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C. Prevent a control surface from moving to a full-deflection
position due to aerodynamic forces.
B X
165..Duty and rest period rules require that a flight
crewmember
A.not be assigned to any duty with the air carrier during any
required rest period.
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B.not be on duty aloft for more than 100 hours in any 30-day
period.
C.be relieved of all duty for at least 24 hours during any 7
consecutive days.
A X
166..[Refer to Figure 4-41.] What is the total time from
starting to the alternate through completing the approach
for Operating Conditions below? WEIGHT (START TO ALT):
84,000,DISTANCE (NM): 120,WIND COMPONENT: 20HW,HOLDING
TIME AT ALT (MIN): 15
A.30 minutes.
B.45 minutes.
C.29 minutes.
B X
167..What flight condition should be expected when an aircraft
leaves ground effect?
A.An increase in induced drag requiring a higher angle of
attack.
B.A decrease in parasite drag permitting a lower angle of
attack.
C.An increase in dynamic stability.
A X
168..(Refer to Figure 6-2) If an aircraft is cleared to
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circle-to-land on Rwy 36L at CAPITAL, and its maximum speed
is approximately 180 knots, what height above the airport
could it descend to?
A.870 feet.
B.762 feet.
C.755 feet.
C X
169..(Refer to Figure 6-2) The highest terrain shown in the
plan view section of the ILS/DME Rwy 36L approach chart is
A.1,496 feet.
B.1,244 feet.
C.900 feet.
B X
170..An air carrier may schedule a pilot to fly in an airplane,
in any calendar month, for no more than
A.80hours
B.90 hours
C.100hours
B X
171..Identify the type stability if the aircraft attitude
remains in new position after the controls have been
neutralized.
A.Negative longitudinal static stability
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B. Neutral longitudinal dynamic stability
C.-Neutral longitudinal static stability
C X
172..Which performance factor decreases as airplane gross
weight increases, for a given runway?
A.Critical engine failure speed.
B.Rotation speed.
C.Accelerate-stop distance.
A X
173..The blind spot is
A.the area of the lens which is screened by the iris.
B.at the junction of the optic nerve and the retina
C.an area on the cornea which does not respond to light.
B X
174..What action should a pilot take when a clearance appears
to be contrary to a regulation?
A.Request a clarification from the ATC.
B.Read the clearance back entirely.
C.Do not accept the clearance.
A X
175..The fuel reserve required for a
reciprocating-engine-powered supplemental air carrier
airplane upon arrival at the most distant alternate airport
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during a flight in the contiguous China is
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.
A X
176..[Refer to Figure 4-25.] Which of the following
configurations will result in the shortest landing distance
over a 50-foot obstacle to a dry runway?
A.Brakes and spoilers at 125,000 pounds gross weight.
B.Brakes and reversers at 115,000 pounds gross weight.
C.Brakes, spoilers, and reversers at 130,000 pounds gross
weight.
C X
177..Which letter do you select to fill in the TYPE OF FLIGHT
box during IFR flight training?
A.N.
B.S.
C.G.
C X
178..In northern sphere, the air cyclone circumfluence is
A. outward, downward and clockwise
B. outward, upward and clockwise
C. inward, upward and counterclockwise
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C X
179..It is the responsibility of the pilot and crew to report a
near midair collision as a result of proximity of at least
A. 50 feet or less to another aircraft.
B. 500feet or less to another aircraft.
C. 1,000 feet or less to another aircraft.
B X
180..In northern hemisphere, if fly from high pressure area to
low pressure area at 6000 meters, the wind on the course is
_____.
A.right crosswind
B.tailwind
C. left crosswind
C X
181..which rule applies to the use of the cockpit voice
recorder erasure feature?
A.All recorded information may be erased, except for the last
30 minutes prior to landing.
B.Any information more than 30 minutes old may be erased
C.All recorded information may be erased, unless the NTSB
needs to be notified of an occurrence.
B X
182..What is the purpose of a control tab?
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A.Move the flight controls in the event of manual reversion.
B.Reduce control forces by deflecting in the proper direction
　
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