ATPL网上题库4飞行原理 下载本文

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B.could cause FDP vapors to enter the aircraft but would have no effect on engine thrust or power.

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C.can reduce engine performance and cause surging and/or compressor stalls.

正确答案:C

(119)Which is an effect of ice, snow, or frost formation on an airplane?

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A.Decreased angle of attack for stalls. B.Decreased stall speed. C.Decreased pitchup tendencies.

正确答案:A

(120)Which is an effect of ice, snow, or frost formation on an airplane?

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A.Increased stall speed.

B.Increased pitchdown tendencies. C.Increased angle of attack for stalls.

正确答案:A

(121)Baffle plates in wing fuel cells prevent

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Fuel coming from one tank to another during turbulent flight

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Over pressure in the fuel tank

Movement of the fuel (surging) in the tank during acceleration/deceleration and in turbulence

正确答案:C

(122)Engine bleed air is supplied to the air gap above the fuel in the tanks primarily to

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A.warm the fuel

B.ensure an adequate supply of fuel pressure is maintained to the APU

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C.prevent cavitation

正确答案:C

(123)Minimum specific fuel consumption of the turboprop engine is normally available in which altitude range?

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A.10,000 feet to 25,000 feet. B.25,000 feet to the tropopause. C.The tropopause to 45,000 feet

正确答案:B

(124)ESHP (Equivalent shaft horsepower) of a turboprop engine is a measure of

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A.Turbine inlet temperature B.Shaft horsepower and jet thrust C.Propeller thrust only

正确答案:B

(125)What does the term of Equivalent shaft horsepower (ESHP) of a turboprop engine describe?

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A.shaft horsepower and jet thrust. B.jet thrust only. C.propeller thrust only.

正确答案:A

(126)What criteria determines which engine is the \

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A.The one with the center of thrust closest to the centerline of the fuselage.

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B.The one with the center of thrust farthest from the centerline of the fuselage.

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C.The one designated by the manufacturer, which develops most usable thrust.

正确答案:A

(127)Where is the critical altitude of a supercharged-reciprocating engine?

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A.the altitude at which maximum allowable BMEP can be obtained

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B.the highest altitude at which a desired manifold pressure can be obtained

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C.highest altitude where the mixture can be leaned to best power ratio

正确答案:B

(128)What is the definition of the critical altitude of a supercharged-reciprocating engine?

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A.Highest altitude where the mixture can be leaned to best power ratio.

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B.The highest altitude at which a desired manifold pressure can be obtained.

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C.The altitude at which maximum allowable BMEP can be obtained.