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
Private Pilot : 2007年 Airman Knowledge Test Question (Written Exam)
緑色の問題は、Airplane以外やPrivate以外の問題です。
631.
FAA advisory circulars containing subject matter specifically related to Air Traffic Control and General Operations are issued under which subject number?
A) 60.
B) 70.
C) 90.
632.
The maximum altitude that a rigid airship can reach (under a given atmospheric condition) and then return safely to the surface is determined by
A) the disposable load.
B) ballonet capacity.
C) pressure altitude.
633.
An unbalanced condition of an airship in flight must be overcome by
A) valving air from the ballonets.
B) valving gas from the envelope.
C) a negative or a positive dynamic force.
634.
Which items are included in the empty weight of an aircraft?
A) Unusable fuel and undrainable oil.
B) Only the airframe, powerplant, and optional equipment.
C) Full fuel tanks and engine oil to capacity.
635.
High airspeeds, particularly in turbulent air, should be avoided primarily because of the possibility of
A) an abrupt pitchup.
B) retreating blade stall.
C) a low-frequency vibration developing.
636.
The upward bending of the rotor blades resulting from the combined forces of lift and centrifugal force is known as
A) coning.
B) blade slapping.
C) inertia.
637.
(Refer to figure 10.) During flight, if cyclic control pressure is applied which results in a maximum increase in pitch angle of the rotor blade at position A, the rotor disc will tilt
A) forward.
B) aft.
C) left.
Figure 10
638.
(Refer to figure 40.) Determine the total takeoff distance required for a gyroplane to clear a 50-foot obstacle if the temperature is 95 °F and the pressure altitude is 1,700 feet.
A) 1,825 feet.
B) 1,910 feet.
C) 2,030 feet.
Figure 40へ
639.
(Refer to figure 40.) Determine the total landing distance to clear a 50-foot obstacle in a gyroplane. The outside air temperature (OAT) is 75°F and the pressure altitude at the airport is 2,500 feet.
A) 521 feet.
B) 525 feet.
C) 529 feet.
Figure 40へ
640.
For internal cooling, reciprocating aircraft engines are especially dependent on
A) a properly functioning thermostat.
B) air flowing over the exhaust manifold.
C) the circulation of lubricating oil.
和訳 と Engine Coolingに付いて
緑色の問題は、Airplane以外やPrivate以外の問題です。
Private Pilot Knowledge Test (Private Written Exam) 05/23/2007 :
2008年の問題へ