Airport Engineering Zero fuel weight of an aircraft is: Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight Less than empty operating weight Equal to maximum landing weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The runway orientation is made so that landing and takeoff are Perpendicular to wind direction Against the wind direction None of these Along the wind direction Perpendicular to wind direction Against the wind direction None of these Along the wind direction ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to All listed here Impact of heavy wheel loads Improper compaction of sub-grade Punching effect All listed here Impact of heavy wheel loads Improper compaction of sub-grade Punching effect ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Geometric design of holding apron of these statements 2 and 3 are correct 1 alone is correct 1 and 2 are correct 1 and 3 are correct 2 and 3 are correct 1 alone is correct 1 and 2 are correct 1 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight Less than the maximum structural landing weight Equal to the empty operating weight plus the payload More than the maximum structural landing weight Equal to the maximum structural landing weight ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Sonic Subsonic Mach Super-sonic Sonic Subsonic Mach Super-sonic ANSWER DOWNLOAD EXAMIANS APP
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