Airport Engineering For the proposed runway stated in if the aerodrome reference temperature is 17.2°, the net designed length of the runway is 2816 m 3016 m 2916 m 2716 m 2816 m 3016 m 2916 m 2716 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The capacity of parallel runway pattern depends upon Lateral spacing between two runways and weather conditions Lateral spacing between two runways and navigational aids available Lateral spacing between two runways, weather conditions and navigational aids available. Weather conditions and navigational aids available Lateral spacing between two runways and weather conditions Lateral spacing between two runways and navigational aids available Lateral spacing between two runways, weather conditions and navigational aids available. Weather conditions and navigational aids available ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings Gross total weight of the aircraft/total available H.P of engines Gross total weight of the aircraft/ wing area Gross total weight of the aircraft/ load of the wings Load of the wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Castor angle is defined as the angle Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the direction of wind and the longitudinal axis of the runway ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 15 kmph 45 kmph 25 kmph 35 kmph 15 kmph 45 kmph 25 kmph 35 kmph ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Equal to empty operating weight Less than empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to maximum landing weight Equal to empty operating weight Less than empty operating weight ANSWER DOWNLOAD EXAMIANS APP
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