Airport Engineering An aircraft is flying in an atmosphere of 30°C with a speed of 1260 kmph. Its speed is known as Subsonic Sonic Mach Super-sonic Subsonic Sonic Mach Super-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 0.043055555555556 0.045138888888889 0.069444444444444 0.047222222222222 0.043055555555556 0.045138888888889 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/total available H.P of engines Load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The lift off distance is the distance along the centre of the runway between the starting point and Point where air craft attains a height of 10.7 m End of the runway End of stop-way Point where air craft becomes air borne Point where air craft attains a height of 10.7 m End of the runway End of stop-way Point where air craft becomes air borne ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 35 kmph 45 kmph 15 kmph 25 kmph 35 kmph 45 kmph 15 kmph 25 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering To cope up high temperature of 196°C, the taxi ways and aprons are constructed with Plain concrete Asphaltic concrete Rubberised tar concrete All listed here Plain concrete Asphaltic concrete Rubberised tar concrete All listed here ANSWER DOWNLOAD EXAMIANS APP
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