
airport authorities, which does not contain obstructions and
can be considered when calculating takeoff performance.
B.An area, at least the same width as the runway, capable of
supporting an airplane during a normal takeoff.
C.An area beyond the takeoff runway, which is able to support
the airplane, for use in decelerating the airplane during an
aborted takeoff.
A X
33..What is an area identified by the term "stopway"?
A.An area, at least the same width as the runway, capable of
supporting an airplane during a normal takeoff.
B.An area designated for use in decelerating an aborted
takeoff.
C.An area, not as wide as the runway, capable of supporting
an airplane during a normal takeoff.
B X
34..What is the best method of speed reduction if hydroplaning
is experienced on landing?
A.Apply full main wheel braking only.
B.Apply nosewheel and main wheel braking alternately and
abruptly.
C.Apply aerodynamic braking to the fullest advantage.
C X
35..What is the correct symbol for minimum unstick speed?
A.VMU.
B.VMD.
C.VFC.
A X
36..What is the correct symbol for takeoff decision speed?
A.V2.
B.V1.
C.VLOF.
B X
37..What is the correct symbol for the Minimum Control Speed,
 
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