曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

A.9,800 pounds.
B.11,200 pounds.
C.17,000 pounds.
B X
98..[Refer to Figure 4-30.] What thrust is required to
maintain level flight at 110,000 pounds, with gear down, flaps
40o, and an airspeed of 118 knots?
A.17,000 pounds.
B.20,800 pounds.
C.22,300 pounds.
B X
99..[Refer to Figure 4-32.] What is the turbulent air
penetration N1 power setting for Operating Conditions below?
WEIGHT (*1000): 100,PRESSURE ALTITUDE: 35,000,TOTAL AIR TEMP
(TAT): -11oC
A.83.4 percent.
B.86.0 percent.
C.87.4 percent.
C X
100..[Refer to Figure 4-32.] What is the turbulent air
penetration N1 power setting for Operating Conditions below?
WEIGHT (*1000): 80,PRESSURE ALTITUDE: 25,000,TOTAL AIR TEMP
(TAT): -28oC
A.77.5 percent.
B.75.3 percent.
C.79.4 percent.
B X
101.[Refer to Figure 4-32.] What is the turbulent air
penetration N1 power setting for Operating Conditions below?
WEIGHT (*1000): 90,PRESSURE ALTITUDE: 15,000,TOTAL AIR TEMP
(TAT): 11oC,
A.75.4 percent.
B.74.2 percent.
C.72.9 percent.
A X
102..[Refer to Figure 4-34.] What are the recommended IAS and
EPR settings for holding under Operating Conditions
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
103..[Refer to Figure 4-34.] What are the recommended IAS and
EPR settings for holding under Operating Conditions below?
ALTITUDE: 25,000,WEIGHT (*1000): 102.5,ENGINES OPERATING:
2,HOLDING TIME (MIN): 40
A.216 knots and 1.62 EPR.
B.223 knots and 2.01 EPR.
C.219 knots and 1.81 EPR.
A X
104..[Refer to Figure 4-34.] What are the recommended IAS and
EPR settings for holding under Operating Conditions below?
ALTITUDE: 35,000,WEIGHT (*1000): 100,ENGINES OPERATING:
2,HOLDING TIME (MIN): 30
A.221 knots and 1.83 EPR.
B.223 knots and 2.01 EPR.
C.217 knots and 1.95 EPR.
C X
105..[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
106..[Refer to Figure 4-34.] What is the approximate fuel
consumed when holding under Operating Conditions below?
ALTITUDE: 25,000,WEIGHT (*1000): 102.5,ENGINES OPERATING:
2,HOLDING TIME (MIN): 40
A.3,625 pounds.
B.3,240 pounds.
C.2,980 pounds.
B X
107..[Refer to Figure 4-34.] What is the approximate fuel
consumed when holding under Operating Conditions below?
ALTITUDE: 30,000,WEIGHT (*1000): 92.5,ENGINES OPERATING:
2,HOLDING TIME (MIN): 10
A.732 pounds.
B.1,023 pounds.
C.1,440 pounds.
A X
108..[Refer to Figure 4-37.] How many minutes of dump time
is required to reach a weight of 144,500 pounds? Initial
weight: 180,500 lb,Zero fuel weight: 125,500 lb
A.13 minutes.
B.15 minutes.
C.16 minutes.
B X
109..[Refer to Figure 4-37.] How many minutes of dump time
is required to reach a weight of 151,500 pounds? Initial
weight: 181,500 lb,Zero fuel weight: 126,000 lb
A.15 minutes.
B.14 minutes.
C.13 minutes.
C X
110..[Refer to Figure 4-37.] How many minutes of dump time
is required to reach a weight of 151,500 pounds? Initial
weight: 187,500 lb,Zero fuel weight: 125,500 lb
A.14 minutes.
B.16 minutes.
C.17 minutes.
C X
111..[Refer to Figure 4-37.] How many minutes of dump time
is required to reduce fuel load to 18,000 pounds? Initial
weight: 162,500 lb,Zero fuel weight: 120,500 lb
A.10 minutes.
B.9 minutes.
C.8 minutes.
A X
112..[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): 100,ENGINE ANTI-ICE:
ON,WING ANTI-ICE: ON,ISA TEMPERATURE: +10oC,AIR CONDITIONING:
ON
A.16,400 feet.
B.19,600 feet.
C.18,700 feet.
A X
113..[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): 80,ENGINE ANTI-ICE:
ON,WING ANTI-ICE: OFF,ISA TEMPERATURE: ISA,AIR CONDITIONING:
OFF
A.24,600 feet.
B.23,400 feet.
C.20,000 feet.
A X
114..[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
　
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