Airport Engineering The size of landing area for multi engine helicopters operating under 1 FR conditions is 22.5 m × 22.5 m 22.5 m × 30 m 60 m × 120 m 30 m × 30 m 22.5 m × 22.5 m 22.5 m × 30 m 60 m × 120 m 30 m × 30 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 25 kmph 35 kmph 45 kmph 15 kmph 25 kmph 35 kmph 45 kmph 15 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Maximum gross takeoff weight of an aircraft is Less than the maximum structural landing weight Equal to the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload Less than the maximum structural landing weight Equal to the maximum structural landing weight More than the maximum structural landing weight Equal to the empty operating weight plus the payload ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The main disadvantage of angle nose out parking configuration of aircraft is that the Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building Overall apron area required is more Aircraft rear loading door is far away from terminal building All listed here Hot blast is directed towards the terminal building ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, the minimum basic runway length for A and E type of airport will be 2100 m and 750 m 1500 m and 750 m 2100 m and 600 m 1500 m and 600 m 2100 m and 750 m 1500 m and 750 m 2100 m and 600 m 1500 m and 600 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings Gross total weight of the aircraft/ wing area Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ load of the wings ANSWER DOWNLOAD EXAMIANS APP
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