FAAの筆記試験(Knowledge Exam)について。　：　 Privateの筆記試験について　：　PVTの問題へ　：　IFR、筆記の解説　：　IFR問題へ

2008-09　Private Pilot Knowｌedge (Private Written) Exam 米国自家用操縦士筆記試験

11. PLT245
In what flight condition must an aircraft be placed in order to spin?
A) Partially stalled with one wing low.
B) In a steep diving spiral.
C) Stalled.

12. PLT477
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.

和訳と解説

13. PLT168
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.

14. PLT194
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.

和訳と解説

15. PLT012
(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.

16. PLT012
(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.

17. PLT124
(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.

18. PLT019
(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.

19. PLT008
(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.

20. PLT019
(Refer to figure 8.) Determine the pressure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22 at standard temperature.
A) 2,913 feet MSL.
B) 2,991 feet MSL.
C) 3,010 feet MSL.