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時間:2010-10-01 06:59來源:藍天飛行翻譯 作者:admin
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A: 45 minutes at normal cruising fuel consumption.
B: The fuel required to fly to the alternate, plus 10 percent.
C: 3 hours at normal cruising fuel consumption.
169 題目: Empty Field Myopia is the tendency of the ciliary muscle to
relax when there are no close objects in the field of view
A:This causes the eye to take up a focal length of approximately)one
to two meters
B: five meters
C: infinity
170 題目:What is the hijack code?
A: 7200.
B: 7500
C: 7777.
171 題目: In addition to the localizer; glide slope; marker beacons;
approach lighting and HIRL, which ground components are required to
be operative for a category II instrument approach to a DH below 150
feet ACL??
A: TDZL;RCLS and RVR;
B:RCLS and REIL;
C:Rader and RVR
172 題目: To make all the route aircraft have the same zero altitude, the
altimeter should set on .
A: the standard air pressure of the mean sea level
B: the standard air pressure of the local station
C: the standard air pressure of the calibrated sea level
173 題目: Which maximum range factor increases as weight decreases?
A:Angle of attack
B: Altitude
C: Airspeed
174 題目:When must an air carrier airplane be DME equipped?
A: In class e airspace for all IFR or VFR on top operations
B:Whenever VOR navigational receivers are required
C: For flights at or above FL 180
175 題目:what weather is predicted by the term Vcts in a TAF
A: between 5 and 25 km
B:within 50 km
C: TS are expected in the vicinty
176 目:When a pilot plans a flight using NDB NAVAIDS. Which rule
applies?
A:The airplane must have sufficient fuel to proceed. by means of VOR
NAVIDS,to a suitable airport and land
B: The pilot must be able to return to the departure airport using
other navigation radios.
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C:The airplane must have sufficient fuel to proceed, by means of VOR
NAVAIDS, to a suitable airport and complete an instrument approach by
use of the remaining airplane radio system.
177 題目:During the life cycle of a thunderstorm, which stage is
characterized predominately by downdrafts?
A: cumulus
B: dissipating
C:mature
178 題目: [Refer to Figures 4-22, and 4-24.] What is the go-around EPR
for Operating Conditions L-3?
A: 2.06 EPR.
B: 2.07 EPR
C: 2.09 EPR
179 題目:What conditions are indicated on a weather depiction chart
A: Forecast ceiling & visibilities over a geographic area
B: actual en route ……
C: actual sky cover……
180 題目: Carbon monoxide is dangerous because
A: it displace oxygen from the blood‘s red cells
B: it is highly acidic and attacks the lining of the lungs
C: it displaces oxygen from the lungs causing suffocation
181 題目:Which of the following is considered an auxiliary flight control?
A:Ruddervator
B:Upper rudder
C: Leading-edge flaps
182 題目: What factor is the demonstrated all engines take off distance
increase to determine a TODR
A: 1.15
B: 1.2
C: 2
183 題目: If an engine failure occurs at an altitude above single-engine
ceiling, what airspeed should be maintained?
A:VMC.
B: VYSE.
C: VXSE.
184 題目:Which operational requirement must be observed by a
commercial operator when ferrying a large, three-engine,
turbojet-powered airplane from one facility to another to repair an
inoperative engine?
A: The Airplane Flight Manual must include procedures and
performance data which allow for the safe operation of such a flight.
B: The existing and forecast weather for departure, en route, and
approach must be VFR.
C: Some passengers may be carried.
185 題目: The horizontal wind shear critical for turbulance per 150 miles
is
23
A: 18 knots or less
B: greater than 18 knots
C: not a factar

21
186 題目: Freezing Point Depressant (FPD) fluids used for deicing
A: provide ice protection during flight.
B: are intended to provide ice protection on the ground only.
C: on the ground, cause no performance degradation during takeoff.
187 題目:What effect will an increase in altitude have upon the available
equivalent shaft horsepower (ESHP) of a turboprop engine?
A: Lower air density and engine mass flow will cause a decrease in
power.
B:Higher propeller efficiency will cause an increase in usable power (ESHP) and
thrust.
C: Power will remain the same but propeller efficiency will decrease.
188 題目: (Refer to Figure 6-3) The magnetic direction of Rwy 17 at PUDONG is
A: 162o
B: 172o
 
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