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时间:2010-09-30 22:22来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

domestic area flight information center NOTAMs office
A.25 days ago.
B.15 days ago.
C.7 days ago.
B X
91..(according to figure 2), at ZBAA, the max predicting wind
speed is___.
A. 17 m/s
28
B. 8 m/s
C. 6 m/s
A X
92.. [Refer to Figure 4-28.] What is the ground roll when
landing with 5o of flaps at a landing weight of 142,500 pounds?
A.1,750 feet.
B.2,100 feet.
C.2,500 feet.
C X
93..Which of the following is not normally a symptom of
hypoxia?
A.increased visual field
B.An increase in breathing rate
C.Sleepiness or frequent yawning
A X
94.. (Refer to Figure 6-3) The true direction of Rwy 35 at
PUDONG is
A.342o.
B.347o.
C.352o.
A X
95.. What effect would a change in air density have on
gas-turbine-engine performance?
29
A.As air density decreases, thrust increases.
B.As air density increases, thrust increases.
C.As air density increases, thrust decreases.
B X
96. When is DME required for an instrument flight?
A.At or above 24000 feet MSL if VOR navigational equipment is
required
B.In terminal radar service areas
C.Above 12,500 feet MSL
A X
97. . (Refer to Figure 6-2) Which approach lighting is
available for ILS/DME Rwy 36L?
A.HIALS with PAPI.
B.HIALS.
C.PAPI.
A X
98.. (According to Figure 1) which station reports the max wind
speed
A.ZSSS
B.ZUUU
C.ZWWW
C X
99.What is a characteristic of longitudinal instability?
30
A.Pitch oscillations becoming progressively greater.
B.Bank oscillations becoming progressively greater.
C.Aircraft constantly tries pitch down.
A X
100.. (Refer to Figure 6-3, 6-4) What distance is available for
takeoff on Rwy 17 at PUDONG?
A.12,093 feet.
B.12,097 feet.
C.13,123 feet.
C X
101..Crew resource management is a process using all
available information and resources, i.e. equipment,
procedures and people, to achieve a safe and
A.(续正文,efficient flight operation. The statement is)right
B.wrong
A X
102.. [Refer to Figure 4-41.] What is the approximate landing
weight for Operating Conditions below? WEIGHT (START TO ALT):
87,000,DISTANCE (NM): 370,WIND COMPONENT: 60HW,HOLDING
TIME AT ALT (MIN): 15
A.80,850 pounds.
B.85,700 pounds.
C.77,600 pounds.
31
A X
103..(Refer to Figure 1) What weather condition is reported at
Urumchi (ZWWW)
A. Strong wind with shower
B. Snow and rain
C. Strong west wind and blowing snow
C X
104.. [Refer to Figure 4-28 and 4-29.] What approach speed and
landing distance will be needed when landing at a weight of
140,000 pounds with 15o of flaps?
A.123 knots and 3,050 feet.
B.138 knots and 3,050 feet.
C.153 knots and 2,050 feet.
B X
105.If a required instrument on a multiengine airplane
becomes inoperative, which document dictates whether the
flight may continue en route?
A. An approved Minimum Equipment list for the airplane.
B. Original dispatch release.
C. Certificate holder's manual.
C X
106.. [Refer to Figure 4-34.] What are the recommended IAS and
EPR settings for holding under Operating Conditions
32
below? ,ALTITUDE: 30,000,WEIGHT (*1000): 92.5,ENGINES
OPERATING: 2,HOLDING TIME (MIN): 10
A.221 knots and 1.83 EPR.
B.210 knots and 1.69 EPR.
C.217 knots and 1.81 EPR.
B X
107.. How often is SNOWTAM broadcast to distant centers?
A.Hourly.
B.One hour and a half a time.
C.30 minutes a time.
A X
108..When light passes through the lens it is brought to focus
at the back of the eyeball on the
A.retina
B.cornea
C.iris
A X
109..When is the course deviation indicator (CDI) considered
to have a full-scale deflection?
A.When the CDI deflects from full-scale left to full-scale
tight, or vice versa.
B.When the CDI deflects from the center of the scale to
full-scale left or right.
33
C.When the CDI deflects from half-scale left to half-scale
right, or vice versa.
B X
110..Effective CRM has some characteristics, which of the
following is right description about it?
A.CRM is a process using all available information and
resources, i.e. equipment, procedures and people, to achieve a
safe and efficient flight operation.
B.CRM can be blended into all forms of aircrew training
C.A and B
C X
111.. [Refer to Figure 4-25.] What is the maximum landing
weight which will permit stopping 1,500 feet short of the end
of a 4,950-foot dry runway with reversers and spoilers
 
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