11. - PLT213
An airplane said to be inherently stable will
A) be difficult to stall.
B) require less effort to control.
C) not spin.
和訳 ： 「Stable」安定について
12. - 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.
和訳 ： 航空用語の説明
13. - 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
14. - 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.
和訳 ： 航空用語の説明
15. - 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
16. - 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 22C
Manifold pressure 20.8 inches Hg
Wind Calm
A) 60.2 gallons.
B) 70.1 gallons.
C) 73.2 gallons.
和訳 ： チャートの見方
17. - 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.
和訳 ： チャートの見方
18. - 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 ressure 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.
和訳 ： チャートの使い方
19. - 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.
和訳 ： チャートの使い方
20. - PLT008
(Refer to figure 38.) Determine the approximate total distance required to land over a 50-foot
obstacle.
OAT 90F
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.
和訳 ： Chartの読み方
