Airport Engineering As per ICAO, for airports serving big aircrafts, the crosswind component should not exceed 25 kmph 15 kmph 35 kmph 45 kmph 25 kmph 15 kmph 35 kmph 45 kmph 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 Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear Between the horizontal and the fuselage axis Between the true speed of the aircraft and the crosswind component Between the direction of wind and the longitudinal axis of the runway Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Punching effect Improper compaction of sub-grade Impact of heavy wheel loads All listed here Punching effect Improper compaction of sub-grade Impact of heavy wheel loads All listed here ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Zero fuel weight of an aircraft is: Equal to maximum landing weight Less than empty operating weight Equal to sum of empty operating weight and the maximum pay load Equal to empty operating weight Equal to maximum landing weight Less than empty operating 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 length of clear zone for none instrument runway of a small aircraft is 600 m 150 m 750 m 300 m 600 m 150 m 750 m 300 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The thickness design of the pavement, is decided on the load carried by Main gears Nose wheel Tail wheel All listed here Main gears Nose wheel Tail wheel All listed here ANSWER DOWNLOAD EXAMIANS APP
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