?
B.could cause FDP vapors to enter the aircraft but would have no effect on engine thrust or power.
?
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?
? ? ?
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?
? ? ?
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
?
Fuel coming from one tank to another during turbulent flight
? ?
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
? ?
A.warm the fuel
B.ensure an adequate supply of fuel pressure is maintained to the APU
?
C.prevent cavitation
正确答案:C
(123)Minimum specific fuel consumption of the turboprop engine is normally available in which altitude range?
? ? ?
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
? ? ?
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?
? ? ?
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 \
?
A.The one with the center of thrust closest to the centerline of the fuselage.
?
B.The one with the center of thrust farthest from the centerline of the fuselage.
?
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?
?
A.the altitude at which maximum allowable BMEP can be obtained
?
B.the highest altitude at which a desired manifold pressure can be obtained
?
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?
?
A.Highest altitude where the mixture can be leaned to best power ratio.
?
B.The highest altitude at which a desired manifold pressure can be obtained.
?
C.The altitude at which maximum allowable BMEP can be obtained.