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controllable?
A.VSO.
B.VS.
C.VS1.
B X
146..At what minimum speed (rounded off) could dynamic
hydroplaning occur on main tires having a pressure of 121
PSI?
A.90 knots.
B.96 knots.
C.110 knots.
B X
147..What condition is necessary for the formation of
structural icing in flight?
A. flying in any clouds.
B. Flying in rain.
C. the temperature of the aircraft surface is 0oC or colder and
supercooled water drops.
C X
148..Which condition reduces the required runway for takeoff?
A.Higher-than-recommended airspeed before rotation.
B.Lower-than-standard air density.
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C.Increased headwind component.
C X
149..Which document includes descriptions of the required
crewmember functions to be performed in the event of an
emergency?
A. Airplane Flight Manual.
B. Certificate holder's manual.
C. Pilot's Emergency Procedures Handbook.
B X
150..[Refer to Figures 4-49, 4-50,4-51,4-52,4-53, and 4-54.]
What is the ETE at .80 Mach?
A.1 hours 02 minutes.
B.1 hours 04 minutes.
C.1 hours 07 minutes.
C X
151..(According to figure 6) What changes take place from
point B fly to point D
A. The wind speed increases, temperature rises
B. The wind speed increases, temperature reduced
C. The wind speed and wind direction is no changes,
temperature reduced
B X
152..When an ATC controller assigns a too low speed for the
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aircraft's operating limitation under the existing
circumstance, what should the pilot do?
A. reduce speed to the assigned speed.
B. reduce speed to the minimum speed at that circumstance.
C. advise ATC of the speed that will be used.
C X
153..The "age 60 rule" of CCAR Part 121 not applies to
A.any required pilot crewmember.
B.any flight crewmember.
C.flight engineer or navigator.
C X
154..(Refer to Figure 2-1and 2-2) To which aircraft position
dose HSI presentation "D" correspond?
A.4
B.15
C.17
C X
155..(Refer to Figure 2-6) What is the magnetic bearing TO the
station as indicated by illustration 4?
A.285
B.055
C.235
B X
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156..What performance should a pilot of a light, twin-engine
airplane be able to maintain at Vmc ?
A.Heading.
B.Heading and altitude.
C.Heading, altitude, and ability to climb 50 ft/min.
A X
157..[Refer to Figure 4-39.] What is the approximate level-off
pressure altitude after drift-down under Operating
Conditions below?WT AT ENG FAIL (*1000): 90,ENGINE ANTI-ICE:
OFF,WING ANTI-ICE: OFF,ISA TEMPERATURE: +20oC,AIR
CONDITIONING: OFF
A.19,400 feet.
B.20,000 feet.
C.23,800 feet.
B X
158..When a speed adjustment is necessary to maintain
separation, what minimum speed may ATC request of a
turboprop arrival aircraft operating below 3,000 meters?
A. 210 knots
B. 200 knots
C. 170 knots
B X
159..What is the purpose of a prohibited airspace?
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A.To prohibit entry of any aircrafts.
B.To prohibit entry of air force aircrafts only.
C.To prohibit entry of civil aircrafts only.
A X
160..The critical altitude of a supercharged reciprocating
engine is
A.The highest altitude where the mixture can be leaned to best
power ratio.
B.The highest altitude at which a desired manifold pressure
can be obtained.
C.The altitude at which maximum allowable BMEP can be
obtained.
B X
161..[Refer to Figure 4-34.] What is the approximate fuel
consumed when holding under Operating Conditions
below? ,ALTITUDE: 35,000,WEIGHT (*1000): 100,ENGINES
OPERATING: 2,HOLDING TIME (MIN): 30
A.1,625 pounds.
B.1,950 pounds.
C.2,460 pounds.
C X
162..For a flag air carrier flight to be released to an island
airport for which an alternate airport is not available, a
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turbojet-powered airplane must have enough fuel to fly to
that airport and thereafter to fly
A. at least 2 hours at normal cruising fuel consumption.
B. for 3 hours at normal cruising fuel consumption.
C. back to the departure airport.
A X
163..If the airplane flies through a high pressure center in the
northern hemisphere, the wind direction usually changes.
A. from headwind to tailwind.
B. from left crosswind to right crosswind.
C. from right crosswind to left crosswind
C X
164..What is the purpose of a servo tab?
A.Move the flight controls in the event of manual reversion.
B. Reduce control forces by deflecting in the proper direction
to move a primary flight control.
　
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