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时间:2010-09-30 22:22来源:蓝天飞行翻译 作者:admin
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engines operating.
B X
289..Who is responsible for the issue of SNOWTAM?
A.ATMB NOTAMs office.
B.Area flight information center.
C.Airport flight information office.
C X
290..Deference is one of the "hazardous thoughts" which affect
human behavior and decision making. It refer to
A.the tendency to resist authority and object to regulation
B.the tendency to believe that "it can not happen to me"
C.the tendency to blame another person or circumstance for
whatever goes wrong
C X
291..The kinds of operation that a certificate holder is
88
authorized to conduct are specified in the
A.certificate holder's operations specifications.
B.application submitted for an Air Carrier or Operating
Certificate, by the applicant.
C.Air Carrier Certificate or Operating Certificate.
A X
292..One of the effects of hypoxia is a degradation of night
vision. This effect begins at about
A.5000 feet
B.10000 feet
C.8000 feet
A X
293..For an airport with only one set of VOR approach, if the
applicable instrument visibility minimum is 2,000 meters, it
may be listed as an alternate airport only when the visibility
is forecast to be at least
A.3000m.
B.3,600m.
C.2,800m.
B X
294..During a supplemental air carrier flight, who is
responsible for obtaining information on meteorological
conditions?
89
A.Aircraft dispatcher.
B.Pilot in command.
C.Director of operations or flight follower.
B X
295..A dispatch release for a flag or domestic air carrier must
contain or have attached to it
A.minimum fuel supply and weather information for the
complete flight.
B.trip number and weight and balance data.
C.weather information for the complete flight and a crew list.
A X
296..An air carrier may schedule a pilot, on a four-pilot crew
(including a second-in-commander pilot), for flight deck
duty during any 24 consecutive-hour period for not more than
A.17 hours
B.24 hours
C.25 hours
A X
297..(Refer to Figure 7) Flying from Kunming to Chengdu, which
weather system we would encounter
A. A worm front and mountain waves
B. A cold front and moderate icing
C. A stationary front and a upper jet
90
C X
298..[Refer to Figure 4-41.] What is the approximate landing
weight for Operating Conditions below? WEIGHT (START TO ALT):
77,000,DISTANCE (NM): 70,WIND COMPONENT: 25TW,HOLDING TIME
AT ALT (MIN): 15
A.74,000 pounds.
B.74,180 pounds.
C.73,400 pounds.
A X
299..Which information must be contained in, or attached to,
the dispatch release for a flag air carrier flight?
A.Type of operation (e.g., IFR, VFR), trip number.
B. Total fuel supply and minimum fuel required on board the
airplane.
C.Passenger manifest, company organization name, and cargo
weight.
A X
300..Which equipment requirement must be met by an air
carrier that elects to use a dual inertial Navigation System
(INS) on a proposed flight?
A.The dual system must consist of two operative INS units.
B.A dual VORTAC/ILS system may be substituted for an
inoperative INS.
91
C.Only one INDS is required to be operative, if a Doppler Radar
is substituted for the other INS.
C X
301..(Refer to Figure 6-1) When the aircraft is intercepting
R-188 HUR with an intercept angle of 45o during go-around,
how much is the intercept heading?
A.143o.
B.233o.
C.53o.
A X
302..If a received ATC clearance seems to be conflict to a
regulation, the pilot should
A.Do not accept the clearance.
B.Read the clearance back entirely.
C.Request a clarification from the ATC immediately.
C X
303..Airflow separation over the wing can be delayed by using
vortex generators.
A.Directing high pressure air over the top of the wing or flap
through slots and making the wing surface smooth.
B.Directing a suction over the top of the wing or flap through
slots and making the wing surface smooth.
C. Making the wing surface rough and/or directing high
92
pressure air over the top of the wing or flap through slots.
C X
304..At what minimum speed (rounded off) could dynamic
hydroplaning occur on main tires having a pressure of 110
PSI?
A.90 knots.
B.95 knots.
C.100 knots.
B X
305..The minimum speed during takeoff, following a failure of
the critical engine at VEF, at which the pilot may continue the
takeoff and achieve the required height above the takeoff
surface within the takeoff distance, is indicated by symbol
 
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