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B： not change
C：may change or may not change
1093 題目：Which procedural is recommended to prevent or overcome spatial
disorientation?
A： Reduce head and eye movement to the greatest possible extent.
B： Rely on the kinesthetic sense.
C： Rely entirely on the indications of the fl ight instruments.
1094 題目： What is the recommended technique to counter the loss of airspeed and
resultant l i ft from wind shear?
A：avoid overstressing the aircraft pitch to airspeed and apply maximum power
B： lower the pitch attitude and regain lost airspeed
C：maintain or increase pitch attitude and accept the lower-than-normal
airspeed indicatiors
1095 題目：Which weather condition is present when the tropical storm is upgraded
to a hurricane?
A： a clear eare or hurricane eye has formed;
B： sustained winds of 65kt or more;
C： highest wind speed locokt or more;
1096 題目：What ef fect, i f any, does high ambient temperature have upon the thrust
output of a turbine engine?
A： Thrust wi l l be reduced due to the decrease in air density.
B： Thrust wi l l remain the same, but turbine temperature wi l l be higher.
C：Thrust wi l l be higher because more heat energy is extracted from the hotter air.
1097 題目：Where is the critical altitude of a supercharge-reciprocating engine?
A： the altitude at which maximum al lowable BMEP can be obtained;
B： the highest altitude at which a desired mani fold pressure can be obtained;
C： highest altitude where the mipfure can be leaned to best power ratio;
1098 題目：(Refer to Figure 6-4) For an aircraft of Category D with 4 turbo-powered
engines, what is the takeof f minimum for Rwy 17 at PUDONG with HIRL and CL
operating?
119
A： RVR 300m.
B： RVR 400m.
C： RVR 250m.
1099 題目： Night vision is enhanced by
A： looking sl ightly to one side of the object you wish to view
B： fixing your gaze director on the object you wish to view.
C： ensuring that the cockpit remains brightly i lluminated
1100 題目： [Refer to Figure 4-28.] How much wi l l landing distance be reduced by
using 15o of f laps rather than 0o f laps at a landing weight of 115,000 pounds?
A： 500 feet.
B： 800 feet.
C： 2,700 feet.
1101 題目：Assuming that al l ILS components are operating and the required visual
references are not required, the missed approach should be initiated up on
A： Arrival at the visual descent point
B： Expiration of the time l isted on the approach chart for missed approach
C： Arrival at the DH on gl ide slope
1102 題目： Ⅲ A minmum
A： DH 50 feet and RVR 350m
B： RVR 300m
C： RVR 200m
1103 目： Before plates in wing fuel cells prevent
A： Fuel coving frond our tank to another during turbulent f l ight
B： Over pressure in the fuel tank
C：movement of the fuel (cruising) in the tank during
acceleration/deceleration and in turbulent
1104 題目：Which wind-shear condition results in an increase in airspeed?
A： Increase tailwind wind and decreasing headwind.
B： Headwind or tai lwind increase
C： Increasing headwind and decreasing tai lwind.
1105 題目：Which type jet stream can be expected to cause the greater turbulence
A： A jet stream associated whither wide isotherm spacing
B： A straight jet stream associated with a high-pressure ridge
C： A curring jet stream associated with a deep low pressure through
1106 題目：What is the advantage of HIRL or MIRL on an IFR runway as compared
to a VFR runway?
A： Lights are closer together and easi ly distinguished from surrounding l ights
B： Amber l ights replace white on the last 2,000 feet of runway for a caution
zone
C： Alternate red and white l ights replace the white on the last 3,000 feet of
runway for caution zone
1107 題目： (Refer to Figures 2-4 and 2-5)To which aircraft position does HSI
presentation ”A” correspond?
A： 9and6
B： 9 only
C： 6 only
1108 題目： The bottom of the Class B airspace is appropriate to
A： FL 6,300m.
120
B： FL 6,000m.
C： FL 600m.
1109 題目： At what maximum indicated airspeed can a reciprocating-engine
airplane operate in the airspace underlying Class B airspace?
A： 180 knots.
B： 200 knots.
C： 230 knots.
1110 題目：En route at FL270, the altimeter is set correctly. On descent, a pi lot fai ls
to set the local altimeter setting of 30.57.If the field elevation is 650feet,and the
altimeter is functioning properly, what wi l l it indicate upon landing?
A： 585feet
B： 1.300feet
C： Sea level
1111 題目： (Refer to Figure 2-13) What is the runway distance remaining at "B" for
　
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