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Private Pilot : 2007年 Airman Knowledge Test Question (Written Exam)
401.
An aircraft is loaded 110 pounds over maximum certificated gross weight. If fuel (gasoline) is drained to bring the aircraft weight within limits, how much fuel should be drained?
A) 15.7 gallons.
B) 16.2 gallons.
C) 18.4 gallons.
402.
(Refer to figures 33 and 34.) Determine if the airplane weight and balance is within limits.
|
Front seat occupants |
415 lb |
|
Rear seat occupants |
110 lb |
|
Fuel, main tanks |
44 gal |
|
Fuel, aux. tanks |
19 gal |
|
Baggage |
32 lb |
A) 19 pounds overweight, CG within limits.
B) 19 pounds overweight, CG out of limits forward.
C) Weight within limits, CG out of limits.
参考の表(Figures 33 and 34)はこちらへ
403.
(Refer to figure 35.) What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope?
|
|
WEIGHT (LB) |
MOM/1000 |
|
Empty weight |
1,350 |
51.5 |
|
Pilot and front passenger |
250 |
--- |
|
Rear passengers |
400 |
--- |
|
Baggage |
??? |
--- |
|
Fuel, 30 gal |
--- |
--- |
|
Oil, 8 qt |
--- |
-0.2 |
A) 105 pounds.
B) 110 pounds.
C) 120 pounds.
参照のグラフ(Figure 35)は
404.
(Refer to figure 35.) Calculate the moment of the airplane and determine which category is applicable.
|
|
WEIGHT (LB) |
MOM/1000 |
|
Empty weight |
1,350 |
51.5 |
|
Pilot and front passenger |
310 |
--- |
|
Rear passengers |
96 |
--- |
|
Fuel, 38 gal |
--- |
--- |
|
Oil, 8 qt |
--- |
-0.2 |
A) 79.2, utility category.
B) 80.8, utility category.
C) 81.2, normal category.
参照のグラフ(Figure 35)は
405.
(Refer to figure 35.) What is the maximum amount of fuel that may be aboard the airplane on takeoff if loaded as follows?
|
|
WEIGHT (LB) |
MOM/1000 |
|
Empty weight |
1,350 |
51.5 |
|
Pilot and front passenger |
340 |
--- |
|
Rear passengers |
310 |
--- |
|
Baggage |
45 |
--- |
|
Oil, 8 qt |
--- |
--- |
A) 24 gallons.
B) 32 gallons.
C) 40 gallons.
参照のグラフ(Figure 35)は
406.
An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be
A) a longer takeoff run.
B) difficulty in recovering from a stalled condition.
C) stalling at higher-than-normal airspeed.
407.
What is an advantage of a constant-speed propeller?
A) Permits the pilot to select and maintain a desired cruising speed.
B) Permits the pilot to select the blade angle for the most efficient performance.
C) Provides a smoother operation with stable RPM and eliminates vibrations.
和訳 : Constant-Speed Propellerの解説
408.
(Refer to figure 24.) While en route on Victor 185, a flight crosses the 248° radial of Allendale VOR at 0953 and then crosses the 216° radial of Allendale VOR at 1000. What is the estimated time of arrival at Savannah VORTAC?
A) 1023.
B) 1028.
C) 1036.
Figure 24 へ
409.
What is the definition of a high-performance airplane?
A) An airplane with 180 horsepower, or retractable landing gear, flaps, and a fixed-pitch propeller.
B) An airplane with an engine of more than 200 horsepower.
C) An airplane with a normal cruise speed in excess of 200 knots.
和訳と説明
410.
If recency of experience requirements for night flight are not met and official sunset is 1830, the latest time passengers may be carried is
A) 1829.
B) 1859.
C) 1929.
Private Pilot Knowledge Test (Private Written Exam) 05/23/2007 :
2008年の問題へ