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Private Pilot : 2007年 Airman Knowledge Test Question (Written Exam)
21.
As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will
A) decrease as the true airspeed decreases.
B) decrease as the true airspeed increases.
C) remain the same regardless of altitude.
説明と訳、英単語も
22.
The angle of attack at which an airplane wing stalls will
A) increase if the CG is moved forward.
B) change with an increase in gross weight.
C) remain the same regardless of gross weight.
23.
An ATC radar facility issues the following advisory to a pilot flying north in a calm wind:
`TRAFFIC 9 O`CLOCK, 2 MILES, SOUTHBOUND...`
Where should the pilot look for this traffic?
A) South.
B) North.
C) West.
説明と訳、英単語も
24.
(Refer to figure 36.) What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions?
Pressure altitude
8,000 ft
Temperature
22 °C
Manifold pressure
20.8 inches Hg
Wind
Calm
A) 60.2 gallons.
B) 70.1 gallons.
C) 73.2 gallons.
To Figure 36
25.
(Refer to figure 36.) What fuel flow should a pilot expect at 11,000 feet on a standard day with 65 percent maximum continuous power?
A) 10.6 gallons per hour.
B) 11.2 gallons per hour.
C) 11.8 gallons per hour.
26.
(Refer to figure 8.) What is the effect of a temperature decrease and a pressure altitude increase on the density altitude from 90 °F and 1,250 feet pressure altitude to 55 °F and 1,750 feet pressure altitude?
A) 1,300-foot decrease.
B) 1,700-foot decrease.
C) 1,700-foot increase.
To Figure 8
27.
(Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97.
A) 1,341 feet MSL.
B) 1,451 feet MSL.
C) 1,562 feet MSL.
To Figure 8
28.
(Refer to figure 8.) What is the effect of a temperature increase from 30 to 50 °F on the density altitude if the pressure altitude remains at 3,000 feet MSL?
A) 900-foot increase.
B) 1,100-foot decrease.
C) 1,300-foot increase.
To Figure 8
29.
(Refer to figure 38.) Determine the approximate total distance required to land over a 50-foot obstacle.
OAT
90 °F
Pressure altitude
4,000 ft
Weight
2,800 lb
Headwind component
10 kts
A) 1,525 feet.
B) 1,775 feet.
C) 1,950 feet.
Figure 38 に
30.
(Refer to figure 38.) Determine the total distance required to land.
OAT
32 °F
Pressure altitude
8,000 ft
Weight
2,600 lb
Headwind component
20 kts
Obstacle
50 ft
A) 850 feet.
B) 1,400 feet.
C) 1,750 feet.
Figure 38 に
Private Pilot Knowｌedge Test (Private Written Exam) 05/23/2007 :
2008年の問題へ
