Airport Engineering Pick up the component not applicable to aeroplanes Air screw None of these Engines Wings Air screw None of these Engines Wings ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering Wing loading of an aircraft is 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 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 ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The length of clear zone for none instrument runway of a small aircraft is 750 m 300 m 600 m 150 m 750 m 300 m 600 m 150 m ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The depressions and undulations in the pavement, are caused due to Impact of heavy wheel loads All listed here Punching effect Improper compaction of sub-grade Impact of heavy wheel loads All listed here Punching effect Improper compaction of sub-grade ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering The lift off distance is the distance along the centre of the runway between the starting point and End of the runway End of stop-way Point where air craft attains a height of 10.7 m Point where air craft becomes air borne End of the runway End of stop-way Point where air craft attains a height of 10.7 m Point where air craft becomes air borne ANSWER DOWNLOAD EXAMIANS APP
Airport Engineering For determining the basic runway length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is 0.4 0.5 0.6 0.75 0.4 0.5 0.6 0.75 ANSWER DOWNLOAD EXAMIANS APP
EXAMIANS