Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/total available H.P of engines Load of the wings 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 Super-sonic Subsonic Mach Sonic Super-sonic Subsonic Mach Sonic ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The slope of the obstruction clearance line from the boundary of the heliport should be 0.069444444444444 0.047222222222222 0.045138888888889 0.043055555555556 0.069444444444444 0.047222222222222 0.045138888888889 0.043055555555556 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Beaufort scale is used to determine None of these Height of air-crafts Direction of winds Strength of winds None of these Height of air-crafts Direction of winds Strength of winds ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Geometric design of holding apron of these statements 1 and 2 are correct 1 and 3 are correct 1 alone is correct 2 and 3 are correct 1 and 2 are correct 1 and 3 are correct 1 alone is correct 2 and 3 are correct ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Total correction for elevation, temperature and gradient for a runway should not be more than 0.15 0.2 0.35 0.25 0.15 0.2 0.35 0.25 ANSWER DOWNLOAD EXAMIANS APP
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