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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
15
C.235
B X
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?
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
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.
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.
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
16
COMPONENT: 20HW,HOLDING TIME ATALT (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 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
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.
　
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